Embraer EMB145 Operation Manual
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Embraer EMB145 Operation Manual

Embraer EMB145 Operation Manual

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Table of Contents

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AIRPLANE OPERATIONS MANUAL
This manual is applicable to the EMB-145 airplanes equipped
with AE3007A1 engines operating under FAA certification.
THIS
PUBLICATION
OPERATIONS MANUAL AOM–145/1114 VOLUME 2
TEMPORARY REVISION 41.1 – SEPTEMBER 15, 2015
In connection with the use of this document, Embraer does not provide any express or implied warranties and
expressly disclaims any warranty of merchantability or fitness for a particular purpose.
This document contains trade secrets, confidential, proprietary information of Embraer and technical data subject to
U.S. Export Administration Regulation ("EAR") and other countries export control laws and regulations. Diversion
contrary to the EAR and other laws and regulations is strictly forbidden. The above restrictions may apply to data on
VOLUME 1
EMBRAER S.A.
IS
INCOMPLETE
all pages of this document.
Copyright © 2015 by Embraer S.A. All rights reserved.
WITHOUT
AIRPLANE
AOM–145/1114-105
OCTOBER 31, 1996

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Summary of Contents for Embraer EMB145

  • Page 1 OCTOBER 31, 1996 TEMPORARY REVISION 41.1 – SEPTEMBER 15, 2015 In connection with the use of this document, Embraer does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose.
  • Page 2 OCTOBER 31, 1996 REVISION 41 – MARCH 06, 2015 In connection with the use of this document, Embraer does not provide any express or implied warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose. This document contains trade secrets, confidential, proprietary information of Embraer and technical data subject to U.S.
  • Page 4 Sincerely, Embraer Flight Operations Support Please return this form to: Embraer - VOC/DSS/GEO - PC176/2 Av. Brigadeiro Faria Lima, 2170 CEP 12227-901 São José dos Campos - SP - BRASIL Phone: +55 12 3927-1706...
  • Page 5 Airplane Operations Manual AOM–145/1114 Section/Page/Code: Date of Page: Revision: Name: Position: Company: Fax Number: Phone Number: E-Mail: Comment/Suggestion: Space reserved for Embraer CCF nº: Comment received: Date Acknowledged: Person in Charge: Action to be taken: Proposed date for implementation: Implemented:...
  • Page 6 Rain Repellent Coating  1-01-82 code 02 installation that can perform the Windshield Wiper functions. Removed steps from Before Takeoff  1-02-01 code 01 Checklist. Page Code REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 7 Changed the denomination of loose snow to  1-04-30 code 02 dry snow. Included block-code containing  1-12-60 code 01 information about Ground Resets procedures. Page Code REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 8 Windshield Wiper functions. Included information related incorporation of SB 145-35-0008, which  2-16-05 code 01 provides gaseous oxygen supply in the lavatories. Page Code REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 9 HIGHLIGHTS OF AIRPLANE CHANGE OPERATIONS MANUAL Included information related incorporation of SB 145-35-0008, which  2-16-15 code 01 provides gaseous oxygen supply in the lavatories. Page Code REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 10 RECORD OF AIRPLANE TEMPORARY OPERATIONS REVISIONS MANUAL RECORD OF TEMPORARY REVISIONS AOM–145/1114-105 TR 41.1 ................SEP 15, 2015 TEMPORARY REVISION 41.1 RTR-1 Copyright © by Embraer. Refer to cover page for details.
  • Page 11 RECORD OF AIRPLANE TEMPORARY OPERATIONS REVISIONS MANUAL INTENTIONALLY BLANK TEMPORARY REVISION 41.1 RTR-2 Copyright © by Embraer. Refer to cover page for details.
  • Page 12 REVISION....35 ....JUN 30, 2008 REVISION....36 ....DEC 19, 2008 REVISION....37 ....OCT 30, 2009 REVISION....38 ....AUG 15, 2011 REVISION....39 ....OCT 22, 2012 Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 13 REVISION....41 ....MAR 06, 2015 NOTE: The references to the deleted pages from the previous revisions (revision 40 and earlier) were removed from the LEP. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 14 REVISION 41 1-LEP REVISION 41 1-LEP REVISION 41 1-LEP REVISION 41 1-LEP REVISION 41 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 15 REVISION 41 1-00-10 REVISION 41 1-00-10 REVISION 41 1-00-10 REVISION 41 1-00-10 REVISION 41 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 16 145 FAA LR 1-01-05 REVISION 31 1-01-05 REVISION 31 1-01-05 REVISION 31 1-01-05 REVISION 31 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 17 REVISION 41 1-01-38 REVISION 39 1-01-38 REVISION 39 1-01-40 REVISION 41 145 A1 FAA * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 18 1-01-80 REVISION 38 FAA PRIMUS 1000 AFCS 1-01-80 REVISION 38 1-01-82 REVISION 41 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 19 REVISION 37 1-02-17 REVISION 37 1-02-17 REVISION 38 1-02-17 REVISION 37 1-02-17 REVISION 37 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 20 1-02-37 REVISION 40 1-02-37 REVISION 40 1-02-40 REVISION 34 ALL EXCEPT XR A1E * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 21 REVISION 41 1-02-79 REVISION 41 1-02-79 REVISION 41 1-02-79 REVISION 41 1-02-79 REVISION 41 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 22 REVISION 40 1-02-80 REVISION 40 1-02-80 REVISION 40 1-02-80 REVISION 40 1-02-80 REVISION 40 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 23 REVISION 40 1-02-80 REVISION 40 1-02-80 REVISION 40 1-02-80 REVISION 40 1-02-80 REVISION 40 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 24 REVISION 39 1-02-94 REVISION 39 1-02-95 REVISION 36 1-02-95 REVISION 36 1-02-95 REVISION 36 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 25 1-03-03 REVISION 40 1-03-05 REVISION 25 1-03-05 REVISION 24 1-03-05 MAR 30, 2001 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 26 1-03-26 MAR 30, 2001 1-03-30 REVISION 39 1-03-30 REVISION 40 1-03-30 REVISION 40 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 27 REVISION 38 1-03-45 REVISION 40 1-03-45 REVISION 40 1-03-45 REVISION 40 1-03-45 REVISION 40 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 28 REVISION 41 1-03-56 REVISION 41 1-03-56 REVISION 41 1-03-56 REVISION 41 1-03-56 REVISION 41 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 29 REVISION 40 1-03-60 DEC 20, 2002 1-03-60 MAR 30, 2001 1-03-65 REVISION 25 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 30 REVISION 38 1-03-70 REVISION 38 1-03-70 REVISION 38 1-03-70 REVISION 38 1-03-70 REVISION 38 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 31 1-04-03 REVISION 34 1-04-03 REVISION 34 1-04-03 REVISION 34 1-04-05 DEC 20, 2002 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 32 1-04-15 REVISION 20 145 A1 FAA lb 1-04-15 REVISION 32 1-04-15 REVISION 32 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 33 REVISION 40 1-04-20 REVISION 40 1-04-20 REVISION 40 1-04-20 REVISION 40 1-04-20 REVISION 40 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 34 REVISION 41 1-04-30 REVISION 41 1-04-30 REVISION 41 1-04-30 REVISION 41 1-04-30 REVISION 41 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 35 REVISION 41 1-04-30 REVISION 41 1-04-30 REVISION 41 1-04-30 REVISION 41 1-04-30 REVISION 41 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 36 REVISION 40 1-05-10 REVISION 40 1-05-10 REVISION 40 1-05-10 REVISION 40 1-05-10 REVISION 40 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 37 REVISION 40 1-05-15 REVISION 40 1-05-15 REVISION 40 1-05-15 REVISION 40 1-05-15 REVISION 40 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 38 145 A1, A1P lb 1-05-35 REVISION 39 1-05-35 REVISION 39 1-05-35 REVISION 39 1-05-35 REVISION 39 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 39 MAR 28, 2002 1-05-40 MAR 28, 2002 1-05-40 MAR 28, 2002 1-05-40 MAR 28, 2002 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 40 REVISION 38 1-05-50 REVISION 38 1-05-50 REVISION 38 1-05-50 REVISION 38 1-05-50 REVISION 38 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 41 DEC 20, 2002 1-06-30 DEC 20, 2002 1-06-30 JUN 29, 2001 1-06-30 JUN 29, 2001 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 42 1-06-50 SEP 20, 1999 1-07-00 REVISION 38 1-07-00 REVISION 38 1-07-10 REVISION 23 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 43 REVISION 36 145 Interior 1 +145 XR 1-07-30 REVISION 36 1-07-30 REVISION 36 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 44 Cart stowage unit 1-07-70 REVISION 38 1-07-70 REVISION 38 1-07-70 REVISION 38 1-07-70 REVISION 38 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 45 FAA/EASA 1-08-23 REVISION 39 1-08-28 REVISION 40 1-08-28 REVISION 36 1-08-28 REVISION 36 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 46 REVISION 27 1-08-57 REVISION 27 1-08-78 REVISION 27 1-08-78 REVISION 27 1-09-00 REVISION 36 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 47 SEP 29, 2000 1-10-08 DEC 20, 2002 145 Interior 1 - 50 pax * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 48 1-10-30 SEP 20, 1999 1-10-35 REVISION 30 1-10-35 REVISION 30 1-10-35 REVISION 31 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 49 SEP 20, 1999 1-12-05 SEP 20, 1999 1-12-05 SEP 20, 1999 1-12-10 REVISION 39 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 50 REVISION 38 1-12-25 REVISION 38 1-12-25 REVISION 38 1-12-25 REVISION 38 1-12-25 REVISION 38 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 51 1-12-50 SEP 20, 1999 1-12-60 REVISION 41 1-12-60 REVISION 41 1-12-60 REVISION 41 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 52 REVISION 41 1-12-60 REVISION 41 1-12-60 REVISION 41 1-12-60 REVISION 41 1-12-60 REVISION 41 * Asterisk indicates pages revised, added or deleted by the current revision. Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 53 LIST OF AIRPLANE EFFECTIVE PAGES OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-LEP REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 54 TABLE OF AIRPLANE CONTENTS OPERATIONS MANUAL TABLE OF CONTENTS AOM - VOLUME 1 1-00 - GENERAL INFORMATION AND DEFINITION OF TERMS 1-01 - LIMITATIONS 1-02 - NORMAL PROCEDURES 1-03 - EMERGENCY ABNORMAL PROCEDURES 1-04 - PERFORMANCE 1-05 - FLIGHT PLANNING 1-06 - WEIGHT AND BALANCE 1-07 -...
  • Page 55 TABLE OF AIRPLANE CONTENTS OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-TOC REVISION 23...

  • Page 56: Table Of Contents

    GENERAL AIRPLANE OPERATIONS MANUAL SECTION 1-00 GENERAL INFORMATION AND DEFINITION OF TERMS TABLE OF CONTENTS Page Block General Information ..............1-00-00 Definition of Terms..............1-00-10 Units Conversion ................1-00-20 EICAS Versions ................1-00-30 Service Bulletin Table ..............1-00-35 Page Code 1-00-00 REVISION 39...

  • Page 57: General Information

    The information contained herein is based on the airplane as delivered and further modifications developed and supplied by Embraer, as well as customizations requested by the original owner/operator. It is the owner/operator sole responsibility to guarantee that Embraer has complete and accurate information on any modifications made to the delivered configuration.
  • Page 58 GENERAL OPERATIONS MANUAL In the EMBRAER Operational Manuals, the Brazilian Civil Aviation authority is identified as both ANAC and CTA. Therefore, whenever you find either, it corresponds to Brazilian certification. This is because since March 21, 2006, the Brazilian Civil Aviation authority was replaced by Civil Aviation National Agency (ANAC) instead of CTA.
  • Page 59 The idea is to standardize manuals, training and operation, so as to make it easier for a pilot to change equipment. As an example, if a pilot used to fly an EMBRAER airplane (ERJ-145) is scheduled to fly another EMBRAER airplane (EMBRAER 170/175/190/195), the training syllabus required for both airplane families/models needs to be very similar;...
  • Page 60 Presents training information. EMBRAER AIRPLANE OPERATIONS MANUAL This EMBRAER Airplane Operations Manual covers only Part B. Parts A and D should be generated by the operator only. Part C can be generated by the operator with the help of EMBRAER operations software (runway analysis, driftdown and route analysis).
  • Page 61 GENERAL AIRPLANE OPERATIONS MANUAL − Volume 2: − 2-1 Airplane Description − 2-2 Equipment and Furnishings − 2-3 Emergency Equipment − 2-4 Crew Awareness − 2-5 Electrical − 2-6 Lighting − 2-7 Fire Protection − 2-8 Fuel − 2-9 Auxiliary Power Unit −...
  • Page 62 GENERAL AIRPLANE OPERATIONS MANUAL The page numbering of each part is independent from the remaining parts. Each page number is presented just to the right of the block number. As a complement, a code number is provided, to help identifying to which configuration each block is applicable.
  • Page 63 OPERATIONS MANUAL REVISIONS EMBRAER may revise this manual periodically as required to update information or to provide information not available at the time of printing the original issue. Revised data may result from EMBRAER approved airplane modifications or from improved techniques gained through operational experience.

  • Page 64: Definition Of Terms

    OTHER RELATED INFORMATION WHICH RESULT DAMAGE DESTRUCTION EQUIPMENT, IF NOT CAREFULLY FOLLOWED. NOTE: Operating procedures, techniques other related information which are considered essential to emphasize. Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 65 Kilograms per Hour Knot Pounds Meter Milibar Minute Millimeter Miles per Hour Nautical Mile Pound per Square Inch Second Ampere Aircraft Alternating Current Air Cycle Machine Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 66 Automatic Navigation Realignment Antenna Angle of Attack Autopilot Antenna Position Indicator Automatic Power Reserve Auxiliary Power Unit APU Starting Contactor Air Traffic Control ATDT, ATTD Attendant Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 67 Brake Control Unit Brake Control Valve Beat Frequency Oscillator Built In Test BKUP INPH Back-Up Interphone Bleed Bus Tie Contactor Bottle CAB EMERG Cabin Emergency Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 68 COMM, COM Communication Continuous CPAM Cabin Pressure Acquisition Module CPCS Cabin Pressure Control System Cruise Cruise Compressor Variable Geometry Cockpit Voice Recorder Clockwise Digital Audio Panel Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 69 Electrical Distribution Logic Electrical Distribution System EFIS Electronic Flight Instrument System EGPWS Enhanced Ground Position Warning System Exhaust Gas Temperature EHSI Electronic Horizontal Situation Indicator Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 70 Flight Level Change Mode Flexible Flight Management System FPDU Flap Power and Drive Unit FPLN Flight Plan FPMU Fuel Pump and Metering Unit FQIS Fuel Quantity Indicating System Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 71 Ground Power Contactor Global Positioning System Ground Power Unit GPWS Ground Proximity Warning System Heading High Frequency High Pressure HectoPascal HSCU Horizontal Stabilizer Control Unit Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 72 Inertial Reference System Inertial Reference Unit International Standard Atmosphere ISIS Integrated Standby Instrument System Interturbine Temperature KCAS Calibrated Airspeed in Knots KEAS Equivalent Airspeed in Knots Kilohertz Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 73 Lightning Detection Mach Mean Aerodynamic Chord Manual Maximum Marker Beacon Minimum Enroute Altitude Multifunction Display MFDU Magnetic Flux Detector Unit Megahertz Minimum Marker Microwave Landing System Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 74 Operations Manual OUTBD Outboard OVHT Overheating OVLD Overload OVPRESS Overpressure Oxygen Passenger Address Amplifier Passenger Address System PAST Pilot Activated Self Test Passenger Protective Breathing Equipment Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 75 Question Normal Height - Sea Level Pressure (Q-code) Quantity Radio Altimeter Receiver/Transmitter/Antenna REACT Rain Echo Attenuation Compensation Technique Reference Remote Engine Inoperative Right-hand Radio Magnetic Indicator Radio Management System Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 76 Short Range Single Sideband Traffic Advisory True Airspeed Total Air Temperature TCAS Traffic Alert and Collision Avoidance System Transponder TACAN Tactical Air Navigation Aid TEMP Temperature Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 77 Very High Frequency Maximum Landing Gear Extended Speed Very Low Frequency Maximum Landing Gear Operating Speed Lift Off Speed Valve Visual Minimum Condition Air Minimum Control Speed Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 78 Landing Reference Speed associated to the REFXX flap setting XX Stall Speed Vertical Speed Windshield Weight and Balance Wide Bandwidth Wing Weather Detection Cross Transfer Page Code 1-00-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 79 RELIEF VALVE OPTIONAL EQUIPMENT SYSTEM MODULE COMMUNICATION LINE ELECTRIC PUMP MECHANIC PUMP ACCUMULATOR ELECTRIC CONTACTOR (OPEN POSITION) SWITCH NACA AIR INLET Page Code 1-00-10 REVISION 41 (Pages 17 and 18 deleted) Copyright © by Embraer. Refer to cover page for details.

  • Page 80: Units Conversion

    GENERAL AIRPLANE OPERATIONS MANUAL UNITS CONVERSION TO CONVERT INTO MULTIPLY BY AND ADD Degree Celsius Degree Fahrenheit 1.8000 (ºC) (ºF) Degree Fahrenheit Degree Celsius 0.5556 -17.7778 (ºF) (ºC) Feet (ft) Meter (m) 0.3048 Inches (In) Millimeter (mm) 25.4000 Inches of Mercury Millibar (mb) 33.8636 (in.Hg)
  • Page 81 GENERAL AIRPLANE OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-00-20 REVISION 13...

  • Page 82: Eicas Versions

     E1 (2) CTL A (B) FAIL revised (indicates loss of CVG/MMV control);  E1 (2) NO DISP incorporated;  E1 (2) SHORT DISP incorporated. Page Code 1-00-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 83  Support to Inertial System (IRS) as an AHRS replacement.  Improvement in the Cabin Pressure Control System (CPCS) indication in order to avoid unnecessary amber indication on the EICAS. Page Code 1-00-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 84  Electrical system display improvements : valid GPU 0V voltage and valid Generator 0A amperage.  Oil Pressure limits presented in both amber and red bands above the green one. Page Code 1-00-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 85 (4) For EICAS 14, a placard is installed in the cockpit allowing the operation in the amber band, between 91 and 115 psi, during the takeoff and go-around phases, time limited to 5 minutes. Page Code 1-00-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 86  Change of HGS FAIL from ADVISORY to AMBER (caution) to comply with AC 120-28D requirements.  AHRS:  New advisory messages AHRS 1-2 NO PPOS, AHRS 1-2 NO MAG HDG. Page Code 1-00-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 87 Windshear indication on PFD always in red when RA test button is  pressed. Due to mandatory installation of IM-600 on this EICAS version and  on, the CAT II Operation is available and indicated. Page Code 1-00-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 88  EMB-145 XR model). New message HI ALT LDG-T/O (only applicable to EMB-145 XR  model). Changes to cabin altitude indication on EICAS display.  Page Code 1-00-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 89 Pitch Primary Monitor during the Coupled Autopilot Go- Around test (only applicable to EMB-145 XR model). General Changes New AZ-950 MADC Maintenance Page on PFD.  Page Code 1-00-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 90 This modification is enabled only in the 135 family airplane (EMB-135ER, EMB-135LR and EMB-135BJ) via IM-600 new parameter called RUDDER BIAS. Page Code 1-00-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 91 Thrust Set, and N2 is below 53.6%, then the message is inhibited. Besides, it was included a time delay of 5 seconds to activate the message. Page Code 1-00-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 92: Service Bulletin Table

    Electromechanical Gust Lock Lever Redesign. SB 145-28-0018 High Level Exceeding Indication System Installation. SB 145-30-0019 Improves the Piccolo Burst Monitoring System. SB 145-30-0021 Replaces the Anti-Icing System Valves. Page Code 1-00-35 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 93 Changes Nose Wheel Steering System logic. SB 145-34-0046 Improves TCAS/AWU interface. SB 145-34-0049 Changes the Integrated Standby Instrument System (ISIS) into new P/N C16221GC03 - Amendment A. Page Code 1-00-35 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 94 SB 145-73-0010 Incorporates FADEC B5.1.1 Version AE3007A and A1/1 Engines. SB 145-73-0011 Incorporates FADEC B5.1.1 Version AE3007A1 Engines. SB 145-73-0012 Incorporates FADEC B5.1.1 Version AE3007A1P Engines. Page Code 1-00-35 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 95 Includes Placard for 115 psi Oil Pressure Limit. SB 145-77-0004 New EICAS N2 Red Line Margin for A1 and A1/3 Engines. SB T-62T-49-152 Incorporates Modification to Permit APU Start Above 25000 ft. Page Code 1-00-35 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 96 LIMITATIONS AIRPLANE OPERATIONS MANUAL SECTION 1-01 LIMITATIONS TABLE OF CONTENTS Page Block Introduction ................1-01-00 General Limitations ..............1-01-01 Weight and CG ................1-01-05 Operational Limitations .............. 1-01-10 Supplementary Operational Limitations (*) ........ 1-01-12 Systems: Crew Alerting................. 1-01-30 Electrical ................1-01-32 Fuel ..................

  • Page 97: Introduction

    LIMITATIONS AIRPLANE OPERATIONS MANUAL INTRODUCTION The airplane must be operated in accordance with the limitations presented in this Section. These limitations also apply to operations in accordance with an approved Supplement or Appendix to the AFM, except as modified by such Supplement or Appendix. The information contained in this section is derived from the Approved Airplane Flight Manual.
  • Page 98 LIMITATIONS AIRPLANE OPERATIONS MANUAL GENERAL MINIMUM CREW Minimum Flight Crew ............ PILOT AND COPILOT KINDS OF OPERATION This airplane may be flown day and night in the following conditions, when the appropriate equipment and instruments required by airworthiness and operating regulations are approved, installed and in an operable condition: −...
  • Page 99 LIMITATIONS AIRPLANE OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-01-01 REVISION 39...
  • Page 100 LIMITATIONS AIRPLANE EMB-145 ER FAA OPERATIONS MANUAL WEIGHT AND CENTER OF GRAVITY EMB-145 ER MODEL - TAKEOFF WITH FLAPS 9° APPLICABLE TO AIRPLANES PRE-MOD. SB 145-53-0064. MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 45635 lb...

  • Page 101: Weight And Cg

    LIMITATIONS AIRPLANE EMB-145 ER FAA OPERATIONS MANUAL APPLICABLE TO AIRPLANES POST-MOD. SB 145-53-0064 OR EQUIPPED WITH AN EQUIVALENT MODIFICATION FACTORY INCORPORATED. MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 45635 lb 45414 lb 41226 lb...
  • Page 102 LIMITATIONS AIRPLANE EMB-145 ER FAA OPERATIONS MANUAL EMB-145 ER MODEL - TAKEOFF WITH FLAPS 22° APPLICABLE TO AIRPLANES PRE-MOD. SB 145-53-0064. MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 45635 lb 45414 lb 41226 lb...
  • Page 103 LIMITATIONS AIRPLANE EMB-145 ER FAA OPERATIONS MANUAL APPLICABLE TO AIRPLANES POST-MOD. SB 145-53-0064 OR EQUIPPED WITH AN EQUIVALENT MODIFICATION FACTORY INCORPORATED. MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 45635 lb 45414 lb 41226 lb...
  • Page 104 LIMITATIONS AIRPLANE EMB-145 ER FAA OPERATIONS MANUAL To comply with the performance and operating limitations of the regulations, the maximum allowable takeoff and landing operational weights may be equal to, but not greater than, the design limits. The takeoff weight (weight at brake release or at start of takeoff run) is the lowest among MTOW and the following weights: −...
  • Page 105 LIMITATIONS AIRPLANE EMB-145 ER FAA OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-01-05 REVISION 31...
  • Page 106 LIMITATIONS AIRPLANE EMB-145 LR FAA OPERATIONS MANUAL WEIGHT AND CENTER OF GRAVITY EMB-145 LR MODEL - TAKEOFF WITH FLAPS 9° APPLICABLE TO AIRPLANES PRE-MOD. SB 145-53-0068. MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 48722 lb...
  • Page 107 LIMITATIONS AIRPLANE EMB-145 LR FAA OPERATIONS MANUAL APPLICABLE TO AIRPLANES POST-MOD. SB 145-53-0068 OR EQUIPPED WITH AN EQUIVALENT MODIFICATION FACTORY INCORPORATED. MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 50044 lb 49823 lb 43651 lb...
  • Page 108 LIMITATIONS AIRPLANE EMB-145 LR FAA OPERATIONS MANUAL EMB-145 LR MODEL - TAKEOFF WITH FLAPS 22° APPLICABLE TO AIRPLANES PRE-MOD. SB 145-53-0068. MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 48722 lb 48501 lb 42549 lb...
  • Page 109 LIMITATIONS AIRPLANE EMB-145 LR FAA OPERATIONS MANUAL APPLICABLE TO AIRPLANES POST-MOD. SB 145-53-0068 OR EQUIPPED WITH AN EQUIVALENT MODIFICATION FACTORY INCORPORATED. MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 50044 lb 49823 lb 43651 lb...
  • Page 110 LIMITATIONS AIRPLANE EMB-145 LR FAA OPERATIONS MANUAL To comply with the performance and operating limitations of the regulations, the maximum allowable takeoff and landing operational weights may be equal to, but not greater than, the design limits. The takeoff weight (weight at brake release or at start of takeoff run) is the lowest among MTOW and the following weights: −...
  • Page 111 LIMITATIONS AIRPLANE EMB-145 LR FAA OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-01-05 REVISION 31...
  • Page 112 LIMITATIONS AIRPLANE EMB-145 MP FAA OPERATIONS MANUAL WEIGHT AND CENTER OF GRAVITY EMB-145 MP MODEL - TAKEOFF WITH FLAPS 9° MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 46495 lb 46275 lb 42549 lb 39462 lb...
  • Page 113 LIMITATIONS AIRPLANE EMB-145 MP FAA OPERATIONS MANUAL EMB-145 MP MODEL - TAKEOFF WITH FLAPS 22° MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 46495 lb 46275 lb 42549 lb 39462 lb 50000 39.5%...
  • Page 114 LIMITATIONS AIRPLANE EMB-145 MP FAA OPERATIONS MANUAL To comply with the performance and operating limitations of the regulations, the maximum allowable takeoff and landing operational weights may be equal to, but not greater than, the design limits. The takeoff weight (weight at brake release or at start of takeoff run) is the lowest among MTOW and the following weights: −...
  • Page 115 LIMITATIONS AIRPLANE EMB-145 MP FAA OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-01-05 REVISION 26...
  • Page 116 LIMITATIONS AIRPLANE EMB-145 EP FAA OPERATIONS MANUAL WEIGHT AND CENTER OF GRAVITY EMB-145 EP MODEL - TAKEOFF WITH FLAPS 9° APPLICABLE TO AIRPLANES PRE-MOD. SB 145-53-0064. MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 46495 lb...
  • Page 117 LIMITATIONS AIRPLANE EMB-145 EP FAA OPERATIONS MANUAL APPLICABLE TO AIRPLANES POST-MOD. SB 145-53-0064 OR EQUIPPED WITH AN EQUIVALENT MODIFICATION FACTORY INCORPORATED. MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 46495 lb 46275 lb 41226 lb...
  • Page 118 LIMITATIONS AIRPLANE EMB-145 EP FAA OPERATIONS MANUAL EMB-145 EP MODEL - TAKEOFF WITH FLAPS 22° APPLICABLE TO AIRPLANES PRE-MOD. SB 145-53-0064. MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 46495 lb 46275 lb 41226 lb...
  • Page 119 LIMITATIONS AIRPLANE EMB-145 EP FAA OPERATIONS MANUAL APPLICABLE TO AIRPLANES POST-MOD. SB 145-53-0064 OR EQUIPPED WITH AN EQUIVALENT MODIFICATION FACTORY INCORPORATED. MAXIMUM WEIGHT Max. Ramp Max. Takeoff Max. Landing Max. Zero Fuel Weight (MRW) Weight (MTOW) Weight (MLW) Weight (MZFW) 46495 lb 46275 lb 41226 lb...
  • Page 120 LIMITATIONS AIRPLANE EMB-145 EP FAA OPERATIONS MANUAL To comply with the performance and operating limitations of the regulations, the maximum allowable takeoff and landing operational weights may be equal to, but not greater than, the design limits. The takeoff weight (weight at brake release or at start of takeoff run) is the lowest among MTOW and the following weights: −...
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  • Page 122: Operational Limitations

    - Total Air Temperature in cruise flight above 25000 ft is limited to -45°C. However, if momentary deviations happen to temperature up to -50°C, no maintenance action is required. Page Code 1-01-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 123 LIMITATIONS AIRPLANE OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-01-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 124 COMBINATION WITH LARGE CHANGES IN PITCH, ROLL, OR YAW (E.G.LARGE SIDE SLIP ANGLES) MAY RESULT IN STRUCTURAL FAILURES AT ANY SPEED, EVEN BELOW V A Page Code 1-01-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 125 200 210 220 230 240 250 260 270 280 290 300 310 320 330 340 350 AIRSPEED - KIAS NOTE: The V may not be deliberated exceeded in any regime of flight (climb, cruise, or descent). Page Code 1-01-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 126 200 210 220 230 240 250 260 270 280 290 300 310 320 330 340 350 AIRSPEED - KIAS NOTE: The V may not be deliberated exceeded in any regime of flight (climb, cruise, or descent). Page Code 1-01-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 127 MAXIMUM FLAP EXTENDED ALTITUDE Maximum Altitude for Flap Extension ......20000 ft PITCH TRIM Maximum Airspeed after Takeoff/During Climb without Retrimming..........160 KIAS Page Code 1-01-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 128 Wet runway.............. 30 kt Runway with Compacted Snow....... 25 kt Runway with Standing Water/Slush/Dry Snow..20 kt Runway with Ice (no melting) ........10 kt Page Code 1-01-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 129 FLAPS UP (9°,18°, 22° and 45°) Positive 2.50 g 2.00 g Negative -1.00 g RUNWAY Runway Slope ............... -2% TO +2% Runway Surface Type........... PAVED Page Code 1-01-10 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 130: Supplementary Operational Limitations

    AIRPLANE LIMITATIONS ANAC/FAA OPERATIONS MANUAL SUPPLEMENTARY OPERATIONAL LIMITATIONS OPERATIONAL ENVELOPE APPLICABLE ONLY TO EMB-145ER, EP, EU AND MP MODELS POST-MOD. 145-00-0031 EQUIPPED WITH EQUIVALENT MODIFICATION FACTORY INCORPORATED 40000 -65°C -21.5°C 37000 ft 35000 30000 25000 ISA + 35°C 20000 15000 10000 8500 ft 5000...
  • Page 131 LIMITATIONS AIRPLANE ANAC/FAA OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-01-12 REVISION 36...
  • Page 132 (Refer to AMM Task 5-50-02). Minimum Total Air Temperature in cruise flight above 25000 ft is -45°C. Only APU T-62T-40C14 is allowed for operations on ground above 8000 ft. Page Code 1-01-12 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 133 AIRPLANE LIMITATIONS OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-01-12 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 134 200 ft above or below Sea Level (not applicable to EGPWS software version 216 and on with FMS Honeywell or FMS Universal Post Mod.SB145-34-0112). Page Code 1-01-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 135 MFD 2 terrain information. If the terrain picture bus fail is not annunciated (TERR amber annunciation), the MFD 2 must be used as terrain picture reference. Page Code 1-01-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 136: Electrical

    LIMITATIONS AIRPLANE OPERATIONS MANUAL ELECTRICAL Maximum Load on Main Generator ......400 A Maximum Load on APU Generator: Up to 30000 ft ............400 A Above 30000 ft............300 A Maximum Battery Temperature ........70°C Page Code 1-01-32 SEPTEMBER 20, 1999...
  • Page 137 LIMITATIONS AIRPLANE OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-01-32 SEPTEMBER 20, 1999...

  • Page 138: Fuel

    FCOC must be above 4°C. If this condition is satisfied, the caution message “E1(2) LO TEMP” is not presented (refer to FUEL LOW TEMPERATURE Procedure). Page Code 1-01-36 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 139 LIMITATIONS AIRPLANE OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-01-36 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 140 FCOC must be above 4°C. If this condition is satisfied, the caution message “E1(2) LO TEMP” is not presented (refer to FUEL LOW TEMPERATURE Procedure). Page Code 1-01-36 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 141 LIMITATIONS AIRPLANE OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-01-36 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 142: Apu

    LIMITATIONS AIRPLANE OPERATIONS MANUAL AUXILIARY POWER UNIT OPERATIONAL LIMITS APU Model T-62T-40C11 T-62T-40C14 PARAMETER TEMPERATURE (3) 54°C ALTITUDE FOR START 25000 ft or 30000 ft (2) 30000 ft OPERATION ALTITUDE 37000 ft 37000 ft ROTOR SPEED 108% 108% (5) EGT: START 884°C (1) 884°C...
  • Page 143 LIMITATIONS AIRPLANE OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-01-38 REVISION 39...

  • Page 144: Powerplant

    102.5%. 3) For airplanes Post-Mod. SB 145-77-0004 the N2 limit is 105.0%. 4) Takeoff thrust is time limited to 5 minutes. CONTINUES ON NEXT PAGE Page Code 1-01-40 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 145 Vibration in any flight phase in the amber range up to 1.5 IPS for less than 30 seconds does not require maintenance action. Page Code 1-01-40 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 146 Do not attempt a go-around procedure after deployment of the thrust reversers following a landing. Selection of thrust reversers in flight or their preselection before touchdown is prohibited. Page Code 1-01-40 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 147 Airplanes equipped with FADEC software version B5.1.1 must decrease the Approach Climb Gradient by 1% and decrease the Approach Climb Limited Weight by 1920 lb. Page Code 1-01-40 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 148: Pressurization

    LIMITATIONS AIRPLANE OPERATIONS MANUAL PNEUMATIC, CONDITIONING PRESSURIZATION PRESSURIZATION Maximum differential pressure........7.8 psi Maximum differential overpressure....... 8.1 psi Maximum differential negative pressure ....... -0.3 psi Page Code 1-01-48 SEPTEMBER 20, 1999...
  • Page 149 LIMITATIONS AIRPLANE OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-01-48 SEPTEMBER 20, 1999...

  • Page 150: Ice And Rain Protection

    LIMITATIONS AIRPLANE OPERATIONS MANUAL ICE AND RAIN PROTECTION OPERATION IN ICING CONDITIONS Maximum Temperature for Anti-icing Operation ....10°C Minimum Temperature for Manual Anti-Icing Operation ..-40°C Single engine or single bleed maximum altitude operation in icing conditions ..............15000 ft Holding configuration: Landing Gear..............UP Flaps.................UP Minimum Airspeed ............200 KIAS...
  • Page 151 LIMITATIONS AIRPLANE OPERATIONS MANUAL WINDSHIELD WIPER OPERATION Maximum Airspeed for Windshield Wiper Operation ..170 KIAS Page Code 1-01-50 REVISION 24...

  • Page 152: Ozone Concentration

    LIMITATIONS AIRPLANE OPERATIONS MANUAL OZONE CONCENTRATION The tables below show the airplane altitude limitations due to ozone concentration in atmosphere. NOTE: - These tables are based on FAA ADVISORY CIRCULAR 120.38. - The tables show altitude limitations calculated for constant ozone concentration, cabin stabilized at 8000 ft, and both recirculation fans turned on.
  • Page 153 LIMITATIONS AIRPLANE OPERATIONS MANUAL NORTH AMERICA - MAXIMUM OZONE CRITERIA FLIGHT LEVEL LATITUDE 80°N 75°N 70°N 65°N 360 340 330 330 340 330 330 330 330 340 350 60°N 360 350 340 340 330 330 340 330 350 350 55°N 360 350 350 340 340 340 340 350 50°N 360 340 350 340 350...
  • Page 154 LIMITATIONS AIRPLANE OPERATIONS MANUAL NORTH AMERICA - TWA OZONE CRITERIA NOTE: Values below are the altitude limitations in which the airplane is allowed to fly more than 3 continuous hours. FLIGHT LEVEL LATITUDE 80°N 75°N 70°N 65°N 320 310 310 270 310 290 300 270 270 270 310 290 60°N 330 310 310 290 310 300 290 270 270 270 310 290 55°N...
  • Page 155 LIMITATIONS AIRPLANE OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-01-52 SEPTEMBER 20, 1999...
  • Page 156 LIMITATIONS AIRPLANE OPERATIONS MANUAL NAVIGATION EQUIPMENT RADAR Do not operate weather radar during refueling, near fuel spills or people. ATTITUDE AND HEADING REFERENCE SYSTEM Airplane must not be moved until all attitude and heading information presented on PFD is valid. For the AH-900 AHRS version the following limits are applicable: - Maximum latitude for alignment..
  • Page 157 LIMITATIONS AIRPLANE OPERATIONS MANUAL - The airplanes may not be operated within the following North and South magnetic polar cut-out regions: MAGNETIC CUT-OUT LATITUDE LONGITUDE REGIONS Between 70°N and Between 80°W and 82°N 135°W North North of 82°N Between 0° and 180°W/E Between 60°S and Between 118°30’E and 82°S...
  • Page 158 LIMITATIONS AIRPLANE OPERATIONS MANUAL COMMUNICATION EQUIPMENT Do not rely on ADF indications shown on PFD while transmitting in Do not transmit through HF Radio during airplane fueling. TRANSPONDER MODE S ENHANCED SURVEILLANCE For airplanes Post-Mod. SB 145-34-0096 or equipped with an equivalent modification factory incorporated, the installed Mode S system satisfies the data requirements of ICAO Doc 7030/4, Regional Supplementary Procedures for SSR Mode S Enhanced Surveillance in...
  • Page 159 LIMITATIONS AIRPLANE OPERATIONS MANUAL AUTOPILOT (APPLICABLE TO EMB-145 XR MODEL ONLY) The following limitations are applicable to the Autopilot: − Minimum Decision Altitude During ILS Approach..200 ft AGL − Minimum Engagement Height After Takeoff ..500 ft − Minimum Use Height ..........160 ft −...
  • Page 160 LIMITATIONS AIRPLANE OPERATIONS MANUAL NAVIGATION EQUIPMENT RADAR Do not operate weather radar during refueling, near fuel spills or people. ATTITUDE AND HEADING REFERENCE SYSTEM Airplane must not be moved until all attitude and heading information presented on PFD is valid. For the AH-900 AHRS version the following limits are applicable: −...
  • Page 161 LIMITATIONS AIRPLANE OPERATIONS MANUAL − The airplanes may not be operated within the following North and South magnetic polar cut-out regions: MAGNETIC CUT-OUT LATITUDE LONGITUDE REGIONS Between 70°N and Between 80°W and 82°N 135°W North North of 82°N Between 0° and 180°W/E Between 60°S and Between 118°30’E and...
  • Page 162 LIMITATIONS AIRPLANE OPERATIONS MANUAL − The airplanes may not be operated within the following North and South magnetic polar cut-out regions: MAGNETIC CUT-OUT LATITUDE LONGITUDE REGIONS Between 70°N and Between 90°W and 82°N 120°W North North of 82°N Between 0° and 180°W/E Between 60°S and Between 120°E and 82°S...
  • Page 163 LIMITATIONS AIRPLANE OPERATIONS MANUAL COMMUNICATION EQUIPMENT − Do not rely on ADF indications shown on PFD while transmitting in − Do not transmit through HF Radio during airplane fueling. TRANSPONDER MODE S ENHANCED SURVEILLANCE For airplanes Post-Mod. SB 145-34-0096 or equipped with an equivalent modification factory incorporated, the installed Mode S system satisfies the data requirements of ICAO Doc 7030/4, Regional Supplementary Procedures for SSR Mode S Enhanced Surveillance in...

  • Page 164: Fms

    AIRPLANE LIMITATIONS OPERATIONS MANUAL FMZ2000 FLIGHT MANAGEMENT SYSTEM The following limitations are applicable to the FMS: The Honeywell Flight Management System (FMS) Pilot's Operating Manual, Honeywell Publication Number A28-1146-122-00, August 1997 edition (or later revision of the manual) for the software version NZ4.8, Honeywell Publication Number A28-1146-133-00, February 1999 edition (or later revision of the manual) for the software version NZ5.2 or FAA accepted Operating Manual, must...
  • Page 165 LIMITATIONS AIRPLANE OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE When using FMS guidance for conducting instrument approach procedures that do not include a GPS reference in the title of the published procedure, the flight crew must verify that the procedure specified navaid and associated avionics are operational. For airplanes equipped with single FMS, when using FMS guidance for conducting instrument approach procedures, the procedure navaid must be tuned and valid, and the raw data must be...
  • Page 166 AIRPLANE LIMITATIONS OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE The FMS is approved for those oceanic and North Atlantic (NAT) Minimum Navigation Performance Specification (MNPS) routes requiring only a single FMS and a single GPS in accordance with AC 20-130A. The pilot must check for leg gaps in the Flight Plan Display on EFIS and input waypoints to fill in any gaps as necessary.
  • Page 167 LIMITATIONS AIRPLANE OPERATIONS MANUAL NAVIGATION OPERATIONAL APPROVALS The single Honeywell FMZ2000 Flight Management System, with the software version NZ4.8 Mod A or Mod C, and the single or dual Honeywell FMZ2000 Flight Management System software version NZ5.2 Mod B, Mod C, Mod D and Mod E have been demonstrated capable of and have been shown to meet the requirements for the following operations: OCEANIC AND REMOTE...
  • Page 168 AIRPLANE LIMITATIONS OPERATIONS MANUAL RNP-10 - REQUIRED NAVIGATION PERFORMANCE − The dual FMZ2000 installation with dual Global Positioning System (GPS) sensors as installed has been found to comply with the requirements of FAA Order 8400.12A, as amended, as a primary means of navigation with no time limitation, when used in conjunction with Honeywell Off Line RAIM prediction program.
  • Page 169 LIMITATIONS AIRPLANE OPERATIONS MANUAL NON-PRECISION APPROACH In accordance with AC 20-130A, TSO C129a C1 and AC 90-94 (Phase II and III overlay approaches and GPS only approaches), provided: − The APP annunciation is set on the PFD at the Final Approach Fix. −...
  • Page 170 LIMITATIONS AIRPLANE OPERATIONS MANUAL UNS-1K FLIGHT MANAGEMENT SYSTEM The Universal UNS1 Operator’s Manual or an Operating Manual accepted by the Certification Authority must be immediately available to the flight crew whenever navigation is predicated on the use of FMS. The software status stated in the Operator’s Manual must match that displayed on the FMS Control Display Unit (CDU).
  • Page 171 LIMITATIONS AIRPLANE OPERATIONS MANUAL For airplanes equipped with single FMS, when using FMS guidance for conducting instrument approach procedures, the procedure navaid must be tuned and valid, and the raw data must be displayed in the cockpit, under the following conditions: For VOR approaches (where the procedure specified navaid is a VOR only navaid no-DME capability) and NDB approaches, without GPS (GPS failed or RAIM out of limits or unavailable).
  • Page 172 LIMITATIONS AIRPLANE OPERATIONS MANUAL Coupled FMS vertical guidance is not available. Therefore, during FMS operation with Autopilot coupled, the pilot must use the Flight Guidance Controller for vertical control. Advisory vertical guidance is available only in descent. During oceanic, North Atlantic (NAT) Minimum Performance Specification (MNPS), enroute and terminal area operation with DR annunciated on the PFD, the flight crew must verify the FMS position using VOR/DME raw data or other appropriate means.
  • Page 173 LIMITATIONS AIRPLANE OPERATIONS MANUAL NAVIGATION OPERATIONAL APPROVALS The Universal UNS-1K Flight Management System, with the version 603.X software, has been demonstrated capable of and has been shown to meet the requirements for the following operations: Oceanic and Remote - In accordance with AC 20-130A, along routes requiring a Long Range Navigation (LRN) System, provided it is receiving usable signals from the GPS which meets requirements of AC 90-94 for use as the only LRN...

  • Page 174: Doors

    LIMITATIONS AIRPLANE OPERATIONS MANUAL DOORS COCKPIT SECURITY DOOR On airplanes equipped with a cockpit security door, two crewmembers must be in the cockpit during all flight phases. If one of the pilots leaves the flight deck, he must be replaced in the cockpit by another crewmember.
  • Page 175 LIMITATIONS AIRPLANE OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-01-70 REVISION 25...
  • Page 176 LIMITATIONS AIRPLANE OPERATIONS MANUAL CAT II OPERATION WITH PRIMUS 1000 AUTOMATIC FLIGHT CONTROL SYSTEM MINIMUM EQUIPMENT REQUIRED The performance of Category II approaches requires that the following equipment and instruments be in proper operating conditions: 2 Attitude and Heading Reference Systems; 1 Yaw Damper System;...
  • Page 177 LIMITATIONS AIRPLANE OPERATIONS MANUAL AUTOPILOT SYSTEM Minimum Decision Height (DH)..........100 ft NOTE: Although the radio altitude setting may be adjusted down to 80 ft, if requested by an ILS Cat II Approved Chart, the Decision Height (DH) is limited to 100 ft above ground level. Minimum Use Height (MUH) ...........
  • Page 178 Headwind..............25 kt Tailwind..............10 kt Crosswind ..............11 kt NOTE: The maximum wind limits listed above include gusts. Page Code 1-01-82 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 179 With the HGS Combiner deployed, airplane sun visors must not be placed in a position, during takeoff, approach or landing, that will prevent the correct operation of the forward fly-away movement of the Combiner. Page Code 1-01-82 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 180 Rain Repellent Coating replace Windshield Wipers. Approved Rain Repellent Coatings are listed in AMM chapter 30-41-04. 2 Primary Flight Displays (PFD). − Page Code 1-01-82 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 181 NOTE: GPS is not required in case of dual IRS configuration. APPROACH AND LANDING FLAPS AIII mode approaches and landings must be performed with flaps 22°. Page Code 1-01-82 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 182 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL SECTION 1-02 NORMAL PROCEDURES TABLE OF CONTENTS Page Block Introduction .................1-02-00 Checklist ..................1-02-01 Normal Procedures External Safety Inspection.............1-02-05 Internal Safety Inspection ............1-02-09 Power Up ................1-02-13 Before Start - First Flight ............1-02-17 Before Start - Through Flight ..........1-02-21 Engine Start................1-02-23 After Start................1-02-29 Before Takeoff ...............1-02-33...
  • Page 183 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Supplementary Procedures Page Block Fuel Crossfeed Operation ............. 1-02-78 Environmental Operation in Icing Conditions........1-02-79 Turbulent Air Penetration ..........1-02-79 Volcanic Ash ..............1-02-79 Lightning Strike ............. 1-02-79 Pressurization in Manual Mode........1-02-79 Navigation Flight Management System .......... 1-02-80 RVSM Operation ............

  • Page 184: Introduction

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL INTRODUCTION The operating procedures defined in this section have been defined with the purpose of providing expanded normal procedures that should be used by trained flight crew to ensure that the airplane is in a proper condition and correctly configured for each phase of flight.
  • Page 185 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-02-00 REVISION 37...

  • Page 186: Checklist

    Avionics Master 1 or 2.. PUSHED IN Autopilot .......CKD ∗ Batteries Voltage..CKD Gust Lock.....LOCKED ∗ Backup Battery Reversionary Panel ..SET ♦ Flight Instruments..SET/X-CKD (EMB XR only) ..CKD Page Code 1-02-01 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 187 GPU/APU ....OFF AIR COND/PNEUM Panel SET Fuel Pumps ....OFF Altimeters ....SET/X-CKD Batteries ...... OFF Pressurization....CKD ♦ ON THROUGH FLIGHTS APU......AS RQRD CHECKLITS. Page Code 1-02-01 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 188: Normal Procedures

    Access Doors and Panels..........SECURED Static Ports..............NO OBSTRUCTION Sensors and Pitot Tubes ..........CONDITION, OBSTRUCTION Windshield Wipers (or Rain Repellent Coating) ... CONDITION Air Inlets ................ NO OBSTRUCTION Page Code 1-02-05 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 189 Emergency Lights ............CONDITION Wing Leading Edge............CONDITION Access Doors and Panels ..........SECURED Direct Measuring Sticks ..........PUSHED IN Air Inlets, Outlets and Vents.......... NO OBSTRUCTION Page Code 1-02-05 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 190 Logo Lights ..............CONDITION Flight Control Surfaces ..........CONDITION Static Dischargers............NUMBER AND CONDITION APU................CONDITION Pressurization Static Ports..........NO OBSTRUCTION Baggage Door............... LATCHED/ LOCK PANEL CLOSED Code Page 1-02-05 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 191 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-02-05 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 192: Internal Safety Inspection

    F/O seat. If any CB is pulled verify the reason for it and if there is any operational implication advise the other pilot. Page Code 1-02-09 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 193 Ignitions..............AUTO Start/Stop Selectors ..........STOP Fire Extinguishing Handle 2........IN Ailerons & Rudders Shutoff ........IN Engine Pump Shutoff ..........GUARDED Electric Hydraulic Pumps......... OFF Page Code 1-02-09 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 194 To release the parking brake, first press the brake pedals to full deflection then release the emergency/parking brake handle. Page Code 1-02-09 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 195 This procedure must be carried out with gear pins in place. Page Code 1-02-09 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 196: Power Up

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL POWER UP APU START RECOMMENDATIONS For APU start and operation the following is recommended: Starting cycle: After First Attempt..........60 SECONDS OFF After Second Attempt...........60 SECONDS OFF After Third Attempt..........30 MINUTES OFF In case of an unsuccessful APU start or if BATT 1 OFF BUS followed by APU GEN OFF BUS messages are displayed on EICAS, the APU master switch must be set to OFF position and time intervals as stated above shall be observed before the next start attempt.
  • Page 197 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL APU START WITH BATTERIES Internal Safety Inspection ..........COMPLETED Batteries 1 & 2............... AUTO Immediately after the batteries are switched ON the aural message “AURAL UNIT OK” can be heard. Avionics Master 1 or 2 ..........ON Batteries Voltage ............
  • Page 198 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Fire Detection ............... CHECKED Press and hold (for at least 2 seconds) the Fire Detection Test button while observing the following events: EICAS messages: Warning: APU FIRE, ENG 1 (2) FIRE, BAGG SMOKE (*) Caution: APU FIREDET FAIL, E1 (2) FIREDET FAIL (*) for class C compartment only.
  • Page 199 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL APU Bleed..............OPEN Air Conditioning............. AS REQUIRED Should it be necessary to climatize the airplane: - Both Packs ON; - XBLEED to OPEN; - Set both temperature controls to AUTO. If control of the Pack 2 by the cabin attendant is desired, select the corresponding knob to ATTD.
  • Page 200 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL APU START WITH GPU Internal Safety Inspection ..........COMPLETED Batteries 1 & 2 .............. AUTO Immediately after the batteries are switched ON the aural message “AURAL UNIT OK” can be heard. Avionics Master 1 or 2 ..........ON Batteries Voltage............
  • Page 201 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Fire Extinguisher handles illuminated. BAGG EXTG button illuminated (applies to airplane with baggage hold extinguishing only). Aural fire warning. APU Master..............ON/WAIT 3 SECONDS/ START/THEN ON Turn the knob to ON, wait 3 seconds, and then momentarily to START.
  • Page 202 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL GPU POWER (NO APU) Internal Safety Inspection ..........COMPLETED Batteries 1 and 2 ............AUTO Immediately after the batteries are switched ON the aural message ”AURAL UNIT OK” can be heard. Avionics Master 1 or 2 ..........ON Batteries Voltage ............
  • Page 203 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-02-13 REVISION 37...

  • Page 204: Before Start - First Flight

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL BEFORE START - FIRST FLIGHT begin cockpit preparation EXTERNAL SAFETY INSPECTION and the INTERNAL SAFETY INSPECTION must have been completed and the airplane must be powered up. Airplane Manual & Documents ........ON BOARD Check the local regulations and company policy for the required on- board operational documents.
  • Page 205 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL - Select HOT MIC on the control wheel communication switch; - Actuate the test button on the mask stowage location. Check that the blinker changes color; (*) - The OXY ON flag must appear on the stowage box; (*) - For EROS masks: While maintaining the RESET TEST lever (TEST/SHUTOFF sliding control) depressed, check that the blinker changes color momentarily, and then depress the...
  • Page 206 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL CVR ................CHECKED Press the CVR TEST button and check the STATUS LED illuminated for about one second. Batteries 1 & 2 ............AUTO Immediately after the batteries are switched ON the aural message ”AURAL UNIT OK” can be heard. Electrical Panel ............SET Check if: All four generator buttons and the APU generator button are...
  • Page 207 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Fuel System ............... SET Select the fuel pumps according to the alternating policy in use. If the APU is running, feed it from the tank that has more fuel. Reset the used fuel readout on the MFD. PC Power System (if installed) ........
  • Page 208 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL APU CONTROL Panel..........CHECK APU MASTER Selector........AS REQUIRED APU FUEL SHUTOFF Button ......OFF - Verify APU FUEL SHUTOFF Button OFF, guarded and no striped bars illuminated. Ignition ................ AUTO Verify both switches set to AUTO. Takeoff Data ...............
  • Page 209 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL The ERJ145/135 anti-ice system is such that if any ice is detected at a speed above 25 Kt the whole ice protection system goes ON. If chances are that ice will be encountered during takeoff then REF A/ICE must be set to ON so that the FADEC allows a ITT margin for the anti-ice ON condition.
  • Page 210 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Air Conditioning ............AS REQUIRED If air conditioning is desired and if the APU has been running for more than 3 minutes (5 minutes is preferable) open the CROSSBLEED and select both PACKS to OPEN. The recirculation fans (RECIRC button) must be ON.
  • Page 211 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL AHRS ................SET AH-800 AHRS: both pilots must check if the respective AHRS is set to SLVD. AH-900 AHRS: enter the present position through the FMS CDU. Flight Guidance Controller .......... SET Autopilot ..............CHECKED The crew assigned for the flight must carry out the AUTOPILOT check as follows: - Release the GUST LOCK, bring the control column to its...
  • Page 212 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL Flight Instruments ............SET & X-CHECKED Both pilots must set their respective altimeters to the local QNH. They must also select an initial course as per the expected departure procedure. The CPT must also set the HDG bug according to the intended runway heading.
  • Page 213 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Verify if the ATC/TCAS window is in SBY. Select the ABOVE function. Test the TCAS by placing the yellow cursor box over the code. Press the RMU test button for 5 to 7 seconds until the test OK message on the RMU and "TCAS TEST, PASSED"...
  • Page 214 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL BACK-UP TUNING (if installed) ........SET Set to NORMAL and copying RMU2. COMM 3 (if installed) ............ SET Press the transfer button in case of an error message on the radio display. Pressurization ............... SET Set the system to the destination airport elevation and verify that the DUMP and AUTOMAN switches are guarded and were not pushed (if they have been pushed the white mark on the buttons...
  • Page 215 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL HF (if installed) .............. SET Pitch Trim ..............SET/ZERO/ ZERO Pitch Trim must be set as per the CG position stated in the weight and balance sheet. Doors & Windows ............CLOSED Both pilots must verify that their respective cockpit window is closed and the RSP should select MFD T/O page to check all airplane doors closed indications.
  • Page 216 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL BEFORE START - FIRST FLIGHT begin cockpit preparation EXTERNAL SAFETY INSPECTION and the INTERNAL SAFETY INSPECTION must have been completed and the airplane must be powered up. Airplane Manual & Documents ........ON BOARD Check the local regulations and company policy for the required on- board operational documents.
  • Page 217 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL - Select HOT MIC on the control wheel communication switch; - Actuate the test button on the mask stowage location. Check that the blinker changes color; - The OXY ON flag must appear on the stowage box; - For EROS masks: While maintaining the RESET TEST lever (TEST/SHUTOFF sliding control) depressed, check that the blinker changes color momentarily, and then depress the...
  • Page 218 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL CVR ................CHECKED Press the CVR TEST button and check the STATUS LED illuminated for about one second. Batteries 1 & 2 ............AUTO Immediately after the batteries are switched ON the aural message ”AURAL UNIT OK” can be heard. Electrical Panel ............SET Check if: All four generator buttons and the APU generator button are...
  • Page 219 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Fuel System ............... SET Select the fuel pumps according to the alternating policy in use. If the APU is running, feed it from the tank that has more fuel. Reset the used fuel readout on the MFD. PC Power System (if installed) ........
  • Page 220 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL FIRE EXTINGUISHER Panel ........CHECK APU fire extinguishing Button OFF and no lights. BAGG fire extinguishing Button OFF and no lights. APU CONTROL Panel..........CHECK APU MASTER Selector........AS REQUIRED APU FUEL SHUTOFF Button ......OFF Verify APU FUEL SHUTOFF Button OFF, guarded and no striped bars illuminated.
  • Page 221 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL The ERJ145/135 anti-ice system is such that if any ice is detected at a speed above 25 Kt the whole ice protection system goes ON. If chances are that ice will be encountered during takeoff then REF A/ICE must be set to ON so that the FADEC allows a ITT margin for the anti-ice ON condition.
  • Page 222 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Air Conditioning ............AS REQUIRED If air conditioning is desired and if the APU has been running for more than 3 minutes (5 minutes is preferable) open the CROSSBLEED and select both PACKS to OPEN. The recirculation fans (RECIRC button) must be ON.
  • Page 223 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Flight Number & Clocks ..........SET The crew must enter the flight number into the appropriate place in the clock at his side. AHRS (if installed)............SET AH-800 AHRS: both pilots must check if the respective AHRS is set to SLVD.
  • Page 224 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL DIGITAL AUDIO Panel ..........AS REQUIRED Select the microphone and audio reception buttons as required and adjust the volume levels. Reversionary Panels........... NORMAL Both pilots must check that their respective MFD Selector Knobs are set to NORM. Flight Instruments ............
  • Page 225 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Standby Instruments ............. SET Conventional Standby Instruments: Uncage the STANDBY ATTITUDE indicator, if it is caged, and observe that the red flag is removed and the horizon is steady. Compare its indication with the main attitude indicators. Set the QNH and compare its readout with one of the main altitude tapes.
  • Page 226 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL Thrust Levers..............IDLE Stall Protection System..........CHECKED The AHRS/IRS should be aligned. CUTOUT 1 and 2 buttons must be guarded and not illuminated and QUICK DISCONNECT BUTTON must be released. Carry out the Stall Protection System test as follows: - Pull the control column all the way back and momentarily press the SPS TEST button (the TEST button must not be kept pressed beyond the shaker actuation).
  • Page 227 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL FMS................SET The PF assigned for the flight must enter all the data that does not depend on the final ship papers. So the FMS initialization including the check if the DATABANK is still valid, check for correct date and time and check for possible messages related to the status of the FMS.
  • Page 228 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Doors & Windows ............CLOSED Both pilots must verify that their respective cockpit window is closed and the RSP should select MFD T/O page to check all airplane doors closed indications. Check the cockpit door securely closed. Both pilots should select TCAS page on MFD for takeoff.
  • Page 229 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Safety Pins ..............ON BOARD Verify that the safety pins are on board, behind the CPT seat. Locking Pins (if applicable) ........... ON BOARD Verify that the locking pins are on board, behind the CPT seat. Page Code 1-02-17...

  • Page 230: Before Start - Through Flight

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL BEFORE START - THROUGH FLIGHT Fuel System and Quantity ..........CHECKED lb/kg The CPT must alternate the fuel pumps, reset the used fuel reading and check the fuel on board is not less than the required fuel for the next flight.
  • Page 231 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL HGS Combiner (if applicable) ........SET Lower the combiner to its operating position and check to verify that symbology is displayed. Following the combiner check, it may be stowed or the symbology may be cleared if not desired during any remaining pre-flight or taxi-out.
  • Page 232 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL Once these actions are completed, the pilots must carry out an instrument crosscheck as follows: Both AIRSPEED TAPES not showing speed; EADI’s level and flag-free; Both ALTIMETERS with their QNH set, and reading consistent altitudes; Both VERTICAL SPEED INDICATORS showing zero;...
  • Page 233 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL HGS Control Panel (if applicable) ......... SET Enter runway length and TDZE for possible return for landing. Enter glideslope angle for the expected runway. Select or verify the primary (PRI) mode on the HCP. Pressurization ............... SET Select the elevation of the destination airport.
  • Page 234 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Pitch Trim..............SET/ZERO/ ZERO Pitch Trim must be set as per the CG position stated in the weight and balance sheet. Doors & Windows ............CLOSED Both pilots must verify that their respective cockpit window is closed and the RSP should select MFD T/O page to check all airplane doors closed indications.
  • Page 235 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Steering................. AS REQUIRED Push-back required: DISENGAGE pressing the trigger on the yoke and observe STEERING INOP message on EICAS. No push-back required or after push-back: ENGAGE pressing STEERING HANDWELL and observe STEERING INOP message disappear on EICAS. NOTE: Steering handle actuation with nose wheels beyond their operational limits may cause damage to the nose wheel steering system.

  • Page 236: Engine Start

    However, a dry motoring procedure must not be performed if one of the FADECs is declared incapable. Page Code 1-02-23 TEMPORARY REVISION 41.1 Copyright © by Embraer. Refer to cover page for details.
  • Page 237 However, a dry motoring procedure must not be performed if one of the FADECs is declared incapable. Page Code 1-02-23 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 238 If any starting limit is exceeded prior to aborting a start, do not attempt further starts and report to the maintenance personnel. If a hung or no start occurs, accomplish the Dry Motoring Procedure before attempting another start. Page Code 1-02-23 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 239: After Start

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL AFTER START Ground Equipment............REMOVED Do not start taxiing before receiving confirmation from the ground crew that the airplane is free to taxi. Then acknowledge that and switch OFF the cockpit dome lights. It is recommended that the taxi light be ON during taxi even during daytime.
  • Page 240 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL AIR COND/PNEUMATIC Panel ........SET ENGINE ENGINE CONDITION CROSSBLEED MODE BLEED BLEED ALT T/O Open Closed Auto No icing T/O (1) Closed Open Open E T/O Closed Open Open ALT T/O Open Closed Auto Icing Open Closed Auto...

  • Page 241: Before Takeoff

    Briefings consisting of mechanical repetition of a memorized speech without having the mind set on the subject are useless. Cabin Crew ..............ADVISE Page Code 1-02-33 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 242 FD button and select GO AROUND by pressing the respective button at the thrust lever head. Check that the flight director bar on T/O mode became visible on the PFD. Page Code 1-02-33 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 243 Gust Lock Caution Lights remain blinking until unlocking cycle is completed. This cycle is completed with the gust lock lever at unlocked position (full forward). Page Code 1-02-33 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 244 (“Warm” Engine) ensure at least 2 minutes to warm-up before apply takeoff power. - To increase N2 above 83% the engine oil temperature must be at least 40°C. Page Code 1-02-33 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 245: Cleared Into Position

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL CLEARED INTO POSITION External Lights .............. ON The following lights must be turned on by the CPT prior to entering the runway: LDG 1, NOSE, LDG 2, TAXI (if not ON yet) and STROBE. It is advisable to have strobe lights ON whenever entering or crossing an active runway.
  • Page 246 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-02-37 REVISION 40...

  • Page 247: Takeoff

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL TAKEOFF (APPLICABLE TO ALL ENGINES EXCEPT AE3007A1P AND AE3007A1E) Thrust Levers ..............THRUST SET If an Alternate Takeoff Mode has been selected, check green ATTCS indication presented on EICAS. NOTE: - If the runway is considered to be limiting, a static takeoff must be accomplished.
  • Page 248 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL At level off height altitude: For takeoff with flaps 9°: At V + 15 KIAS or higher........FLAPS UP For takeoff with flaps 18°: At V + 10 KIAS or higher........FLAPS 9° At V + 30 KIAS or higher........FLAPS UP For takeoff with flaps 22°: At V + 5 KIAS or higher........FLAPS 9°...

  • Page 249: After Takeoff

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL AFTER TAKEOFF NOTE: Keep the airplane trimmed to avoid excessive loads on the Horizontal Stabilizer Actuator (HSA). The airplane should be trimmed before 160 KIAS. Failure to accomplish the above procedure may lead to an inoperative trim condition not associated with any EICAS message.
  • Page 250 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Air Conditioning............. SET Once CLB thrust is set the air conditioning should be set as follows: - If the takeoff was performed on APU BLEED then both engine BLEEDS must be selected to OPEN, the CROSS BLEED must be set to AUTO and the APU bleed must be CLOSED.

  • Page 251: Descent

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL DESCENT Windshield Heating............ON The system must be switched ON to prevent fog and ice formation on the windshield inner layer. Approach Briefing ............COMPLETED The crew must review the descent, approach and landing procedures. HGS Combiner (if installed)..........
  • Page 252 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Pressurization ............... CHECKED Verify that the digital controller was set to the destination airport elevation. BELOW 10000 FT External Lights .............. ON The following lights must be turned ON upon crossing 10000 ft: - LDG1, NOSE AND LDG2. During night time, the LOGO light must also be turned ON.

  • Page 253: Approach

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL APPROACH XFEED ................OFF PASS SIGNS Panel............SET AIR COND/PNEUMATIC Panel........SET Altimeters..............SET & XCHECKED When the altimeters are set to QNH (passing the Transition Level) the Approach Checklist should be called for, if it is a flight in ICAO airspace.
  • Page 254 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL The tables below shows the flap maneuvering speeds during a visual approach or during an instrument approach: ALL ENGINES EXCEPT EMB-145XR MODEL FLAP MANEUVERING SPEED (KIAS) BELOW MSLW* ABOVE MSLW* NO ICING WITH ICING NO ICING WITH ICING FLAPS GEAR CONDITIONS...
  • Page 255 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL NOTE: - The maximum flap 45° extended speed (V ) of 145 KIAS must not be exceeded in any condition. However, if momentary deviations happen to speeds up to 160 KIAS during transition to or flight with flaps 45°, no maintenance action is required.
  • Page 256 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL MISSED APPROACH Go Around Button ............PRESS Press the Go Around buttons at the thrust levers and check if Flight Director goes to pitch 10° nose up. Rotate or verify that autopilot rotates the airplane following the Flight Director. Thrust Levers ..............

  • Page 257: Before Landing

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL BEFORE LANDING Landing Gear ..............DOWN Command gear down and check whether the speed is within limits for landing gear extension. Also check the three green lights before this item is confirmed. Speed Brake ..............CLOSE Flaps ................
  • Page 258 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-02-61 REVISION 37...

  • Page 259: After Landing

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL AFTER LANDING Thrust Levers..............AS REQUIRED If taxi is not required, thrust levers should be set to idle. Brakes................AS REQUIRED Windshield Heating............AS REQUIRED Turn windshield heating OFF if it is not required to defog or de-ice the windshield.
  • Page 260 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Pitch Trim ..............SET Reset the PITCH TRIM back in the green range (approx. 7.0 UP). APU................AS REQUIRED If the intention is to start the APU, do it now. Do not use the APU BLEED until the airplane is parked and with blocks on (wait at least 3 minutes for use APU bleed).

  • Page 261: Shutdown

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL SHUTDOWN Thrust Levers..............IDLE Emergency/Parking Brake..........ON Typically when approaching the parking position and turning towards the marshal, turn OFF the taxi light. This is especially important during nighttime. Pull the Emergency/Parking Brake and twist it to the set position after airplane has stopped.
  • Page 262 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Start/Stop Selectors ..............STOP Once the Emergency/Parking Brake is applied, shut down the engines by selecting the engine start knobs to STOP. NOTE: - Associated engine BLEED must be CLOSED before selecting the engine START/STOP Selectors to STOP; - The engines will not shut down with START/STOP Selectors unless Thrust Levers are first moved to IDLE.
  • Page 263 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL PUMP PWR ..............AS REQUIRED If the APU is running, keep the right fuel pump ON (or the left pump ON and CROSSFEED open). If the APU is not running, turn both fuel pumps OFF. Elec.
  • Page 264 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-02-73 REVISION 37...

  • Page 265: Leaving The Airplane

    NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL LEAVING THE AIRPLANE Avionics Master 1 & 2 ..............OFF Select the AVIONICS MASTER 1 & 2 OFF prior to switching GPU or APU OFF. If the airplane is equipped with UNIVERSAL FMS installation, switch the FMS's OFF prior to switching OFF AVIONICS MASTER 1 &...
  • Page 266 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL GPU/APU ................OFF Shut APU down by pressing the STOP button on its panel. Verify the shutdown on the EICAS. Wait until APU rotation drops to 5% before switching APU MASTER OFF. NOTE: Do not close the air conditioning packs before shutting down the APU.
  • Page 267 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL LEAVING THE AIRPLANE IRS (If installed) ...............OFF The manual switching of the IRS ensures proper finalization of the IRS software. Wait a minimum of ten seconds before removing the input power. Avionics Master 1 & 2 ..............OFF Select the AVIONICS MASTER 1 &...
  • Page 268 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL Standby Attitude (if applicable) ..........CAGED Cage the standby horizon. Make sure it is caged by checking whether its red flag is visible. GPU/APU ................OFF Shut APU down by pressing the STOP button on its panel. Verify the shutdown on the EICAS.

  • Page 269: Crossfeed Operation

    SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS FUEL MANUAL CROSSFEED OPERATION NOTE: Crossfeed must be OFF during takeoff and landing. If fuel imbalance is verified: Attitude ..............WINGS LEVELED If left wing presents lower level: Crossfeed Selector ..........LOW1 If right wing presents lower level: Crossfeed Selector ..........
  • Page 270 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS FUEL MANUAL INTENTIONALLY BLANK Page Code 1-02-78 REVISION 33...

  • Page 271: Operation In Icing Conditions

    At the completion of the walk-around, if ice, snow or frost is discovered, de-icing, and possibly anti-icing will be required. The check for ice accumulation should be done in a well-lit area. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 272 Fuel Tank Vents ............CLEAR OF ICE OR SNOW Batteries ................ INSTALLED Certain temperatures require batteries removal to prevent cold soaking. Verify that batteries have been re-installed. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 273 The warm-up should be accomplished with all doors closed, if possible. Turn recirculation fans on. CONTINUES ON NEXT PAGE Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 274 OPERATIONS ENVIRONMENTAL MANUAL CONTINUED FROM PREVIOUS PAGE In very cold days, Embraer recommends a gradual warming of the cabin, as follows: - Set air conditioning control to manual mode; - Put the cockpit temperature selection knob in the 9 o’clock position;...
  • Page 275 Air Turbine Starter (ATS) and Starting Control Valve (SCV). Do not allow the hot air from the ground cart to exceed 100°C (212°F), as it may damage the components inside the nacelle. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 276 Continue to monitor engine instruments, mainly oil pressure and temperature. Apply associated abnormal procedure if any failure arises. Main Panel ..............CHECK Check proper operation of all instruments and systems. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 277 Packs should be off to avoid contamination of cabin air with fumes generated from ingestion of fluids in engine/APU. Ice Detection Override Knob ........ENG CONTINUES ON NEXT PAGE Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 278 The Ice Detection Override Knob must be at ENG during all ground operations in icing conditions. Pitch Trim ..............SET Pitch Trim must be set as per CG position stated in the Weight and Balance sheet. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 279 CAUTION: • IF FLAPS WERE LEFT UP DURING TAXI, COMPLETE AFTER START CHECKLIST BEFORE TAKEOFF. • TAXI REDUCED SPEED ICE-COVERED RUNWAYS TO AVOID SKIDDING THE AIRPLANE. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 280 Thrust Levers............IDLE Ice Detection Override Knob ........ENG CAUTION: ICE DETECTION OVERRIDE KNOB MUST NOT BE SET TO "ALL" ON GROUND, EXCEPT DURING TEST. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 281 Check that OPEN inscriptions in the buttons are illuminated and NO ICE-A/ICE ON caution message is displayed on EICAS. The CROSS BLD OPEN advisory message may also be displayed. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 282 High winds and jet blast may cause anti-icing fluid to flow off and many other factors contribute to reduce fluid effectiveness. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 283 Flight controls forces may be heavier than normal, without causing any difficult in controllability. Increased V2 procedures (if available in the approved AFM) may be used if runway length is not a limiting factor. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 284 ECS and Pneumatic page) in the green range. During cruise, observe minimum fuel tank temperature (-40°C). If fuel temperature reaching limit, apply FUEL TEMPERATURE procedure in the AFM. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 285 AFM. When landing below -40°C (-40°F), ensure that rate of descent before touchdown is less than 300 ft/min. After landing, report to the maintenance personnel. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 286 Do not use asymmetric reverse thrust on slippery and icy runways. − Apply brakes with moderate-to-firm pressure, smoothly and symmetrically, and let the anti-skid do its job. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 287 UNOBSTRUCTED Air Conditioning Inlets and Outlets ..CLEAR OF ICE Fuel Tank Vents........CLEAR OF ICE OR SNOW Ask for deice/anti-ice fluid application, if necessary. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 288 -15°C (5°F). Doors and Windows ....... CLOSED All doors and windows must be closed to prevent snow and humidity from entering into the airplane. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 289 Page Code 1-02-79 TEMPORARY REVISION 41.1 Copyright © by Embraer. Refer to cover page for details.
  • Page 290 In this case, the anti-ice system is Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 291 Therefore, as a general policy, the use of flaps in icing conditions should be avoided or minimized whenever possible. Page Code 1-02-79 TEMPORARY REVISION 41.1 Copyright © by Embraer. Refer to cover page for details.
  • Page 292 Therefore, as a general policy, the use of flaps in icing conditions should be avoided or minimized whenever possible. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 293: Turbulent Air Penetration

    In case of inadvertent negative-g condition, reduce thrust levers. NOTE: Do not extend flaps except for approach and landing. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 294: Volcanic Ash

    − damage to the engines, wing and tail leading edge surfaces, windshields, landing lights, etc; Windshield and windows may become opaque, reducing the − visibility. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 295 Avoid static engine operation above idle; − Use APU for engine starting only, not for air conditioning. − Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 296 Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 297 Inform ATC of the encounter. Airspeed................ MONITOR Monitor airspeed for any abnormal indication. If necessary perform the Unreliable Airspeed procedure. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 298: Lightning Strike

    Incident reports also show that lightning strikes occur most commonly under light or heavy turbulence conditions. − Flight regime: Takeoff, climb, level flight, descent or approach. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 299 In case of lightning strike, report the incident to the maintenance personnel, by filling out the LIGHTNING STRIKE REPORT (Abnormal Procedures - Section 1-03-70 - Miscellaneous). Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 300 Fuel System ..............CHECK Check fuel system for normal operation. Monitor fuel remaining and fuel consumption to ascertain that no fuel leak exists. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 301 Perform SECTION 05-50-01 (AMM) for detailed procedures to carry out a general inspection after a lightning strikes the airplane. Make sure that these procedures are carried out before flying the airplane again. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 302: Pressurization In Manual Mode

    This setting allows one outflow valve to be fully open and reduces cabin airflow, thus avoiding uncomfortable pressure changes when the doors are closed or during engine starts. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 303 Maintain the cabin altitude consistent with the airplane altitude specified on the table by close monitoring differential pressure and intermittent setting of the manual controller. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 304 In this position, the outflow valve will be kept fully open, which will equalize outside and inside cabin pressure. After that, cockpit side windows and airplane doors can be opened. Page Code 1-02-79 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 305: Flight Management System

    AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL FMZ 2000 FLIGHT MANAGEMENT SYSTEM The information contained herein supplements the information of the basic AOM Normal Procedures. HOLDING If a Holding Pattern entering is necessary: FMS ................. AS REQUIRED The pilot must check the entry type and turn direction of holding pattern before entering it.
  • Page 306 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL FMS SOURCE SELECTION Flight Plan ..............SELECT OR CREATE FMS Source ..............SELECT The FMS can be selected as the navigation source through the FMS Selector Button located on the Display Control Panel. FMS Label..............CHECK The FMS label appears on the associated PFD and MFD.
  • Page 307 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL TRANSITION FROM FMS TO AUTOPILOT ILS APPROACH ILS Frequency .............. SELECT AS REQUIRED Radio Altitude ............... SELECT AS REQUIRED HDG Mode (Flight Guidance Controller) ...... SELECT Before selection, set the desired interception course on heading bug.

  • Page 308: Rvsm Operation

    SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL NAV Mode (Flight Guidance Controller) ....... SELECT Reselecting the NAV mode the airplane will regain the lateral guidance from the FMS to fly the missed approach legs to the missed holding point and to enter holding, as required. RVSM OPERATION The RVSM operation reduces the EMB-145 minimum vertical separation from 2000 ft to 1000 ft between FL 290 and FL 370.
  • Page 309 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL EMERGENCY AND ABNORMAL PROCEDURES The procedures presented in the basic AOM Emergency/Abnormal Procedures remain unchanged, except as amended herein. In case of emergency or abnormal situation or contingencies (equipment failures, weather, etc.) which affect the ability to maintain the cleared flight level, notify ATC and co-ordinate an action plan that is appropriate to the airspace concerned;...
  • Page 310 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL It has been observed that, during normal operation when flying with the autopilot using ADC 1 as source of information and transponder 2 is selected for transmitting altitude information to ATC or vice versa, the altitude difference between the two ADC’s, however small it is, is seen by ATC as discrepancy between the assigned altitude and the actual altitude, adding to the altitude overall error.

  • Page 311: Enhanced/Ground Proximity Warning

    AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL ENHANCED/GROUND PROXIMITY WARNING Aural Warning: WHOOP-WHOOP PULL UP PULL UP (for EGPWS), SINK RATE, TERRAIN TERRAIN or TERRAIN TERRAIN PULL UP (for EGPWS), CAUTION TERRAIN (for EGPWS), OBSTACLE OBSTACLE PULL UP (for EGPWS), CAUTION OBSTACLE (for EGPWS), DON`T SINK DON`T SINK, TOO LOW TERRAIN, TOO LOW GEAR, TOO LOW FLAPS, GLIDE SLOPE and BANK ANGLE...

  • Page 312: Traffic And Collision Avoidance

    SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL TRAFFIC AND COLLISION AVOIDANCE Aural Warning: According to the Traffic Advisory (TA) and Resolution Advisory (RA) associated. The pilot must not initiate evasive maneuvers using information from the traffic display or the voice message only, without visually sighting the traffic.

  • Page 313: Rnp Approach

    AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL RNP APPROACH INTRODUCTION The material contain herein is a guidance to perform RNP APCH operations. According to AC 90-105, airplanes conducting GPS approaches under AC 90-94 meet the airworthiness requirements of RNP Approach Operations. NOTE: Compliance with the above regulations does not constitute operational approvals.
  • Page 314 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL GENERAL GUIDANCE While performing RNP APCH operations, pilots are required to use the Flight Director and/or Autopilot in lateral navigation mode. RNP APCH operations require flight crew monitoring of lateral track deviations on the PFD to ensure the airplane remains within the bounds defined by the procedure.
  • Page 315 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL PRIOR TO FLIGHT Airplane Minimum Configuration ........CHECK Check the airplane configuration complies with the applicable list below: For RNP APCH Operation: 1 FMS. − − 1 GPS. − 1 DME (*). 1 VOR/LOC (*). −...
  • Page 316 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL APPROACH BRIEFING Procedure..............CONFIRM The flight crew must retrieve the approach procedure by procedure name from the FMS and confirm that the correct approach and missed approach procedures have been selected by comparing the FMS waypoints and distances with the aeronautical charts.
  • Page 317 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL ABNORMAL PROCEDURES In case of loss of GPS based navigation capability, alternate non-GPS procedures at the destination airport must be available. LOSS OF SIGNAL IN SPACE During a RNP APCH operation, if at any time GPS signal is lost the APP annunciation is removed, the DGR (or DR) PFD annunciation is displayed, and the deviations remain displayed and valid.

  • Page 318: Performance Based Navigation (Pbn)

    While performing PBN operations, pilots are encouraged to use the Flight Director and/or Autopilot in lateral navigation mode. The following table presents the EMBRAER ERJ-145 capabilities in terms of the navigation specifications related to PBN. The information provided is based on AFM statements and, when there is no AFM statement, on analysis of the respective guidance material.
  • Page 319 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL The airplane is compliant with AC 90-100A (RNAV 1 and RNAV 2) and with TGL-10 (P-RNAV and B-RNAV). RNAV SPECIFICATIONS Sensors that Guidance Guidance Operation may be used EASA RNAV 10 2 GNSS (2) Order Order (RNP 10)
  • Page 320 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL (5b) AMC 20-4 defines that installations in accordance with AC 20- 130() is an acceptable means of compliance for Basic RNAV systems, with no further substantiation. According to AFM, the EMB-145 RNAV system installation is compliant with AC 20-130A. (6) NO AFM STATMENT - The AC 90-100A compliance table lists that the EMB-145 complies with AC-90-100A, therefore it is capable of RNAV 1 operation.
  • Page 321 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL LIMITATIONS  For RNAV operations in terminal airspace, obstacle clearance protection, up to the Final Approach FIX (FAF), will assume that airplane comply with the required RNAV accuracy requirements;  Obstacle clearance altitude is based upon the infrastructure giving the poorest precision;...
  • Page 322 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL NORMAL PROCEDURES PRE-FLIGHT PLANNING NOTAM NAVAIDS ............VERIFY Verify the availability of the intended RNAV procedure. Verify also if any NAVAID identified in the AIP and on the relevant charts as critical for a specific RNAV procedure is not available. Airplane Minimum Configuration........
  • Page 323 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL Navigation Database ............ CHECK The navigation database must be appropriate for the region of the intended operation and must include the NAVAIDS, waypoints, and coded terminal airspace procedures for the departure, arrival and alternate airfields. In this case, affected procedures must be prohibited by an operator’s notice to the flight crew.
  • Page 324 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL DEPARTURE (RNAV 1/P-RNAV / RNAV 2) NAV Database (both pilots) .......... VERIFY CURRENCY Airplane Position Entry..........CHECK Desired Path (PNF)............VERIFY Airplane Position relative to the Path......CHECK Flight Plan ..............CHECK Compare the navigation charts with the MAP display and the MCDU.
  • Page 325 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL CONTINENTAL ENROUTE (B-RNAV/RNAV 5/RNAV 1/RNAV 2) Cleard Flight Plan ............CHECK Flight crew should cross-check the cleared flight plan by comparing charts or other applicable resources with the navigation system textual display and the airplane map display, if applicable. If required, the exclusion of specific NAVAIDs should be confirmed.
  • Page 326 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL ARRIVAL (RNAV 1/P-RNAV AND RNAV 2) RNAV arrival operation may only be performed down to the FAF, and shall not be used on Final Approach, i.e. from FAF to RWY or during Missed Approach. Active Flight Plan ............
  • Page 327 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL Altitude/Speed Constraints ........... CHECK Flight crew must be aware of any published altitude or speed constraints in the procedure. CONTINGENCY PROCEDURES ATC................NOTIFY Notify any problem with the RNAV system that results in the loss of required navigation capability, together with the proposed course of action.
  • Page 328 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL Operation Required Action Non-RNP Terminal or En-route Crosscheck FMS data with raw (including B-RNAV) data from VOR, DME and NDB. De-select sensor causing error, if detectable. P-RNAV Contact ATC, advise inability to continue P-RNAV. Non-RNP (excluding Use alternate sourse (VOR, NDB...
  • Page 329 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL INCIDENT REPORTING Significant incidents associated with the operation of the airplane which affect or could affect the safety of RNAV operations, need to be reported on the appropriate report manifest. Specific examples may include: ...
  • Page 330 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL INTENTIONALLY BLANK Page Code 1-02-80 REVISION 40...
  • Page 331 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL UNS-1K FLIGHT MANAGEMENT SYSTEM The information contained herein supplements the information of the basic AOM Normal Procedures. HOLDING If a Holding Pattern entering is necessary: FMS ................. AS REQUIRED The pilot must check the entry type and turn direction of holding pattern before entering it.
  • Page 332 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL FMS SOURCE SELECTION Flight Plan ..............SELECT OR CREATE FMS Source ..............SELECT The FMS can be selected as the navigation source through the FMS Selector Button located on the Display Control Panel. FMS Label..............CHECK The FMS label appears on the associated PFD and MFD.
  • Page 333 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL The FMS LOC, B/C, GPS, NDB, RNAV, VOR, VOR/DME and VFR approaches may be linked into the flight plan and laterally coupled to the autopilot/Flight Director as follows: APPROACH TRANSITION When a entire approach transition (e.g., procedure turn, DME arc, etc.) is to be flown, the FMS will automatically enter in the ARM APPR mode at 30 nm from the runway with the lateral deviation scaling of 1 nm (full scale), then:...
  • Page 334 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL TRANSITION FROM FMS TO AUTOPILOT ILS APPROACH ILS Frequency............... SELECT AS REQUIRED Radio Altitude..............SELECT AS REQUIRED HDG Mode (Flight Guidance Controller)....... SELECT Before selection, set the desired interception course on heading bug. Navigation Source............SELECT Select the NAV source on the Display Control Panel (LOC course selected on the PFD).
  • Page 335 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL RVSM OPERATION The RVSM operation reduces the EMB-145 minimum vertical separation from 2000 ft to 1000 ft between FL 290 and FL 370. Airworthiness approval alone does not authorize flight into airspace for which an RVSM operational approval is required by an ICAO Regional Navigation Agreement.
  • Page 336 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL EMERGENCY AND ABNORMAL PROCEDURES The procedures presented in the basic AOM Emergency/Abnormal Procedures remain unchanged, except as amended herein. In case of emergency or abnormal situation or contingencies (equipment failures, weather, etc.) which affect the ability to maintain the cleared flight level, notify ATC and co-ordinate an action plan that is appropriate to the airspace concerned;...
  • Page 337 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL It has been observed that, during normal operation when flying with the autopilot using ADC 1 as source of information and transponder 2 is selected for transmitting altitude information to ATC or vice versa, the altitude difference between the two ADC’s, however small it is, is seen by ATC as discrepancy between the assigned altitude and the actual altitude, adding to the altitude overall error.
  • Page 338 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL ENHANCED/GROUND PROXIMITY WARNING Aural Warning: WHOOP-WHOOP PULL UP PULL UP (for EGPWS), SINK RATE, TERRAIN TERRAIN or TERRAIN TERRAIN PULL UP (for EGPWS), CAUTION TERRAIN (for EGPWS), OBSTACLE OBSTACLE PULL UP (for EGPWS), CAUTION OBSTACLE (for EGPWS), DON`T SINK DON`T SINK, TOO LOW TERRAIN, TOO LOW GEAR, TOO LOW FLAPS, GLIDE SLOPE and BANK ANGLE...
  • Page 339 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL TRAFFIC AND COLLISION AVOIDANCE Aural Warning: According to the Traffic Advisory (TA) and Resolution Advisory (RA) associated. The pilot must not initiate evasive maneuvers using information from the traffic display or the voice message only, without visually sighting the traffic.
  • Page 340 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL RNP APPROACH INTRODUCTION The material contain herein is a guidance to perform RNP APCH operations. According to AC 90-105, airplanes conducting GPS approaches under AC 90-94 meet the airworthiness requirements of RNP Approach Operations. NOTE: Compliance with the above regulations does not constitute operational approvals.
  • Page 341 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL GENERAL GUIDANCE While performing RNP APCH operations, pilots are required to use the Flight Director and/or Autopilot in lateral navigation mode. RNP APCH operations require flight crew monitoring of lateral track deviations on the PFD to ensure the airplane remains within the bounds defined by the procedure.
  • Page 342 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL PRIOR TO FLIGHT Airplane Minimum Configuration........CHECK Check the airplane configuration complies with the applicable list below: For RNP APCH Operation: − 1 FMS. − 1 GPS. − 1 DME (*). − 1 VOR/LOC (*). −...
  • Page 343 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL APPROACH BRIEFING Procedure ..............CONFIRM The flight crew must retrieve the approach procedure by procedure name from the FMS and confirm that the correct approach and missed approach procedures have been selected by comparing the FMS waypoints and distances with the aeronautical charts.
  • Page 344 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL ABNORMAL PROCEDURES In case of loss of GPS based navigation capability, alternate non-GPS procedures at the destination airport must be available. LOSS OF SIGNAL IN SPACE During a RNP APCH operations, if at any time GPS signal is lost a red X is displayed over the Course Deviation Scale and the INTEG annunciation may be displayed.
  • Page 345 While performing PBN operations, pilots are encouraged to use the Flight Director and/or Autopilot in lateral navigation mode. The following table presents the EMBRAER ERJ-145 capabilities in terms of the navigation specifications related to PBN. The information provided is based on AFM statements and, when there is no AFM statement, on analysis of the respective guidance material.
  • Page 346 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL The airplane is compliant with AC 90-100A (RNAV 1 and RNAV 2) and with TGL-10 (P-RNAV and B-RNAV). RNAV SPECIFICATIONS Sensors that Guidance Guidance Operation may be used EASA RNAV 10 Order (RNP 10) 2 GNSS (2) Order 8400.12A...
  • Page 347 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL LIMITATIONS  For RNAV operations in terminal airspace, obstacle clearance protection, up to the Final Approach FIX (FAF), will assume that airplane comply with the required RNAV accuracy requirements;  Obstacle clearance altitude is based upon the infrastructure giving the poorest precision;...
  • Page 348 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL NORMAL PROCEDURES PRE-FLIGHT PLANNING NOTAM NAVAIDS ............VERIFY Verify the availability of the intended RNAV procedure. Verify also if any NAVAID identified in the AIP and on the relevant charts as critical for a specific RNAV procedure is not available. NOTE: If it is requested to inhibit an individual NAVAID, do not perform an operation that uses VOR/DME for positioning.
  • Page 349 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL RNAV System (if required) ........... CONFIRM AVAILABILITY When dual RNAV system is required on the AIP. RAIM (if applicable) ............CONFIRM AVAILABILITY  Confirmation is necessary if a stand-alone GPS is to be used for RNAV 1 and RNAV 2 operations.
  • Page 350 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL DEPARTURE (RNAV 1/P-RNAV / RNAV 2) NAV Database (both pilots) .......... VERIFY CURRENCY Airplane Position Entry..........CHECK Desired Path (PNF)............VERIFY Airplane Position relative to the Path......CHECK Flight Plan ..............CHECK Compare the navigation charts with the MAP display and the MCDU.
  • Page 351 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL CONTINENTAL ENROUTE (B-RNAV/RNAV 5/RNAV 1/RNAV 2) Cleard Flight Plan ............CHECK Flight crew should cross-check the cleared flight plan by comparing charts or other applicable resources with the navigation system textual display and the airplane map display, if applicable. If required, the exclusion of specific NAVAIDs should be confirmed.
  • Page 352 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL ARRIVAL (RNAV 1/P-RNAV AND RNAV 2) RNAV arrival operation may only be performed down to the FAF, and shall not be used on Final Approach, i.e. from FAF to RWY or during Missed Approach. Active Flight Plan ............
  • Page 353 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL Altitude/Speed Constraints ........... CHECK Flight crew must be aware of any published altitude or speed constraints in the procedure. CONTINGENCY PROCEDURES ATC................NOTIFY Notify any problem with the RNAV system that results in the loss of required navigation capability, together with the proposed course of action.
  • Page 354 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL Operation Required Action Non-RNP Terminal or En-route Crosscheck FMS data with raw (including B-RNAV) data from VOR, DME and NDB. De-select sensor causing error, if detectable. P-RNAV Contact ATC, advise inability to continue P-RNAV. Non-RNP (excluding Use alternate sourse (VOR,...
  • Page 355 AIRPLANE SUPPLEMENTARY PROCEDURES OPERATIONS NAVIGATION MANUAL INCIDENT REPORTING Significant incidents associated with the operation of the airplane which affect or could affect the safety of RNAV operations, need to be reported on the appropriate report manifest. Specific examples may include: ...
  • Page 356 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS NAVIGATION MANUAL INTENTIONALLY BLANK Page Code 1-02-80 REVISION 40...

  • Page 357: Engine Start With Airplane Batteries And

    SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS ENGINE MANUAL ENGINE START WITH AIRPLANE BATTERIES AND LOW PRESSURE UNIT (LPU) This procedure may be used when operating without APU or GPU but with the batteries and a Low Pressure Unit (LPU) available for engine start.
  • Page 358 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS ENGINE MANUAL CLEARED TO START Doors and Windows ............CLOSED Red Beacon..............ON Fuel Pump (associated engine)........ON Start Pressure ...............AVAILABLE START Start/Stop Selector (associated engine)......START, THEN Turn the start selector to RUN for 2 seconds, then turn the switch to the START position momentarily (signals the initiate start sequence to the FADEC) and then to RUN, and start the stopwatch.

  • Page 359: Cross Start

    SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS ENGINE MANUAL ENGINE START ASSISTED BY THE OPPOSITE ENGINE (CROSS START) This procedure may be used to start the second engine using the operating engine bleed as the pneumatic source. Crossbleed ..............AUTO or OPEN Engine Bleed (non-operating engine) ......CLOSE Engine Bleed (operating engine)........

  • Page 360: Single Engine Taxi

    SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS ENGINE MANUAL SINGLE ENGINE TAXI The procedures below are provided to allow operators to perform a single engine taxi. This procedure can be adopted at crowded airports, where the taxi time may be too long, leading to unnecessary fuel waste and air pollution.
  • Page 361 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS ENGINE MANUAL BEFORE TAKEOFF Non Operating Engine........... START Crossfeed..............OFF Shed Buses..............AUTO Electric Hydraulic Pumps ..........AUTO Air Conditioning and Pneumatic System....... AS REQUIRED AFTER LANDING Shed Buses..............OVRD Electric Hydraulic Pumps ..........AUTO Air Conditioning and Pneumatic System....... AS REQUIRED Selected Engine ............
  • Page 362 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS ENGINE MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-02-81 MARCH 30, 2001...

  • Page 363: Flight Instruments

    SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS FLIGHT INSTRUMENTS MANUAL ALTIMETER MISCOMPARE TOLERANCES This Section provides information regarding maximum allowed tolerances between PFD altitude indications and standby altimeter. For the EMB-145, ERJ-140 and EMB-135 models, there are two pitot probes, four static probes and one pitot static probe. Pitot probes 1 and 2 and the static ports send information to ADCs 1 and 2.
  • Page 364 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS FLIGHT INSTRUMENTS MANUAL To verify if altimeter difference is within tolerance, the flight crew should proceed as follows: Altitude................STABILIZE Maintain variation within +/- 50 ft. Air Speed...............STABILIZE Maintain variation within +/- 5 kt. Wait a minimum of 15 seconds in straight and leveled flight, preferably with Autopilot engaged, to compare the difference between altitudes using the following table: MAXIMUM...

  • Page 365: Cat Ii Operation

    SUPPLEMENTARY AIRPLANE NORMAL PROCEDURES OPERATIONS CAT II OPERATION MANUAL CAT II OPERATION The information contained herein supplements the information of the the basic AOM Normal Procedures. AUTOPILOT COUPLED CAT II APPROACH BEFORE INTERCEPTING LOCALIZER COURSE − Perform the Descent/Approach/Before Landing checklists, as appropriate.
  • Page 366 SUPPLEMENTARY AIRPLANE NORMAL PROCEDURES OPERATIONS CAT II OPERATION MANUAL AFTER PASSING THE OUTER MARKER INBOUND − The pilot flying should maintain the Approach Speed (V ) for flaps 22° . − Both pilots must monitor the progress of the approach on their displays down to approximately 200 ft above the decision height.
  • Page 367 SUPPLEMENTARY AIRPLANE NORMAL PROCEDURES OPERATIONS CAT II OPERATION MANUAL MISSED APPROACH GO-AROUND Procedure..........ACCOMPLISH LANDING Reaching the Decision Height with runway in sight: Autopilot..............DISENGAGE Speed ..............V REF 22° Landing ..............PERFORM Page Code 1-02-83 REVISION 38...
  • Page 368 SUPPLEMENTARY AIRPLANE NORMAL PROCEDURES OPERATIONS CAT II OPERATION MANUAL INTENTIONALLY BLANK Page Code 1-02-83 REVISION 38...

  • Page 369: Hgs Operation

    SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS HGS OPERATION MANUAL HGS OPERATION information presented this Supplement enables establishment of the conditions required to accomplish the HGS operation. The Flight Dynamics Model 3300 Head-Up Guidance System (HGS) is approved for use throughout the full flight regime as a supplemental display.
  • Page 370 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS HGS OPERATION MANUAL VISIBILITY TAKEOFF CONDITIONS OPERATION The low visibility takeoff display and Ground Roll Guidance Cue are automatically provided to the pilot once the following conditions have been established: − Primary mode selected; − IRS in NAV mode; −...
  • Page 371 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS HGS OPERATION MANUAL USE OF HGS IN MODES OTHER THAN LOW VISIBILITY TAKEOFF AND AIII The use of HGS in all modes other than for Low Visibility Takeoff and AIII must be in accordance with the limitations, emergency and abnormal procedures, normal procedures and performance data contained in the basic AOM.
  • Page 372 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS HGS OPERATION MANUAL NORMAL PROCEDURES The procedures below must replace or complement the Normal Procedures contained in the basic AOM. BEFORE START IRS ................SET TO NAV HGS Combiner............SET HGS Control Panel: HGS Mode ............PRI RUNWAY LENGTH ..........
  • Page 373 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS HGS OPERATION MANUAL BEFORE TAKEOFF Low Visibility Takeoff Briefing ........PERFORM Aircraft Reference Symbol........SET TO RUNWAY CENTERLINE Course Selector 1 ............ READJUST WITH RUNWAY CENTERLINE Course Selector 2 ............ READJUST WITH RUNWAY CENTERLINE Heading Bug ............SET TO RUNWAY CENTERLINE Ground Roll Guidance Cue........
  • Page 374 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS HGS OPERATION MANUAL APPROACH AIII MODE APPROACH NOTE: The approach must be initiated with the airplane in final configuration and stabilized. Display Control Panel 1..........SET TO NAV 1 Display Control Panel 2..........SET TO NAV 2 ALL 3 NAV Receivers ..........
  • Page 375 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS HGS OPERATION MANUAL CAUTION: • IF VISUAL CONTACT IS NOT MADE UPON REACHING THE DECISION HEIGHT OR IF ANY MALFUNCTION COULD NOT BE PROMPTLY IDENTIFIED DURING APPROACH, MISSED APPROACH MUST IMMEDIATELY INITIATED; • RUNWAY REMAINING SUPPLEMENTAL SITUATION AWARENESS DISPLAY DECREASING IN INCREMENTS AVAILABLE...
  • Page 376 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS HGS OPERATION MANUAL WINDSHEAR PREVENTION/RECOVERY will display “WDSHEAR” message when GPWS/EGPWS detects a windshear. In the event of a windshear, the HGS will display a “WDSHEAR” on the combiner and on the PFD. A voice message will be presented in case of a red “WDSHEAR”...

  • Page 377: High Altitude Operation

    If flying in an airport above 8000 ft: High Altitude Mode ..........ON Check that HI ALT LDG-T/O advisory message is displayed on the EICAS. Crew Oxygen Mask ..........DON Page Code 1-02-87 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 378 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS HIGH ALTITUDE MANUAL OPERATION INTENTIONALLY BLANK Page Code 1-02-87 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 379: Operation In Airports Up To 8500 Ft

    SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS OPERATION IN AIRPORTS MANUAL UP TO 8500 FT OPERATION IN AIRPORTS UP TO 8500 FT The actions listed in the procedure below must complement the equivalent procedure contained in the basic AOM. The remaining Normal Procedures section remains unchanged. BEFORE START Pressurization ...............
  • Page 380 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS OPERATION IN AIRPORTS MANUAL UP TO 8500 FT INTENTIONALLY BLANK Page Code 1-02-92 REVISION 31...

  • Page 381: Bounced Landing Recovery

    SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS BOUNCED LANDING MANUAL RECOVERY BOUNCED LANDING RECOVERY The key factor for a successful landing is a stabilized approach and proper thrust/flare coordination. Do not extend the flare at idle thrust as it will significantly increase landing distance. Reducing to idle before the flare will also require an increase in pitch.
  • Page 382 SUPPLEMENTARY AIRPLANE PROCEDURES OPERATIONS BOUNCED LANDING MANUAL RECOVERY INTENTIONALLY BLANK Page Code 1-02-94 REVISION 39...

  • Page 383: Profiles

    AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL PROFILES EM145AOM021001D.DGN Page Code 1-02-95 REVISION 36...
  • Page 384 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL EM145AOM000045A.DGN Page Code 1-02-95 REVISION 36...
  • Page 385 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL EM145AOM000044A.DGN Page Code 1-02-95 REVISION 36...
  • Page 386 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL EM145AOM210001A.DGN Page Code 1-02-95 REVISION 36...
  • Page 387 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL EM145AOM210002A.DGN Page Code 1-02-95 REVISION 36...
  • Page 388 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL EM145AOM021003A.DGN Page Code 1-02-95 REVISION 36...
  • Page 389 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL EM145AOM021004C.DGN Page Code 1-02-95 REVISION 36...
  • Page 390 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL EM145AOM021012A.DGN Page Code 1-02-95 REVISION 36...
  • Page 391 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL EM145AOM021005C.DGN Page Code 1-02-95 REVISION 36...
  • Page 392 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL EM145AOM021019B.DGN Page Code 1-02-95 REVISION 36...
  • Page 393 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL EM145AOM021013C.DGN Page Code 1-02-95 REVISION 36...
  • Page 394 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL EM145AOM021016C.DGN Page Code 1-02-95 REVISION 36...
  • Page 395 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL EM145AOM021014D.DGN Page Code 1-02-95 REVISION 36...
  • Page 396 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL EM145AOM021015C.DGN Page Code 1-02-95 REVISION 36...
  • Page 397 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL EM145AOM021009A.DGN Page Code 1-02-95 REVISION 36...
  • Page 398 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL EM145AOM021011A.DGN Page Code 1-02-95 REVISION 36...
  • Page 399 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL EM145AOM021011A.DGN Page Code 1-02-95 REVISION 36...
  • Page 400 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL EM145AOM021010A.DGN Page Code 1-02-95 REVISION 36...
  • Page 401 AIRPLANE NORMAL PROCEDURES OPERATIONS MANUAL PITCH, N1 AND SPEED TABLE WEIGHT SPEED GEAR PITCH FLAPS (kg) (kt) 20000 61.5 20000 55.3 20000 53.6 20000 53.6 20000 55.3 20000 57.2 20000 59.8 19000 66.9 19000 65.4 19000 64.2 19000 72.5 19000 61.9 18000 60.3...
  • Page 402 NORMAL PROCEDURES AIRPLANE OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-02-95 REVISION 36...
  • Page 403 EMERGENCY AND AIRPLANE ABNORMAL OPERATIONS PROCEDURES MANUAL SECTION 1-03 EMERGENCY AND ABNORMAL PROCEDURES TABLE OF CONTENTS Page Block Introduction .................1-03-00 Emergency Procedures Doors ................1-03-01 Crew Awareness ..............1-03-02 Electrical ................1-03-03 Fire Protection ..............1-03-05 Fuel...................1-03-07 APU ..................1-03-09 Powerplant................1-03-11 Landing Gear..............1-03-14 Flight Controls ..............1-03-20 Air Conditioning/Pressurization/Ice Protection ....1-03-24 Autopilot................1-03-26 Forced Landing..............1-03-30...
  • Page 404 EMERGENCY AND AIRPLANE ABNORMAL OPERATIONS PROCEDURES MANUAL Fuel .................. 1-03-40 APU.................. 1-03-41 Powerplant ............... 1-03-45 Hydraulic ................1-03-48 Landing Gear ..............1-03-50 Flight Controls..............1-03-53 Air Conditioning, Pneumatics and Pressurization ... 1-03-56 Ice Protection..............1-03-57 Oxygen................1-03-58 Navigation ................ 1-03-59 Autopilot ................

  • Page 405: Introduction

    EMERGENCY AND AIRPLANE ABNORMAL OPERATIONS PROCEDURES MANUAL INTRODUCTION The source document for all procedures contained herein is the approved Airplane Flight Manual (AFM). In the event that any procedure disagrees with the AFM, the AFM will prevail. In the event that any of the procedures are missing or unusable, operations may be continued provided the approved AFM is available for use.
  • Page 406 EMERGENCY AND AIRPLANE ABNORMAL OPERATIONS PROCEDURES MANUAL − System controls are in normal condition prior to initiation of the associated procedure. − Aural warnings silenced applicable. Master Warning/Caution lights are reset as soon as the failure is recognized. − Oxygen masks and smoke goggles are donned when cabin altitude is excessive or ambient air is contaminated.
  • Page 407 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL EMERGENCY PROCEDURES MAIN OR SERVICE DOOR OPEN EICAS WARNING: MAIN DOOR OPN or SERVICE DOOR OPN LIGHT: Master Warning INDICATION: Associated door pictorial indication and a DOOR OPEN inscription on MFD are displayed in red. Fasten Seat Belts.............
  • Page 408 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-03-01 REVISION 40...
  • Page 409 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL STALL PROTECTION INOPERATIVE EICAS WARNING: SPS 1 (2) INOP LIGHT: Master Warning Associated Stall Protection System......OFF Avoid skidding the airplane. Add 5 KIAS to go-around speeds. NOTE: The remaining stick shaker is available. Approach and landing configuration: Landing Gear ..............
  • Page 410 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL ENHANCED/GROUND PROXIMITY WARNING EICAS WARNING: GPWS LIGHT: Master Warning Voice Messages: WHOOP-WHOOP PULL UP or PULL UP (for EGPWS), SINK RATE, TERRAIN TERRAIN or TERRAIN TERRAIN PULL UP (for EGPWS), CAUTION TERRAIN (for EGPWS), OBSTACLE OBSTACLE PULL UP (for EGPWS), CAUTION OBSTACLE (for EGPWS), DON`T SINK DON`T SINK, TOO LOW TERRAIN, TOO LOW GEAR,...

  • Page 411: Emergency Procedures

    AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL WINDSHEAR PREVENTION/RECOVERY AURAL WARNING: WINDSHEAR voice message is generated if WDSHEAR red indication is presented (GPWS warning may also be activated). Thrust Levers..............MAX Go-around Buttons ............PRESS Rotate the airplane smoothly to minimize altitude loss. Flight guidance on EADI must be followed.
  • Page 412 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL AIRPLANE OVERSPEED AURAL WARNING: Voice Message HIGHSPEED LIGHT: Master Warning INDICATION: Airspeed and Mach indications on PFD enter the red range. Airspeed ............... BELOW Page Code 1-03-02 REVISION 40...
  • Page 413 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL BATTERY OVERTEMPERATURE EICAS WARNING: BATT 1 (2) OVTEMP LIGHT: Master Warning INDICATION: Associated battery temperature indication on MFD becomes red. Associated Battery............OFF Check that the associated BATT OFF BUS message is on. If the associated BATT OFF BUS message is not on, land at the nearest suitable airport.
  • Page 414 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL LOSS OF ALL GENERATORS EICAS CAUTION: GEN 1, 2, 3, 4 OFF BUS and APU GEN OFF BUS LIGHT: Master Caution Airspeed ................ MAXIMUM 250 KIAS Altitude ................MEA OR 10000 ft, WHICHEVER IS HIGHER Essential Power ............
  • Page 415 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL NOTE: - For EMB-145XR airplanes, ISIS battery duration is 4 hours. - The nose landing gear doors will open if DC Bus 2 is off, therefore the pilot should expect noise increase. - The following warning messages will be presented: SPS 1-2 INOP and ICE COND-A/I INOP.
  • Page 416 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-03-03 REVISION 40...
  • Page 417 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL CABIN FIRE OR SMOKE CONDITION: Smoke is visually confirmed within the cabin, or identified by odor. Crew Oxygen Masks ............. DON, SELECT 100% Smoke Goggles or PBE ..........DON Recirculation Fan ............OFF Crew Communication............ ESTABLISH Diversion ...............
  • Page 418 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL ELECTRICAL SYSTEM FIRE OR SMOKE CONDITION: Smoke visually confirmed as being from electrical source, or identified by odor. If smoke source can be determined: Electrical Power to Associated Equipment....OFF If smoke source cannot be determined: Shed Buses ..............OFF If smoke does not stop or decrease after a reasonable time, cut power to Central DC Bus as follows:...
  • Page 419 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL AIR CONDITIONING SMOKE CONDITION: Smoke visually confirmed as being from the air conditioning distribution, or identified by odor. Suspect Bleed ............... CLOSE Crossbleed ..............OPEN If procedure does not eliminate smoke, change bleed source supplying the air conditioning (including APU bleed).
  • Page 420 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-03-05 MARCH 30,2001...
  • Page 421 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL FUEL LEAK CONDITION: - FMS Fuel Remaining quantity is above the MFD or EICAS total fuel indication. - Excessive Fuel flow from one of the engines. - Fuel imbalance develops. - Fuel quantity of a tank decreases at an abnormal rate. Land at the nearest suitable airport.
  • Page 422 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL FUEL LOW LEVEL EICAS WARNING: FUEL 1 (2) LO LEVEL LIGHT: Master Warning INDICATION: Fuel quantity indication enters in red range. Thrust Levers ..............REDUCE TO LONG RANGE Level the airplane and check both fuel quantities. If fuel quantity is sufficient, complete the flight normally.
  • Page 423 AIRPLANE EMERGENCY OPERATIONS PROCEDURES MANUAL APU FIRE EICAS WARNING: APU FIRE LIGHT: Master Warning AURAL WARNING: BELL APU Fuel Shutoff Valve ..........CLOSE APU Master Knob ............OFF APU FUEL SOV CLSD message on EICAS ..............CONFIRM If the valve is not confirmed closed and the fire message remains: Right Electric Fuel Pumps ........
  • Page 424 AIRPLANE EMERGENCY OPERATIONS PROCEDURES MANUAL INTENTIONALLY BLANK Page Code 1-03-09 REVISION 40...
  • Page 425 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL ENGINE FIRE, SEVERE DAMAGE SEPARATION EICAS WARNING: ENG 1 (2) FIRE (may be presented) LIGHT: Engine Fire Handle (may be illuminated) AURAL WARNING: BELL (in case of fire) (may sound) Associated Thrust Lever ..........IDLE Associated Start/Stop Selector ........
  • Page 426 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE EMERGENCY EVACUATION Procedure..... AS REQUIRED WARNING: • DO NOT ATTEMPT TO RESTART ENGINE. • IF IN ICING CONDITIONS, REFER TO SINGLE ENGINE OR SINGLE BLEED OPERATION IN ICING CONDITIONS PROCEDURE. NOTE: - If in flight below 9700 ft, the air conditioning pack valves may close automatically.
  • Page 427 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL ENGINE ATTCS NO MARGIN EICAS WARNING: E1 (2) ATTCS NO MRGN LIGHT: Master Warning Consider not taking off. For airplanes equipped with A, A1/1, A1 or A3 engines: Perform a Thrust Assurance Check before the next takeoff, as follows: Thrust Levers .............
  • Page 428 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL DUAL ENGINE FAILURE EICAS WARNING: ENG 1-2 OUT LIGHT: Master Warning Airspeed ................ MINIMUM 260 KIAS Oxygen Mask (if required)..........DON Altitude ................MAX 25000 ft ENGINE AIRSTART Procedure........ACCOMPLISH CAUTION: IF APU HAS BEEN USED TO START THE ENGINES, DO NOT ALTERNATE THE FADECS AFTER START.
  • Page 429 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL ENGINE REVERSER FAILURE/DISAGREE EICAS CAUTION: ENG1 (2) REV FAIL or ENG1 (2) REV DISAGREE LIGHT: Master Caution Do not takeoff. During landing: Affected Thrust Lever ..........IDLE In flight: N1 ................CHECK If N1 is decreasing: Associated Thrust Lever........
  • Page 430 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL TAKEOFF WITH ENGINE FAILURE ABOVE V (APPLICABLE TO ALL MODELS EXCEPT EMB-145 XR) Maximum Takeoff Thrust ..........CHECK At V rotate the airplane to 14° (flaps 9°), 13° (flaps 18°) or 12° (flaps 22°). With positive rate of climb: Landing Gear ............
  • Page 431 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE After flaps are retracted: PRECAUTIONARY ENGINE SHUTDOWN or ENGINE FIRE, SEVERE DAMAGE OR SEPARATION Procedure........AS REQUIRED After a maximum of 5 minutes at Takeoff Thrust: Thrust Rating ............AS REQUIRED TAKEOFF WITH ENGINE FAILURE ABOVE V (APPLICABLE TO EMB-145XR MODEL) Maximum Takeoff Thrust ..........
  • Page 432 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-03-11 REVISION 40...
  • Page 433 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL LANDING GEAR/LEVER DISAGREE EICAS WARNING: LG/LEVER DISAGREE LIGHT: Master Warning. EICAS Indication: Landing gear indication may be present one or more boxes cross-hatched or red. Landing Gear ..............CYCLE If the message persists: In a retraction: Landing Gear ............
  • Page 434 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-03-14 REVISION 17...
  • Page 435 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL PITCH TRIM RUNAWAY EICAS WARNING: AUTOPILOT FAIL (may be presented) EICAS CAUTION: AUTO TRIM FAIL (may be presented) LIGHT: Master Warning light illuminates if AUTOPILOT FAIL message is presented. Message Caution light illuminates if AUTO TRIM FAIL message is presented. CONDITION: Uncommanded pitch and respective trim pictorial indication changes Quick Disconnect Button .........
  • Page 436 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL PITCH TRIM INOPERATIVE (APPLICABLE TO EMB-135 AND EMB-145 AIRPLANES) EICAS WARNING: PIT TRIM 1(2) INOP or PTRIM MAIN INOP, PTRIM BACKUP INOP (may be presented) EICAS CAUTION: AUTO TRIM FAIL (may be presented) If at least one message is presented without pressing any Pitch Trim Switch: Affected Pitch Trim System ........
  • Page 437 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE If it is necessary to reduce airspeed below 160 KIAS, extend flaps to 22°. NOTE: Turning the airplane and extending the landing gear helps to maintain minimum airspeed with unwanted pitch up tendency. Pitch Trim Command..........
  • Page 438 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL PITCH TRIM INOPERATIVE (APPLICABLE TO ERJ-140 AIRPLANES) EICAS WARNING: PIT TRIM 1(2) INOP or PTRIM MAIN INOP, PTRIM BACKUP INOP EICAS CAUTION: AUTO TRIM FAIL If at least one message is presented without pressing any Pitch Trim Switch: Affected Pitch Trim System ........
  • Page 439 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE If pitch trim is not recovered: Consider landing at the nearest suitable airport. Approach and landing configuration: Landing Gear ........... DOWN Flaps............22° Airspeed ........... V REF 45 10 KIAS CAUTION: TO DETERMINE THE MINIMUM SUITABLE LANDING DISTANCE, MULTIPLY...
  • Page 440 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL JAMMED ELEVATOR EICAS WARNING: SPS 1-2 INOP (may be presented) EICAS CAUTION: STICK PUSHER FAIL (may be presented) LIGHT: Master Warning and Master Caution lights illuminate if STICK PUSHER FAIL and SPS 1-2 INOP messages are presented. CONDITION: Both control columns can not be moved either forward or backward.
  • Page 441 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL AILERON/ROLL TRIM RUNAWAY CONDITION: Uncommanded roll noticed by pilots. INDICATION: Trim pictorial indication if caused by roll trim runway. Quick Disconnect Button ..........PRESS AND HOLD Aileron System 1 and 2..........OFF Roll Trim Circuit Breaker (F23) ........PULL Quick Disconnect Button ..........
  • Page 442 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL JAMMED AILERON CONDITION: Both control columns can not be moved to either side. Aileron Disconnect ............PULL Autopilot ................ OFF Airspeed ................ MAXIMUM 200 KIAS NOTE: Roll rate with aileron disconnected is lower than with full system.
  • Page 443 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL JAMMED RUDDER CONDITION: Pedals can not be moved. Command rudder through yaw trim. If not possible: Rudder System 2............. OFF If still jammed: Rudder System 2............. ON Rudder System 1............. OFF If rudder control through pedals is not restored: Airspeed..............
  • Page 444 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL INADVERTENT SPOILER OPENING IN FLIGHT EICAS CAUTION: SPOILER FAIL (may be presented) LIGHT: Master Caution CONDITION: Sudden airspeed or altitude loss, buffeting or roll tendency. INDICATION: SPLRS OPN Speed Brake ..............CLOSE Speed Brake Circuit Breaker (F13)....... PULL Ground Spoiler Outboard Circuit Breaker (F14) ..........
  • Page 445 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL BLEED LEAK EICAS WARNING: BLD 1 (2) LEAK or BLD APU LEAK LIGHT: Master Warning and leak inscription in the associated bleed button illuminated. Crossbleed..............CLOSE Confirm the failed side and proceed. Associated Bleed and APU Bleed......... CLOSE Check on EICAS the following messages: CROSS BLD SW OFF and associated BLD VLV CLSD.
  • Page 446 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL BLEED OVERTEMPERATURE EICAS WARNING: BLD 1 (2) OVTEMP LIGHT: Master Warning INDICATION: Pointer on MFD may be out of view and indication may be red. Crossbleed ..............OPEN Cross-side Bleed............OPEN Associated Bleed ............CLOSE Altitude ................
  • Page 447 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL ANTI-ICING INOPERATIVE IN ICING CONDITIONS EICAS WARNING: ICE COND-A/I INOP with any or all Anti-icing System EICAS CAUTION LIGHT: Master Warning and Master Caution. On the ground, whenever the message is displayed, do not takeoff and perform the test below: Thrust Levers............
  • Page 448 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-03-24 REVISION 40...
  • Page 449 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL AUTOPILOT FAILURE EICAS WARNING: AUTOPILOT FAIL LIGHT: Master Warning AURAL WARNING: AUTOPILOT (only below 2500 ft radio altitude, when autopilot is disconnected) Autopilot ................ DISENGAGE Trim the airplane as required. NOTE: If associated with autopilot hardover a sudden deviation from the expected flight path may occur.
  • Page 450 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-03-26 MARCH 30, 2001...
  • Page 451 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL EMERGENCY DESCENT Cabin Crew ..............NOTIFY Fasten Belts..............ON Thrust Levers..............IDLE Speed Brakes ............... OPEN Airspeed................ 250 KIAS Landing Gear ..............DOWN Minimum Enroute Altitude ..........CHECK CAUTION: THIS PROCEDURE ASSUMES THAT THE INTEGRITY STRUCTURE AFFECTED.
  • Page 452 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL FORCED LANDING This procedure is recommended for landings, with engines operative or not, including places other than a runway. ATC and Cabin Crew ............ NOTIFY Transponder..............7700 ELT................ON Emergency Lights ............ON Passenger ..............PREPARE FOR FORCED LANDING Cabin (below 10000 ft)..........
  • Page 453 AIRPLANE EMERGENCY PROCEDURES OPERATIONS MANUAL DITCHING WARNING: THE EMB-145 WAS NOT TESTED FOR DITCHING. BELOW ARE THE RECOMMENDED PROCEDURES, WHICH HAVE BEEN DEVELOPED BASED ON PREVIOUS EXPERIENCE. ATC/Cabin Crew............NOTIFY Transponder ..............7700 ELT ................ON Emergency Lights ............ON Passengers ..............
  • Page 454 EMERGENCY AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE Upon water contact: Start/Stop Selectors ..........STOP EMERGENCY EVACUATION Procedure ....ACCOMPLISH WARNING: AIRPLANE EVACUATION MUST BE DONE THROUGH THE OVERWING EMERGENCY EXITS ONLY. DO NOT OPEN REMAINING DOORS. EMERGENCY EVACUATION Parking Brake (if necessary).........
  • Page 455 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ABNORMAL PROCEDURES EQUIPMENT AND FURNISHINGS EMERGENCY EXIT OPEN EICAS CAUTION: EMERG EXIT OPEN LIGHT: Master Caution Fasten Belts ..............ON Verify door handle pushed in and remove passengers from the seats near the associated emergency exit. If emergency exit is not confirmed locked or it is not possible to maintain the pressurization: Altitude ..............
  • Page 456 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL MAIN DOOR BLOCKED LIGHT: Door Blocked Closed (Attendant’s panel) To open the door on ground: Check that the door opening area is free of both people and ground equipment. Hydraulic System 1 ..........OFF Main Door Alternative Opening Valve ......ACTUATE DURING 2 MINUTES Unlock the door and open it.

  • Page 457: Crew Awareness

    AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL CREW AWARENESS ERRONEOUS STALL PROTECTION ACTUATION Immediately and simultaneously: Quick Disconnect Button ..........PRESS Both Stall Protection Systems ........CUTOUT Avoid skidding the airplane. Add 5 KIAS to approach, landing and go-around speeds. Landing configuration: Flaps................
  • Page 458 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL STICK PUSHER JAMMING EICAS CAUTION: STICK PUSHER FAIL LIGHT: Master Caution Elevator Disconnection Handle........PULL Copilot must fly the airplane. Avoid landings at airports with anticipated turbulence or crosswinds. GPWS INOPERATIVE EICAS CAUTION: GPWS INOP or TERR INOP (for EGPWS) LIGHT: Master Caution Monitor any trend toward terrain contact, excessive sink rate, marginal flight path and airplane configuration.

  • Page 459: Electrical

    AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL ELECTRICAL APU CONTACTOR CLOSED EICAS CAUTION: APU CNTOR CLOSED LIGHT: Master Caution Bus Ties ................ OFF Battery 2 ............... OFF BACKUP BATTERY OFF BUS EICAS CAUTION: BKUP BATT OFF BUS Backup Battery ............. VERIFY ON BATTERY OFF BUS EICAS CAUTION: BATT 1 (2) OFF BUS LIGHT: Master Caution...
  • Page 460 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ELECTRICAL EMERGENCY ABNORMAL TRANSFER EICAS CAUTION: ELEC EMERG ABNORM LIGHT: Master Caution Essential Power ............CHECK OFF If message persists: Land at the nearest suitable airport. Bus Ties ..............OFF Batteries 1 and 2............OFF If message persists: Bus Ties ..............
  • Page 461 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ESSENTIAL BUS 1 OFF EICAS CAUTION: ESS BUS 1 OFF LIGHT: Master Caution MFD Indication: ESS BUS may be amber. On Reversionary Panel 1: SG................PUSH IN Fuel Pump 1 ..............1B OR 1C Fuel Pump 2 ..............2A OR 2C Altitude ................
  • Page 462 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ESSENTIAL BUS 2 OFF EICAS CAUTION: ESS BUS 2 OFF LIGHT: Master Caution MFD Indication: ESS BUS may be amber. Fuel Pump 1..............1A OR 1C Fuel Pump 2..............2B OR 2C Icing Conditions ............EXIT/AVOID Altitude ................
  • Page 463 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL ESSENTIAL BUS 1-2 OFF EICAS CAUTION: ESS BUS 1-2 OFF Bus Ties ................ OFF MFD Electrical Page ............. CHECK If both DC buses are energized: Batteries 1 and 2 ............. OFF Check if the essential buses remain off. Associated ESS BUS OFF Procedure ....
  • Page 464 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL GENERATOR OVERLOAD EICAS CAUTION: GEN 1 (2, 3, 4) OVLD or APU GEN OVLD LIGHT: Master Caution Shed Buses..............OFF If the message remains: Electrical Load (on affected generator) ....REDUCE If APU generator is not affected and any generator is overloaded: APU Generator ............
  • Page 465 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL LIGHTING EMERGENCY LIGHTS NOT ARMED EICAS CAUTION: EMERG LT NOT ARMD LIGHT: Master Caution Emergency Lighting Selector ........ARM If unsuccessful, check that Attendant Emergency Light Control Button is set to NORM. Page Code 1-03-38 OCTOBER 02, 2001...
  • Page 466 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-03-38 MARCH 30, 2001...

  • Page 467: Fire Protection

    AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL FIRE PROTECTION ENGINE TAILPIPE FIRE CONDITION: Tailpipe fire was detected visually by crew or ground personnel. No EICAS message displayed. Affected engine: Thrust Lever ............IDLE Start/Stop Selector ..........STOP Ignition ..............OFF Fuel Pump ............... OFF XFeed Selector Knob ..........
  • Page 468 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL FIRE EXTINGUISHING INOPERATIVE EICAS CAUTION: E1 (2) EXTBTLA INOP, E1 (2) EXTBTLB INOP, APU EXTBTL INOP or BAGG EXTBL INOP (if installed) LIGHT: Master Caution CONDITION: Associated bottle has not been discharged intentionally. On Engines: Only one discharge will be available from the remaining bottle, to protect both engines against fire.

  • Page 469: Fuel

    ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL FUEL FUEL LOW PRESSURE EICAS CAUTION: E1 (2) FUEL LO PRESS LIGHT: Master Caution CONDITION: One or more associated tank electric fuel pump may be inoperative. Select another electric fuel pump on the associated tank. If all pumps in one tank are inoperative: Altitude..............
  • Page 470 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL FUEL CROSSFEED FAILURE EICAS CAUTION: FUEL XFEED FAIL LIGHT: Master Caution Fuel Imbalance.............. MONITOR Asymmetric Thrust ............AS REQUIRED FUEL IMBALANCE EICAS CAUTION: FUEL IMBALANCE LIGHT: Master Caution If fuel imbalance is confirmed: CROSSFEED OPERATION Procedure ............
  • Page 471 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ENGINE FUEL SHUTOFF VALVE CLOSED EICAS ADVISORY: E1 (2) FUEL SOV CLSD Fire Extinguishing Handle ..........CHECK IN If valve is open and engine is running normally, disregard the message. If valve remains closed and it is not possible to restart the affected engine: PRECAUTIONARY ENGINE SHUTDOWN Procedure ........
  • Page 472 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CROSSFEED OPERATION NOTE: Crossfeed must be OFF during takeoff and landing. If fuel imbalance is verified: Attitude ..............WINGS LEVELED If left wing presents lower level: Crossfeed Selector ..........LOW1 If right wing presents lower level: Crossfeed Selector ..........

  • Page 473: Apu

    ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL AUXILIARY POWER UNIT APU OIL LOW PRESSURE/OIL HIGH TEMPERATURE EICAS CAUTION: APU OIL LO PRESS, APU OIL HI TEMP LIGHT: Master Caution If the APU is not essential for the flight: APU ................. SHUTDOWN If APU is essential, monitor APU EGT and RPM. If the APU EGT enters the red or amber range, apply the APU OVERTEMPERATURE Procedure.
  • Page 474 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-03-41 REVISION 40...

  • Page 475: Powerplant

    AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL POWER PLANT ENGINE FAILURE Remaining Engine Thrust Rating........CON Altitude ................MAX 25000 ft MINIMUM MEA ENGINE AIRSTART Procedure ........AS REQUIRED TCAS ................TA ONLY WARNING: IF IN ICING CONDITIONS, REFER TO SINGLE ENGINE OR SINGLE BLEED OPERATION IN ICING CONDITIONS PROCEDURE.
  • Page 476 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ONE ENGINE INOPERATIVE GO-AROUND Quick Disconnect Button..........PRESS Go Around Button ............PRESS Engine Thrust Levers............ MAX Rotate to go-around attitude (10° nose up). Flaps ................9° With positive rate of climb: Landing Gear ............UP Minimum Airspeed ...........
  • Page 477 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL ABNORMAL ENGINE START Abort engine start immediately when:  Only on ground, no light-up in 10 seconds after the first fuel flow indication. NOTE: The start should not be aborted if fuel flow drops to zero pph immediately after light-up.
  • Page 478 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ENGINE DRY MOTORING Dry motor the engine for a minimum of 30 seconds to clear it of unburned fuel prior to attempting another start. FADEC Control Knob............ ALTN Check alternation of FADEC-in-control indication on the EICAS. CAUTION: IF FADEC DOES NOT ALTERNATE, DO NOT PROCEED WITH THE ENGINE DRY MOTORING.
  • Page 479 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL PRECAUTIONARY ENGINE SHUTDOWN CONDITION: Engine malfunction that is likely to result in an engine damage. Associated Thrust Lever ..........IDLE Associated Start/Stop Selector ........STOP NOTE: - In the event of a thrust lever inoperative above Flight Idle, engine may be shutdown using associated engine fire handle.
  • Page 480 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-03-45 REVISION 38...
  • Page 481 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ENGINE AIRSTART Affected engine: One Electric Fuel Pump (A or B) ......ON Ignition ..............AUTO Start/Stop Selector ..........STOP Engine Bleed ............CLOSE Thrust Lever............. IDLE Airspeed and Altitude............ REFER TO AIRSTART ENVELOPE Perform an assisted start or windmilling, as required: CAUTION: IN ICING CONDITIONS DO NOT USE APU BLEED START, TO AVOID LOSS OF ANTI-ICE SYSTEM PERFORMANCE.
  • Page 482 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE Start/Stop Selector..........START, THEN Engine Indication ..........MONITOR Check ignition. Check N2 rising. Observe limits. Abort start immediately if an Abnormal Engine Start is detected. If Windshield Heating and Electric Hydraulic Pump were turned off before engine start: Windshield Heating........
  • Page 483 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE ENGINE AIRSTART ENVELOPE AE3007A ENGINES 30000 WINDMILLING START POSSIBLE AND ASSISTED START REGION 25000 20000 15000 10000 ONLY ASSISTED START 5000 REGION INDICATED AIRSPEED - KIAS NOTE: Shaded area may be below 1. 23 V Page Code 1-03-45...
  • Page 484 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ENGINE HIGH OIL PRESSURE Oil Pressure, Oil Temperature, Oil Level, Engine Vibration ........MONITOR If oil temperature, and/or oil level, and/or engine vibration, exceeds normal operation range: Associated Procedure..........ACCOMPLISH ENGINE HIGH OIL TEMPERATURE EICAS Indication: Oil temperature pointers and digits become red. Associated Thrust Lever ..........
  • Page 485 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL ENGINE ATS SHUTOFF VALVE OPEN EICAS CAUTION: E1 (2) ATS SOV OPN LIGHT: Master Caution Associated Bleed (including APU bleed) ...... CLOSE Crossbleed..............CLOSE On ground: Associated Thrust Lever.......... IDLE Associated Start/Stop ..........STOP If engine shutdown dows not occur: Fire Extinguishing Handle ........
  • Page 486 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ENGINE CONTROL FAILURE EICAS CAUTION: E1 (2) CTL FAIL (may be presented) LIGHT: Master Caution CAUTION: DO MANUALLY ALTERNATE ASSOCIATED FADECS. Verify the associated FADEC in control. Associated FADEC ............RESET If FADEC alternates automatically: Avoid quick movements of the associated Thrust Lever.
  • Page 487 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL THRUST LEVER FAILURE EICAS CAUTION: ENG1 (2) TLA FAIL LIGHT: Master Caution Associated FADEC ............RESET If Thrust Lever command is not available: Associated FADEC ..........ALTN Check on EICAS that FADEC in control has changed. If thrust lever still does not respond thrust can be partially controlled through the Thrust Rating Buttons.
  • Page 488 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ENGINE OUT EICAS CAUTION: ENG1 (2) OUT LIGHT: Master Caution If during takeoff, above V and associated with an engine flameout: TAKEOFF WITH ENGINE FAILURE Procedure ........... ACCOMPLISH If in flight: PRECAUTIONARY ENGINE SHUTDOWN Procedure ........ACCOMPLISH ENGINE AIRSTART Procedure........
  • Page 489 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL ENGINE ABNORMAL VIBRATION EICAS Indication: Vibration in the amber range below 2.5 IPS for more than 5 minutes during the takeoff or go-around phases or for more than 10 seconds during the remainder flight phases or equal or above 2.5 IPS.
  • Page 490 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CHECK ENGINE PERFORMANCE EICAS ADVISORY: CHECK A (A1, A1E, A1P, A3, A1/3) PERF Associated Engine Performance ........CHECK LOSS OF ENGINE INDICATIONS CONDITION: Loss of Thrust Mode, ITT, N1 and N2 indications. If engine is operative but the indications are lost, proceed: Associated FADEC ..........
  • Page 491 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL HYDRAULIC POWER BOTH HYDRAULIC SYSTEMS FAILURE EICAS CAUTION: HYD SYS 1-2 FAIL, RUDDER SYS 1-2 INOP, AIL SYS 1-2 INOP EICAS ADVISORY: E1-2 HYD PUMP FAIL LIGHT: Master Caution INDICATION: Hydraulic pressure indication on MFD may be amber. Airspeed................
  • Page 492 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE Approach and landing configuration: Landing Gear ............DOWN Flaps ..............22° Airspeed.............. V REF 45 30 KIAS Use rudder for directional control on the ground. EMERGENCY BRAKE TECHNIQUE Procedure ........ACCOMPLISH Do not attempt to taxi.
  • Page 493 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE Do not actuate left Thrust Reverser. Use rudder and differential braking technique for directional control on ground. Approach and landing configuration: Landing Gear............DOWN Flaps................ 45° Airspeed ..............V REF 45 CAUTION: TO DETERMINE THE MINIMUM SUITABLE LANDING DISTANCE, MULTIPLY THE UNFACTORED LANDING DISTANCE FOR FLAPS 45°...
  • Page 494 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE Approach and landing configuration: Landing Gear ............DOWN Flaps ................45° Airspeed..............V REF 45 CAUTION: • DO NOT OPEN THE SPEED BRAKE. • TO DETERMINE THE MINIMUM SUITABLE LANDING DISTANCE, MULTIPLY THE UNFACTORED LANDING DISTANCE FOR FLAPS 45°...
  • Page 495 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL HYDRAULIC SYSTEM LOW QUANTITY EICAS ADVISORY: HYD1 (2) LO QTY INDICATION: Hydraulic fluid quantity indication on MFD may be amber. Monitor associated hydraulic system. NOTE: Do not open the Speed Brake if the Hydraulic System 2 is affected.
  • Page 496 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-03-48 REVISION 36...
  • Page 497 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL LANDING GEAR AND BRAKES GEAR LEVER CANNOT BE MOVED TO UP AFTER TAKEOFF CONDITION: Landing gear cannot be moved to up position after takeoff in the normal manner. Wait 10 seconds to verify if the LG AIR/GND FAIL message is displayed.
  • Page 498 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE If the failure persists: Free Fall Lever............ CYCLE Cycle the free fall lever as long as necessary, but limited to 10 times, to lower the landing gear. Wait 20 seconds, with the lever in the uplock position, between each cycle.
  • Page 499 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE NOTE: - The decision to land with all gear up or with any gear extended is left to pilots. The choice of configuration is made with basis on the number of gears available, airplane load distribution, controllability, and conditions of the landing field.
  • Page 500 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL LANDING GEAR AIR/GROUND SYSTEM FAILURE EICAS CAUTION: LG AIR/GND FAIL LIGHT: Master Caution If not in icing conditions: Icing Conditions ............AVOID Landing Configuration: Flaps ..............45° Airspeed.............. V REF 45 CAUTION: TO DETERMINE MINIMUM SUITABLE LANDING DISTANCE,...
  • Page 501 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL BRAKE OVERHEAT EICAS CAUTION: BRAKE OVERHEAT LIGHT: Master Caution If during landing and runway length is enough: Brake Pressure ............REDUCE Use of full reverse thrust is recommended. If after takeoff: Lower landing gear for cooling as soon as possible. Airspeed..............
  • Page 502 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL BRAKES INOPERATIVE EICAS CAUTION: BRK OUTBD (INBD) INOP LIGHT: Master Caution If one pair of brakes is inoperative, apply brakes normally through the pedals. If both pair of brakes are inoperative: EMERGENCY BRAKING TECHNIQUE Procedure........ACCOMPLISH In any case: Landing configuration: Flaps ..............
  • Page 503 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL BRAKES DEGRADED EICAS CAUTION: BRAKE DEGRADED LIGHT: Master Caution Apply brakes normally. Brake effectiveness may be reduced and braking asymmetry may be felt. During landing run: Thrust Levers (if available) ........REVERSE CAUTION: TO DETERMINE THE MINIMUM SUITABLE LANDING DISTANCE, MULTIPLY THE UNFACTORED LANDING DISTANCE FOR FLAPS 45°...
  • Page 504 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL STEERING SYSTEM INOPERATIVE UNCOMMANDED SWERVING ON GROUND EICAS CAUTION: STEER INOP (may be presented) LIGHT: Master Caution Steering Handwheel............DO NOT USE Steering Disengagement Button ........PRESS Control the airplane using differential brakes and rudder. Consider the use of differential thrust reverser if serviceable.

  • Page 505: Flight Controls

    AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL FLIGHT CONTROLS RUDDER/YAW TRIM RUNAWAY Quick Disconnect Button ..........PRESS AND HOLD Rudder Systems 1 and 2 ..........OFF Yaw Trim Circuit Breaker (F12) ........PULL Quick Disconnect Button ..........RELEASE Strongly push pedal opposite to the side of the uncommanded yaw, while applying ailerons to control roll.
  • Page 506 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL AILERON SYSTEM INOPERATIVE EICAS CAUTION: AIL SYS 1 (2) INOP LIGHT: Master Caution Associated Aileron System ........... OFF Airspeed ................ MAXIMUM 250 KIAS If the remaining system fails: Remaining Aileron System ........OFF Quick Disconnect Button ......... PRESS Aileron is operating under mechanical reversion mode.
  • Page 507 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL RUDDER HARDOVER PROTECTION FAILURE EICAS CAUTION: RUD HDOV PROTFAIL LIGHT: Master Caution On ground: Do not takeoff. In flight: Hardover protection is not available. RUDDER SYSTEM INOPERATIVE EICAS CAUTION: RUDDER SYS 1(2) INOP or RUDDER SYS 1-2 INOP LIGHT: Master Caution If only one rudder system is affected:...
  • Page 508 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL FLAP SYSTEM FAILURE (APPLICABLE TO ALL MODELS EXCEPT EMB-145 XR) EICAS CAUTION: FLAP FAIL LIGHT: Master Caution CONDITION: Flap operation is not possible. Flap position indication may be amber. Flaps may be at intermediate positions. Maintain airspeed according to the following: FLAPS POSITION MAXIMUM AIRSPEED...
  • Page 509 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL FLAP SYSTEM FAILURE (APPLICABLE TO EMB-145XR MODEL) EICAS CAUTION: FLAP FAIL LIGHT: Master Caution CONDITION: Flap operation is not possible. Flap position indication may be amber. Flaps may be at intermediate positions. Maintain airspeed according to the following: ABOVE 10000 ft FLAPS...
  • Page 510 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL SPEED BRAKE LEVER DISAGREE EICAS CAUTION: SPBK LVR DISAGREE LIGHT: Master Caution Speed Brake Lever ............CLOSE FLAP LOW ACTUATION SPEED EICAS ADVISORY: FLAP LOW SPEED Anticipate flap actuation. LOSS OF PITCH OR ROLL COMMAND CONDITION: Pitch or roll commands are not effective.
  • Page 511 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL AILERON ARTIFICIAL FEEL INOPERATIVE CONDITION: Control Wheel inputs become light and do not center by itself. Airspeed................ BELOW 200 KIAS Do not make sudden and large aileron inputs. RUDDER ARTIFICIAL FEEL INOPERATIVE CONDITION: Rudder pedals become extremely light and do not center by themselves.

  • Page 512: Autopilot

    ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL GUST LOCK FAILURE LIGHT: GUST LOCK (amber) On ground: Do not takeoff. In flight: Do not push control column full Nose Down. Avoid flying in turbulence conditions. Consider diversion. Avoid landing at airports with anticipated turbulence or crosswind. NOTE: This procedure is applicable only to airplanes equipped with electromechanical gust lock system.
  • Page 513 If the message persists, avoid or exit icing conditions. NOTE: Ice Detection Override Knob must be set to ALL at least 2 minutes after exiting icing conditions after CONDITION advisory message has disappeared. Page Code 1-03-56 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 514 ENGINE OR SINGLE BLEED OPERATION IN ICING CONDITIONS PROCEDURE. If BLD 1(2) VLV CLSD message is not displayed on the EICAS: Monitor the system for the remainder of the flight. Page Code 1-03-56 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 515 If the valve has failed open, associated to a duct leakage or engine overtemperature: Both Engine Bleeds ..........CLOSE APU Bleed ............... CLOSE Altitude..............MEA OR 10000ft, WHICHEVER IS HIGHER Icing Conditions ............EXIT/AVOID Page Code 1-03-56 REVISION 41 Copyright © by Embraer. Refer to cover page for details.

  • Page 516: Crew Awareness

    Pressurization Manual Controller......AS REQUIRED If necessary: Pressurization Manual Controller ....... FULL UP At least one bleed source, engines or APU, must be kept open. Page Code 1-03-56 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 517 Pressurization Manual Controller ......AS REQUIRED If required: Pressurization Manual Controller ....... FULL UP NOTE: At least one bleed source, engines or APU, must be kept open. Page Code 1-03-56 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 518 Pressurization Manual Controller......AS REQUIRED If required: Pressurization Manual Controller ....... FULL UP NOTE: At least one bleed source, engines or APU, must be kept open. Page Code 1-03-56 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 519 If it is not possible to open pack valve: Altitude..............MAX 25000 ft MINIMUM MEA If both packs are closed: Altitude..............MEA OR 10000 ft WHICHEVER IS HIGHER Page Code 1-03-56 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 520 If unsuccessful: Altitude ..............MEA OR 10000 ft, WHICHEVER IS HIGHER Pressurization Manual Controller......FULL DOWN Pressurization Mode Selector........AUTO Pressurization Dump Button ........PRESS Page Code 1-03-56 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 521 3800 26000 4100 27000 4400 28000 4700 29000 5000 30000 5400 31000 5700 32000 6100 33000 6500 34000 6800 35000 7200 36000 7600 37000 8000 Page Code 1-03-56 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 522 ADF 1 CB, DME 1 CB and VOR/ILS 1 CB......PULL Integrated Navigation Unit For INU 2: ADF 2 CB, DME 2 CB and VOR/ILS 2 CB......PULL CONTINUES ON NEXT PAGE Page Code 1-03-56 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 523 If the message remains, maintain a cross-check between main and standby instruments. In case a disagreement arises, assume the main instruments indication is unreliable and land at the nearest suitable airport. Page Code 1-03-56 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 524 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-03-56 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 525 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ICE PROTECTION SYSTEM WING ANTI-ICING FAILURE EICAS WARNING: ICE COND-A/I INOP EICAS CAUTION: WG 1 (2) A/ICE FAIL or WG A/ICE FAIL LIGHT: Master Warning and Master Caution Ice Detection Override Knob......... ALL Thrust Levers..............ADVANCE If failure persists: Wing Anti-Icing Button ..........
  • Page 526 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL STABILIZER ANTI-ICING FAILURE EICAS WARNING: ICE COND-A/I INOP EICAS CAUTION: STAB A/ICE FAIL LIGHT: Master Warning and Master Caution Ice Detection Override Knob ......... ALL Thrust Levers ..............ADVANCE If failure persists: Stabilizer Anti-Icing Button ........CYCLE If failure persists: Stabilizer Anti-Icing Button ........
  • Page 527 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ENGINE ANTI-ICING FAILURE EICAS WARNING: ICE COND-A/I INOP EICAS CAUTION: E1 (2) A/ICE FAIL LIGHT: Master Warning and Master Caution Thrust Levers..............ADVANCE If the message persists: Ice Detection Override Knob........ALL If the message still persists: Engine Air Inlet Anti-Icing Button ......
  • Page 528 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE Above 15000 ft: Anti-icing system performance decreases. If it is not possible to descend below 15000 ft, failure messages may be presented. In this case, exit icing conditions and refer to the appropriate approach and landing procedure.
  • Page 529 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ANTI-ICING ON WITHOUT ICING CONDITIONS EICAS CAUTION: NO ICE- A/ICE ON LIGHT: Master Caution Ice Detection Override Knob......... AUTO If the message persists, check the overhead panel and turn off all unnecessary anti-ice system. If the message persists and is associated with Wing or Stabilizer Anti- Icing System: Altitude..............
  • Page 530 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CLEAR ICE DETECTED (APPLICABLE TO EMB-145XR MODEL) EICAS CAUTION: CLR ICE 1 (2) LIGHT: CLR ICE 1(2) LIGHT: Master Caution Do not takeoff. Airplane de-icing is required. If there is no clear ice on the wing surface, disregard the message. CLEAR ICE DETECTION SYSTEM FAILURE (APPLICABLE TO EMB-145XR MODEL) EICAS CAUTION: CLR/I INOP 1 (2)
  • Page 531 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL PITOT SENSORS HEATING FAILURE EICAS CAUTION: PITOT 1 (2, 3) INOP LIGHT: Master Caution Information on the instruments supplied by the affected system may be unreliable. Cross-check and do not use the affected system if a disagreement is found.
  • Page 532 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-03-57 REVISION 40...
  • Page 533 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL OXYGEN CREW/PASSENGER OXYGEN LOW PRESSURE EICAS CAUTION: OXYGEN LO PRESS CREW (PAX) OXY LOW PRESS LIGHT: Master Caution INDICATION: Oxygen pressure may become red or amber on MFD. Check oxygen pressure on the MFD ECS Page. If message is confirmed or if MFD is not available: Altitude ................
  • Page 534 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-03-58 MARCH 30, 2001...
  • Page 535 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL NAVIGATION AHRS ALIGNMENT EICAS ADVISORY: AHRS 1 (2) ALN This message is normally presented during alignment phase. No action is required. AHRS ALIGNMENT FAULT EICAS CAUTION: AHRS 1 (2) ALN FAULT LIGHT: Master Caution Check and reenter present position. If necessary, reenter present position once again.
  • Page 536 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL AHRS FAIL EICAS CAUTION: AHRS 1 (2) FAIL LIGHT: Master Caution Associated AHRS Reversionary Button......PRESS NOTE: The Autopilot is not available. AHRS NO MAGNETIC HEADING EICAS ADVISORY: AHRS 1 (2) NO MAG HDG Enter Magnetic Heading. AHRS NO PRESENT POSITION EICAS ADVISORY: AHRS 1 (2) NO PPOS Enter Present Position.
  • Page 537 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL CENTRAL MAINTENANCE COMPUTER FAILURE EICAS ADVISORY: CMC FAIL Crew awareness. CHECK IC SOFTWARE EICAS CAUTION: CHECK IC 1 (2) SW LIGHT: Master Caution Do not takeoff. CHECKLIST MISMATCH EICAS ADVISORY: CHECKLIST MISMATCH Do not use Checklist Display. DAU AIRPLANE ID MISCOMPARE EICAS CAUTION: DAU AC ID MISCMP Do not takeoff.
  • Page 538 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL For DAU 2 A FAIL caution message proceed: DAU 2 Reversion ............. ON Check DAU 2 REVERSION message on EICAS. NOTE: The following indications and messages will not be available: - Indications: Engine (temperature pressure), Hydraulic quantity 1 and 2, yaw trim position, cabin temperature, Bleed 2 temperature.
  • Page 539 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL DAU MISCOMPARE EICAS CAUTION: DAU 1 (2) ENG MISCOMP or DAU 1 (2) SYS MISCOMP or DAU 1 (2) WRN MISCOMP LIGHT: Master Caution Associated DAU Reversion .......... ON Check associated DAU REVERSION message on EICAS. NOTE: For each miscompare message and each side, check the following parameters before and after the reversion: - Engine: N1, N2, ITT.
  • Page 540 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL DISPLAY FAN FAILURE EICAS ADVISORY: DU 1 (2, 3, 4, 5) FAN FAIL An overheat condition may arise in the associated display. In this case, it will be shut down automatically. Use reversionary capabilities. DISPLAY OVERHEAT EICAS ADVISORY: DU 1 (2, 3, 4, 5) OVHT An overheat condition may arise in the associated display.
  • Page 541 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL FMS NAVIGATION PERFORMANCE DEGRADED / FMS IN DEAD RECKONING MODE Verify airplane position by using VOR/DME information (enroute and terminal operations) or other sources as appropriate (oceanic). If conducting an instrument approach, discontinue use of FMS for approach guidance and select an alternate source of navigation, if available.
  • Page 542 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL GPS FAILED In case of GPS fail (GPS FAILED Scratchpad Message for single GPS or GPS 1 FAILED and GPS 2 FAILED Scratchpad Messages for dual GPS) associated with FMS Navigation Performance Degraded: FMS NAVIGATION PERFORMANCE DEGRADED / FMS IN DEAD RECKONING MODE Abnormal Procedure ........Accomplish In case of GPS fail (GPS FAILED Scratchpad Message for single GPS...
  • Page 543 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL IC FAILURE/IC BUS FAILURE EICAS CAUTION: IC BUS FAIL may be presented LIGHT: Master Caution if IC BUS FAIL message is presented CONDITION: Associated Display Units blank and with a red X drawn over them. The following features will be inoperative: - EICAS messages miscompare monitoring, - Takeoff speeds synchronization,...
  • Page 544 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE SG 2 Button ............. PRESS If smoke persists: ELECTRICAL SYSTEM FAILURE OR SMOKE Procedure ....ACCOMPLISH Page Code 1-03-59 REVISION 40...
  • Page 545 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL IC’S CONFIGURATION MISMATCH EICAS CAUTION: CHK IC CONFIG with Master Caution Light or EICAS ADVISORY: CONFIG MISMATCH Do not take off. INTEG ANNUNCIATOR ON (UNS-1K) Discontinue the use of FMS whenever using the GPS source solely. If possible and feasible, select an alternate source of navigation for approach guidance.
  • Page 546 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL IRS EXCESSIVE MOTION EICAS ADVISORY: IRS 1 (2) EXC MOTION Make sure the airplane is completely stationary. The IRU will restart a full alignment 30 seconds after the motion is stopped. IRS FAIL EICAS CAUTION: IRS 1 (2) FAIL During power on or alignment phases: IRU Mode Select Switch ..........
  • Page 547 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL IRS ON BATTERY EICAS ADVISORY: IRS 1 (2) ON BATT Associated IRU will operate for 40 minutes. IRS OVERHEAT EICAS CAUTION: IRS 1 (2) OVERHEAT Operate affected IRU until completion of the flight. If MSU FAULT annunciator is lighted, IRS 1 (2) FAIL message is presented or inertial data ceases to be transmitted by IRU: Associated IRS Reversionary Button ......
  • Page 548 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL IRS/MSU FAILURE ANNUNCIATION OPERATION PHASE LIGHT POWER ON ALIGNMENT IN FLIGHT  Flashes  Flashes:  No light:  Check immediately after  Select entry: CB’s. remaining  Check  Set by pressing the mode reenter latitude IRS Button on select switch to...
  • Page 549 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL IRS/MSU FAILURE ANNUNCIATION (Continued) OPERATION PHASE LIGHT POWER ON ALIGNMENT IN FLIGHT   The IRU operates Check IRS CB’s. backup  If the annunciator power will ON BATT remains lighted, ******* operate do not takeoff. minutes.
  • Page 550 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL MESSAGE MISCOMPARISON INDICATION: CAS MSG indication on PFD. Pilot’s MFD Selector Knob ..........EICAS Copilot’s MFD Selector Knob........EICAS Compare the messages displayed on the copilot’s MFD with the messages presented on the pilot’s MFD to check which is the discrepant message.
  • Page 551 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL NAV/FLIGHT INSTRUMENTS FAILURE (Continued) ANNUNCIATO LOCATION ACTION R/FAILURE VS (red) Use cross-side vertical speed by pressing button associated reversionary panel. ROL, PIT, ATT, Compare data with Standby Indicator. IAS or ALT altitude compare (amber) altimeters setting also. If required, use cross-side data pressing...
  • Page 552 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL NAV/FLIGHT INSTRUMENTS FAILURE (Continued) ANNUNCIATOR LOCATION ACTION /FAILURE MENU INOP Crew awareness. (amber) ATT:CAGE Press the CAGE push button in order to recover attitude indication. (amber) Caging the ISIS in flight will result in loss of attitude indication for up to 10 seconds and the amber message ATT 10s will be presented during this ISIS...
  • Page 553 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL AUTOPILOT AUTOPILOT TRIM FAILED EICAS CAUTION: AUTO TRIM FAIL LIGHT: Master Caution Control Column ............. HOLD FIRMLY Quick Disconnect Button..........PRESS Pitch Trim ..............AS REQUIRED Trim the airplane. Autopilot ................ AS REQUIRED STABILIZER OUT OF TRIM EICAS CAUTION: AP ELEV MISTRIM LIGHT: Master Caution CONDITION: Autopilot is engaged and pitch servo is holding force.
  • Page 554 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL FD VERTICAL MODE FAILURE EICAS CAUTION: VERTICAL MODE OFF LIGHT: Master Caution The Flight Director has been reverted to the basic pitch mode. At crew discretion, re-select the Flight Director affected mode or select another mode. NOTE: - 5 seconds after pressing the Master Caution, the message will be removed.
  • Page 555 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CAT II OPERATION HARDOVER If any unusual acceleration or motion is noticed on the airplane flight path the approach must be discontinued, and: Autopilot ..............DISENGAGE MISSED APPROACH Procedure ......PERFORM AS REQUIRED − Consider the possibility of continuing and performing the landing if adequate visual reference has been established to assure the airplane position and approach path.
  • Page 556 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL ENGINE FAILURE ON FINAL APPROACH OR DURING GO-AROUND ONE ENGINE INOPERATIVE GO-AROUND Procedure........APPLY AUTOPILOT MALFUNCTION BEFORE REACHING OUTER MARKER If the autopilot disengages or has to be disengaged, transfer autopilot and reengage it. The pilot on-side of the engaged autopilot may continue the approach.
  • Page 557 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL DISPLAY WARNINGS DURING FINAL APPROACH Discontinue the approach if any of the following warnings occur: - CAT 2 (not displayed or amber) - AURAL WARN FAIL (amber) - RAD ALT FAIL (cyan) (for airplanes Post-Mod. SB 145-31-0020 or with an equivalent modification factory incorporated) - RA (amber) - GS (red or amber)
  • Page 558 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL EXCESSIVE DEVIATION WARNING If warning occurs above 200 ft Radio Altitude: Monitor the ILS deviation to ensure that the airplane returns to the center beam. If not recovered up to 200 ft radio altitude: Discontinue the approach. If warning occurs below 200 ft Radio Altitude: Discontinue the approach.
  • Page 559 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL HGS OPERATION For AIII mode operations, the approach must be discontinued in the event of engine failure above DH. A new approach may be attempted with one engine inoperative. In this case, the normal procedure AIII approach contained in HGS Operation must be used.
  • Page 560 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-03-66 REVISION 40...
  • Page 561 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL MISCELLANEOUS IMPAIRED OR CRACKED WINDSHIELD Associated Windshield Heating ........OFF If only the outer layer (glass) is cracked, no action is required. If not, proceed as follows: Cockpit Door ............CLOSE Altitude..............MEA OR BELOW 10000 ft, WHICHEVER IS HIGHER...
  • Page 562 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL EMB-145 LIGHTNING STRIKE INCIDENT REPORT Part I (to be completed by flight crew) Conditions at time of strike: • Operator: Date of incident: • ACFT S/N: Flight no.: • Route: From • Altitude: Airspeed: • Flight phase: Approach Climb Level Flight...
  • Page 563 AIRPLANE ABNORMAL PROCEDURES OPERATIONS MANUAL BIRD IMPACT Against windshield: CRACKED WINDSHIELD Procedure...... APPLY Against leading edge (wing or tail) or fuselage: Maneuverability may be reduced. Refer to the associated leading edge deicer failure procedure, if necessary. At a safe altitude, perform a controllability check step by step up to the landing configuration.
  • Page 564 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL LANDING BELOW -40°C Before touchdown: Rate of descent............LESS THAN 300 ft/MIN OVERWEIGHT LANDING Before touchdown: Rate of Descent ............MAXIMUM 300 FT/MIN Touch smoothly the runway surface. Reduce the engine thrust only after the touchdown. CAUTION: TO DETERMINE THE MINIMUM SUITABLE LANDING DISTANCE, MULTIPLY THE UNFACTORED LANDING DISTANCE FOR FLAPS 45°...
  • Page 565 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL UNRELIABLE AIRSPEED CONDITION: Airspeed indications are erroneous or unreliable. Autopilot/Yaw Damper ..........DISENGAGE Both Flight Directors ............. OFF If speed indication on both PFD is below 135 kt: Rudder Shutoff Sys 1 ..........PUSH OUT Avoid using the speed brake.
  • Page 566 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL UNRELIABLE AIRSPEED TABLES Airplane: EMB-135 Engine: AE3007A3 Anti-Ice: OFF CLB THRUST MODE WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 Pitch (deg) (240 KIAS) V/S (ft/min) 4100 3400 2900 2400 10000 Pitch (deg) (240 KIAS) V/S (ft/min) 3100 2500...
  • Page 567 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-135 Engine: AE3007A3 Anti-Ice: OFF FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 Pitch (deg) (240 KIAS) V/S (ft/min) -1800 -1700 -1600 -1600 10000 Pitch (deg) (240 KIAS)
  • Page 568 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-135 Engine: AE3007A3 Anti-Ice: OFF Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 48.5 52.3...
  • Page 569 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-135 Engine: AE3007A3 Anti-Ice: ON CLB THRUST MODE WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 Pitch (deg) (240 KIAS) V/S (ft/min) 4000 3300 2800 2300 10000 Pitch (deg) (240 KIAS)
  • Page 570 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-135 Engine: AE3007A3 Anti-Ice: ON FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 Pitch (deg) (240 KIAS) V/S (ft/min) -1000 -1000 -1000 -1000 10000 Pitch (deg) (240 KIAS)
  • Page 571 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-135 Engine: AE3007A3 Anti-Ice: ON Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 48.6 52.3...
  • Page 572 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-135 Engine: AE3007A1/3 Anti-Ice: OFF CLB THRUST MODE WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 Pitch (deg) (240 KIAS) V/S (ft/min) 4800 4000 3400 2900 10000 Pitch (deg) (240 KIAS)
  • Page 573 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-135 Engine: AE3007A1/3 Anti-Ice: OFF FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 Pitch (deg) (240 KIAS) V/S (ft/min) -1800 -1700 -1600 -1600 10000 Pitch (deg) (240 KIAS)
  • Page 574 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-135 Engine: AE3007A1/3 Anti-Ice: OFF Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 48.9 52.5...
  • Page 575 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-135 Engine: AE3007A1/3 Anti-Ice: ON CLB THRUST MODE WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 Pitch (deg) (240 KIAS) V/S (ft/min) 4700 3900 3400 2800 10000 Pitch (deg) (240 KIAS)
  • Page 576 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-135 Engine: AE3007A1/3 Anti-Ice: ON FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 Pitch (deg) (240 KIAS) V/S (ft/min) -900 -900 -900 -900 10000 Pitch (deg) (240 KIAS)
  • Page 577 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-135 Engine: AE3007A1/3 Anti-Ice: ON Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 48.9 52.5...
  • Page 578 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-140 Engine: AE3007A1/3 Anti-Ice: OFF CLB THRUST MODE WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 Pitch (deg) (240 KIAS) V/S (ft/min) 4800 4000 3400 2900 2500 10000...
  • Page 579 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-140 Engine: AE3007A1/3 Anti-Ice: OFF FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 Pitch (deg) (240 KIAS) V/S (ft/min) -1800 -1700 -1600 -1500 -1500 10000 Pitch (deg)
  • Page 580 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-140 Engine: AE3007A1/3 Anti-Ice: OFF Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 48.9 52.5...
  • Page 581 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-140 Engine: AE3007A1/3 Anti-Ice: ON CLB THRUST MODE WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 Pitch (deg) (240 KIAS) V/S (ft/min) 4700 3900 3400 2900 2500 10000...
  • Page 582 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-140 Engine: AE3007A1/3 Anti-Ice: ON FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 Pitch (deg) (240 KIAS) V/S (ft/min) -900 -900 -900 -900 -900 10000...
  • Page 583 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-140 Engine: AE3007A1/3 Anti-Ice: ON Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 48.9 52.5...
  • Page 584 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A Anti-Ice: OFF CLB THRUST MODE WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 Pitch (deg) (240 KIAS) V/S (ft/min) 3800 3100 2700 2200 1900 10000...
  • Page 585 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A Anti-Ice: OFF FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 Pitch (deg) (240 KIAS) V/S (ft/min) -1800 -1700 -1600 -1500 -1500 10000...
  • Page 586 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A Anti-Ice: OFF Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 48.2 52.2...
  • Page 587 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A Anti-Ice: ON CLB THRUST MODE WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 Pitch (deg) (240 KIAS) V/S (ft/min) 3800 3100 2700 2200 1900 10000...
  • Page 588 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A Anti-Ice: ON FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 Pitch (deg) (240 KIAS) V/S (ft/min) -1800 -1700 -1600 -1500 -1500 10000...
  • Page 589 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A Anti-Ice: ON Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 48.2 52.2...
  • Page 590 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A1/1 Anti-Ice: OFF CLB THRUST MODE WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 Pitch (deg) (240 KIAS) V/S (ft/min) 4600 3800 3300 2700 2400 10000...
  • Page 591 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A1/1 Anti-Ice: OFF FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 Pitch (deg) (240 KIAS) V/S (ft/min) -1800 -1700 -1600 -1500 -1500 10000...
  • Page 592 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A1/1 Anti-Ice: OFF Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 48.0 51.8...
  • Page 593 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A1/1 Anti-Ice: ON CLB THRUST MODE WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 Pitch (deg) (240 KIAS) V/S (ft/min) 4600 3800 3300 2700 2400 10000...
  • Page 594 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A1/1 Anti-Ice: ON FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 Pitch (deg) (240 KIAS) V/S (ft/min) -1800 -1700 -1600 -1500 -1500 10000...
  • Page 595 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A1/1 Anti-Ice: ON Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 48.0 51.8...
  • Page 596 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A1&A1P Anti-Ice: OFF CLB THRUST MODE PRESSURE ALTITUDE WEIGHT (lb) (ft) 30000 35000 40000 45000 50000 55000 Pitch (deg) (240 KIAS) V/S (ft/min) 4800 4000 3400 2900 2500...
  • Page 597 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A1&A1P Anti-Ice: OFF FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 55000 Pitch (deg) (240 KIAS) V/S (ft/min) -1800 -1700 -1600 -1500 -1500 -1500 10000 Pitch (deg) (240 KIAS)
  • Page 598 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A1&A1P Anti-Ice: OFF Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 48.9 52.5...
  • Page 599 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A1&A1P Anti-Ice: ON CLB THRUST MODE PRESSURE ALTITUDE WEIGHT (lb) (ft) 30000 35000 40000 45000 50000 55000 Pitch (deg) (240 KIAS) V/S (ft/min) 4700 3900 3400 2900 2500...
  • Page 600 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A1&A1P Anti-Ice: ON FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 55000 Pitch (deg) (240 KIAS) V/S (ft/min) -900 -900 -900 -900 -900...
  • Page 601 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145 Engine: AE3007A1&A1P Anti-Ice: ON Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 48.9 52.5...
  • Page 602 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145XR Engine: AE3007A1E Anti-Ice: OFF CLB THRUST MODE WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 55000 Pitch (deg) (240 KIAS) V/S (ft/min) 4000 3400 3000 2600 2300...
  • Page 603 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145XR Engine: AE3007A1E Anti-Ice: OFF FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 55000 Pitch (deg) (240 KIAS) V/S (ft/min) -3000 -2800 -2500 -2300 -2100 -2000 10000 Pitch (deg) (240 KIAS)
  • Page 604 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145XR Engine: AE3007A1E Anti-Ice: OFF Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 51.4 54.8...
  • Page 605 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145XR Engine: AE3007A1E Anti-Ice: ON CLB THRUST MODE WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 55000 Pitch (deg) (240 KIAS) V/S (ft/min) 3800 3300 2900 2500 2200...
  • Page 606 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB- Engine: AE3007A1E Anti-Ice: ON 145XR FLIGHT IDLE DESCENT WEIGHT (lb) PRESSURE ALTITUDE (ft) 30000 35000 40000 45000 50000 55000 Pitch (deg) (240 KIAS) V/S (ft/min) -2400 -2000 -1800 -1700 -1600 -1500 10000 Pitch (deg) (240 KIAS)
  • Page 607 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL CONTINUED FROM PREVIOUS PAGE UNRELIABLE AIRSPEED TABLES Airplane: EMB-145XR Engine: AE3007A1E Anti-Ice: ON Terminal Area (5000 ft) - %N1 for Level Flight WEIGHT (lb) Flap position + INCREMENT) 30000 35000 40000 45000 Pitch (deg) + 30) N1 (%) 51.4 54.8...
  • Page 608 ABNORMAL AIRPLANE PROCEDURES OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-03-70 REVISION 38...
  • Page 609 EMERGENCY PROFILES AIRPLANE OPERATIONS MANUAL EMERGENCY PROFILES Page Code 1-03-95 SEPTEMBER 29, 2000...
  • Page 610 EMERGENCY PROFILES AIRPLANE OPERATIONS MANUAL Page Code 1-03-95 SEPTEMBER 29, 2000...
  • Page 611 EMERGENCY PROFILES AIRPLANE OPERATIONS MANUAL Page Code 1-03-95 SEPTEMBER 29, 2000...
  • Page 612 EMERGENCY PROFILES AIRPLANE OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-03-95 APRIL 28, 2000...
  • Page 613 ABNORMAL PROFILES AIRPLANE OPERATIONS MANUAL ABNORMAL PROFILES Page Code 1-03-97 REVISION 24...
  • Page 614 ABNORMAL PROFILES AIRPLANE OPERATIONS MANUAL Page Code 1-03-97 REVISION 25...
  • Page 615 ABNORMAL PROFILES AIRPLANE OPERATIONS MANUAL Page Code 1-03-97 DECEMBER 20, 2002...
  • Page 616 ABNORMAL PROFILES AIRPLANE OPERATIONS MANUAL Page Code 1-03-97 DECEMBER 20, 2002...
  • Page 617 PERFORMANCE AIRPLANE OPERATIONS MANUAL SECTION 1-04 PERFORMANCE TABLE OF CONTENTS Page Block Introduction ................1-04-00 Noise Levels................1-04-03 Wind and Altitude Conversion............ 1-04-05 Thrust Setting Tables ..............1-04-10 Takeoff ..................1-04-15 Supplementary Takeoff Information........... 1-04-20 Approach..................1-04-25 Landing ..................1-04-30 Landing Information for Stockholm-Bromma (ESSB) Airport (*)................

  • Page 618: Introduction

    PERFORMANCE AIRPLANE OPERATIONS MANUAL INTRODUCTION This section presents takeoff, approach and landing performance information. For determination of the takeoff and landing limiting weights, the performance data as presented in the approved Airplane Flight Manual (AFM) or Runway Analysis Software must be used. Page Code 1-04-00...
  • Page 619 PERFORMANCE AIRPLANE OPERATIONS MANUAL NOISE LEVELS The following Effective Perceived Noise Levels comply with RBHA 36, 14 CFR Part 36, and ICAO Annex 16 Volume I, Chapter 3. The values below are stated for reference conditions of standard atmosphere pressure at sea level, 25°C ambient temperature, 70% relative humidity, and zero wind.

  • Page 620: Noise Levels

    PERFORMANCE AIRPLANE OPERATIONS MANUAL NOISE LEVEL IN EPNdb Airplane Noise CONDITION Level Sideline Takeoff Approach Maximum 94.0 89.0 98.0 Allowable EMB-145 Actual 85.0 80.1 92.6 EP model EMB-145 Actual 85.1 79.8 92.6 ER model EMB-145 Actual 85.1 79.2 92.6 EU model EMB-145 Actual 85.1...
  • Page 621 PERFORMANCE AIRPLANE OPERATIONS MANUAL 5) For airplanes Post-Mod. SB 145-53-0065 or equipped with an equivalent modification factory incorporated, the actual noise level for Sideline condition is 85.0 EPNdB and for Takeoff condition is 80.5 EPNdB. 6) For airplanes Post-Mod. SB 145-53-0066 or equipped with an equivalent modification factory incorporated, the actual noise level for Sideline condition is 84.9 EPNdB.
  • Page 622 PERFORMANCE AIRPLANE OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-04-03 REVISION 34...

  • Page 623: Wind And Altitude Conversion

    PERFORMANCE AIRPLANE OPERATIONS MANUAL WIND AND ALTITUDE CONVERSION Page Code 1-04-05 DECEMBER 20, 2002...
  • Page 624 PERFORMANCE AIRPLANE OPERATIONS MANUAL Enter the chart with the reported wind velocity and the relative angle to the runway, to read the wind component parallel to the runway and the crosswind. EXAMPLE Given: Wind velocity ............20 kt Wind direction ............60° Determine: Wind component parallel to the runway ....
  • Page 625 PERFORMANCE AIRPLANE OPERATIONS MANUAL ALTIMETER SETTING TO STATION PRESSURE QNH TO PRESSURE ALTITUDE CORRECTION in Hg TO ELEVATION FOR PRES. ALT. (FT) 28.81 to 28.91 976 to 979 1000 28.92 to 29.02 980 to 983 29.03 to 29.12 984 to 986 29.13 to 29.23 987 to 990 29.24 to 29.34...
  • Page 626 PERFORMANCE AIRPLANE OPERATIONS MANUAL QFE TO STATION PRESSURE PRESSURE PRESSURE in Hg ALTITUDE in Hg ALTITUDE (ft) (ft) 31.01 1050 -989 25.55 4313 30.86 1045 -856 25.40 4468 30.71 1040 -723 25.25 4625 30.57 1035 -589 25.10 4781 30.42 1030 -454 24.96 4939...
  • Page 627 PERFORMANCE AIRPLANE OPERATIONS MANUAL GEOMETRIC HEIGHT TO PRESSURE HEIGHT Pressure altimeters are calibrated to indicate true altitude under International Standard Atmosphere (ISA) conditions. Any deviation from ISA will therefore result in an erroneous reading on the altimeter. In the case when the temperature is higher than ISA the true altitude will be higher than the figure indicated by the altimeter, and the true altitude will be lower when the temperature is lower than ISA.
  • Page 628 PERFORMANCE AIRPLANE OPERATIONS MANUAL Example: Airport elevation: ..............1500 ft Airport Temperature............-20 Obstacle Height above airport elevation ......800 ft Altimeter adjusted to airport QNH (on ground altimeter reads 1500 ft). Enter table with 800 ft and -20 C and read 100 ft. So, when the airplane reaches the obstacle geometric height, the altimeter will read 1500 + 800 + 100 = 2400 ft Altimeters read...

  • Page 629: Thrust Setting Tables

    PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL THRUST SETTING TABLES Thrust settings tables are presented for various pressure altitudes and static air temperatures, with engine bleed closed or open, and anti-ice on or off. The tables present the following data: • N1 for T/O-1 mode.
  • Page 630 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR T/O-1 MODE ANTI-ICE OFF AIRSPEED: 0 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -54 -50 -45 -40 -35 -30 -25 -20 -15 -10 -1000 74.8 75.5 76.4 77.2 78.0 78.8 79.6 80.4 81.2 82.0 82.8 75.5 76.1 77.0 77.8 78.7 79.5 80.3 81.1 81.9 82.7 83.5 1000 76.5 77.2 78.0 78.9 79.7 80.6 81.4 82.2 83.0 83.8 84.6...
  • Page 631 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR T/O-1 MODE ANTI-ICE OFF AIRSPEED: 0 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -1000 83.6 84.3 85.1 85.8 86.6 87.3 88.0 88.8 89.5 90.2 90.3 84.2 85.0 85.8 86.5 87.3 88.0 88.8 89.5 90.2 90.9 90.8 1000 85.4 86.2 86.9 87.7 88.5 89.2 90.0 90.7 91.4 91.4 90.1 2000...
  • Page 632 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR ALT T/O-1 MODE ANTI-ICE OFF AIRSPEED: 0 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -54 -50 -45 -40 -35 -30 -25 -20 -15 -10 -1000 72.3 72.9 73.7 74.6 75.3 76.1 76.9 77.7 78.4 79.2 79.9 72.9 73.5 74.3 75.1 75.9 76.7 77.5 78.3 79.1 79.8 80.6 1000 73.7 74.4 75.2 76.1 76.9 77.7 78.5 79.2 80.0 80.8 81.6...
  • Page 633 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR ALT T/O-1 MODE ANTI-ICE OFF AIRSPEED: 0 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -1000 80.7 81.4 82.2 82.9 83.6 84.3 85.0 85.7 86.4 87.1 87.3 81.3 82.1 82.8 83.5 84.3 85.0 85.7 86.4 87.1 87.7 87.5 1000 82.3 83.1 83.8 84.5 85.3 86.0 86.7 87.4 88.1 88.1 86.9 2000...
  • Page 634 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR GO-AROUND ANTI-ICE OFF AIRSPEED: 100 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -54 -50 -45 -40 -35 -30 -25 -20 -15 -10 -1000 74.9 75.6 76.4 77.2 78.1 78.9 79.7 80.5 81.3 82.1 82.8 75.5 76.2 77.1 77.9 78.7 79.5 80.4 81.2 82.0 82.8 83.5 1000 76.5 77.2 78.1 78.9 79.7 80.6 81.4 82.2 83.0 83.8 84.6...
  • Page 635 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR GO-AROUND ANTI-ICE OFF AIRSPEED: 100 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -1000 83.6 84.4 85.1 85.9 86.6 87.3 88.1 88.8 89.5 90.2 90.5 84.3 85.1 85.8 86.6 87.3 88.1 88.8 89.5 90.3 90.9 90.7 1000 85.4 86.2 87.0 87.7 88.5 89.2 90.0 90.7 91.4 91.5 89.9 2000...
  • Page 636 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR GO-AROUND ANTI-ICE OFF AIRSPEED: 150 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -54 -50 -45 -40 -35 -30 -25 -20 -15 -10 -1000 74.8 75.5 76.3 77.2 78.0 78.8 79.6 80.4 81.2 82.0 82.8 75.4 76.1 77.0 77.8 78.7 79.5 80.3 81.1 81.9 82.7 83.5 1000 76.4 77.1 78.0 78.8 79.7 80.5 81.3 82.1 82.9 83.7 84.5...
  • Page 637 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR GO-AROUND ANTI-ICE OFF AIRSPEED: 150 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -1000 83.5 84.3 85.1 85.8 86.5 87.3 88.0 88.7 89.4 90.2 90.4 84.2 85.0 85.8 86.5 87.3 88.0 88.7 89.5 90.2 90.8 90.6 1000 85.3 86.1 86.9 87.6 88.4 89.1 89.9 90.6 91.4 91.3 89.7 2000...
  • Page 638 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR GO-AROUND ANTI-ICE OFF AIRSPEED: 200 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -54 -50 -45 -40 -35 -30 -25 -20 -15 -10 -1000 74.6 75.2 76.1 76.9 77.7 78.5 79.3 80.1 80.9 81.7 82.5 75.2 75.9 76.7 77.6 78.4 79.2 80.0 80.8 81.6 82.4 83.2 1000 76.2 76.9 77.8 78.6 79.5 80.3 81.1 81.9 82.7 83.5 84.3...
  • Page 639 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR GO-AROUND ANTI-ICE OFF AIRSPEED: 200 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -1000 83.2 84.0 84.7 85.5 86.2 87.0 87.7 88.4 89.1 89.8 89.8 83.9 84.7 85.5 86.2 87.0 87.7 88.4 89.2 89.9 90.6 90.3 1000 85.1 85.9 86.7 87.4 88.2 88.9 89.7 90.4 91.1 91.1 89.3 2000...
  • Page 640 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR MAXIMUM CONTINUOUS MODE ANTI-ICE OFF AIRSPEED: 100 KCAS ROLLS ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -65 -60 -54 -50 -45 -40 -35 -30 -25 -20 -15 -10 71.2 72.1 73.1 73.7 74.6 75.4 76.2 77.0 77.8 78.5 79.3 80.1 80.8 2000 72.9 73.8 74.9 75.5 76.4 77.2 78.0 78.8 79.6 80.4 81.2 82.0 82.8...
  • Page 641 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR MAXIMUM CONTINUOUS MODE ANTI-ICE OFF AIRSPEED: 100 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) 81.6 82.3 83.1 83.8 84.5 85.2 85.9 86.6 87.3 88.0 87.8 2000 83.6 84.3 85.1 85.8 86.6 87.3 88.0 88.8 88.9 88.0 87.2 4000 85.7 86.5 87.3 88.1 88.8 89.6 90.1 89.4 88.8 88.1 87.9 6000...
  • Page 642 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR MAXIMUM CONTINUOUS MODE ANTI-ICE OFF AIRSPEED: 150 KCAS ROLLS ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -65 -60 -54 -50 -45 -40 -35 -30 -25 -20 -15 -10 71.2 72.1 73.1 73.8 74.6 75.4 76.2 77.0 77.8 78.6 79.3 80.1 80.9 2000 73.0 73.9 74.9 75.6 76.4 77.3 78.1 78.9 79.7 80.5 81.3 82.1 82.9...
  • Page 643 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR MAXIMUM CONTINUOUS MODE ANTI-ICE OFF AIRSPEED: 150 KCAS ROLLS ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -1000 81.0 81.7 82.4 83.1 83.9 84.6 85.3 86.0 86.7 87.3 87.6 81.6 82.4 83.1 83.8 84.5 85.3 86.0 86.7 87.4 88.0 87.8 1000 82.6 83.4 84.1 84.9 85.6 86.3 87.0 87.8 88.5 88.4 86.8...
  • Page 644 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR MAXIMUM CONTINUOUS MODE ANTI-ICE OFF AIRSPEED: 200 KCAS ROLLS ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -65 -60 -54 -50 -45 -40 -35 -30 -25 -20 -15 -10 71.1 72.0 73.0 73.6 74.5 75.3 76.1 76.9 77.7 78.4 79.2 80.0 80.7 2000 73.1 74.0 75.0 75.7 76.5 77.4 78.2 79.0 79.8 80.6 81.4 82.2 83.0...
  • Page 645 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR MAXIMUM CONTINUOUS MODE ANTI-ICE OFF AIRSPEED: 200 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) 81.5 82.2 83.0 83.7 84.4 85.1 85.8 86.5 87.2 87.8 87.6 2000 83.7 84.5 85.2 86.0 86.7 87.5 88.2 88.9 89.1 87.8 86.6 4000 86.0 86.7 87.5 88.3 89.0 89.8 90.2 89.6 88.9 88.0 87.6 6000...
  • Page 646 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR T/O-1 MODE ANTI-ICE ON AIRSPEED: 0 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -40 -35 -30 -25 -20 -15 -10 -1000 78.3 79.2 80.0 80.8 81.6 82.4 83.2 84.0 83.6 84.3 85.1 79.0 79.8 80.6 81.5 82.3 83.1 83.9 84.7 84.2 85.0 85.8 1000 80.0 80.9 81.7 82.6 83.4 84.2 85.0 85.8 85.4 86.2 86.9...
  • Page 647 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR ALT T/O-1 MODE ANTI-ICE ON AIRSPEED: 0 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -40 -35 -30 -25 -20 -15 -10 -1000 75.7 76.5 77.3 78.1 78.9 79.6 80.4 81.2 80.7 81.4 82.2 76.3 77.1 77.9 78.7 79.5 80.3 81.0 81.8 81.3 82.1 82.8 1000 77.2 78.0 78.8 79.6 80.4 81.2 82.0 82.8 82.3 83.1 83.8...
  • Page 648 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR GO-AROUND ANTI-ICE ON AIRSPEED: 100 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -40 -35 -30 -25 -20 -15 -10 -1000 78.4 79.2 80.0 80.9 81.7 82.5 83.3 84.1 83.6 84.4 85.1 79.0 79.9 80.7 81.5 82.4 83.2 84.0 84.8 84.3 85.1 85.8 1000 80.0 80.9 81.7 82.6 83.4 84.2 85.0 85.8 85.4 86.2 87.0...
  • Page 649 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR GO-AROUND ANTI-ICE ON AIRSPEED: 150 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -45 -40 -35 -30 -25 -20 -15 -10 -1000 77.5 78.3 79.2 80.0 80.8 81.6 82.4 83.2 84.0 83.5 84.3 85.1 78.1 79.0 79.8 80.6 81.5 82.3 83.1 83.9 84.7 84.2 85.0 85.8 1000 79.1 80.0 80.8 81.7 82.5 83.3 84.1 85.0 85.8 85.3 86.1 86.9...
  • Page 650 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR GO-AROUND ANTI-ICE ON AIRSPEED: 200 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -40 -35 -30 -25 -20 -15 -10 -1000 78.1 78.9 79.7 80.5 81.3 82.1 82.9 83.7 83.2 84.0 84.7 78.7 79.5 80.4 81.2 82.0 82.8 83.6 84.4 83.9 84.7 85.5 1000 79.8 80.6 81.5 82.3 83.1 83.9 84.8 85.6 85.1 85.9 86.7...
  • Page 651 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR MAXIMUM CONTINUOUS MODE ANTI-ICE ON AIRSPEED: 100 KCAS ROLLS-ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -40 -35 -30 -25 -20 -15 -10 76.5 77.3 78.1 78.9 79.7 80.5 81.3 82.1 81.6 82.3 83.1 2000 78.3 79.2 80.0 80.8 81.6 82.4 83.2 84.0 83.6 84.3 85.1 4000...
  • Page 652 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR MAXIMUM CONTINUOUS MODE ANTI-ICE ON AIRSPEED: 150 KCAS ROLLS ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -40 -35 -30 -25 -20 -15 -10 76.5 77.4 78.2 79.0 79.8 80.5 81.3 82.1 81.6 82.4 83.1 2000 78.4 79.3 80.1 80.9 81.7 82.5 83.3 84.1 83.7 84.4 85.2 4000...
  • Page 653 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL N1 FOR MAXIMUM CONTINUOUS MODE ANTI-ICE ON AIRSPEED: 200 KCAS ROLLS ROYCE AE3007A1 ENGINES Pressure Static Air Temperature - °C Altitude (ft) -40 -35 -30 -25 -20 -15 -10 76.4 77.2 78.0 78.8 79.6 80.4 81.2 82.0 81.5 82.2 82.9 2000 78.5 79.3 80.2 81.0 81.8 82.6 83.4 84.2 83.7 84.5 85.2 4000...
  • Page 654 PERFORMANCE AIRPLANE EMB-145 A1 OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-04-10 REVISION 27...

  • Page 655: Takeoff

    PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL TAKEOFF TAKEOFF SPEEDS Takeoff performance in the FAA approved EMB-145 AFM and ETOASG (First Principles) software is presented in two formats for airplanes equipped with A1 engines: a) Balanced Field Length (fixed V1/VR ratio): - Flaps 9°, ALT T/O-1 thrust - AFM.
  • Page 656 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL V1/VR/V2 SPEEDS EMB-145 - AE3007A1 ENGINES - FAA CERTIFICATION T/O-1 MODE - NORMAL V2 - FLAPS 9° ANTI-ICE ON OR OFF PRESSURE STATIC AIR TEMPERATURE (° ° C) ALTITUDE (ft)   1000 ...
  • Page 657 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL V1/VR/V2 SPEEDS EMB-145 - AE3007A1 ENGINES - FAA CERTIFICATION T/O-1 MODE - NORMAL V2 - FLAPS 22° ANTI-ICE ON OR OFF PRESSURE STATIC AIR TEMPERATURE (° ° C) ALTITUDE (ft)   1000 ...
  • Page 658 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL V1/VR/V2 SPEEDS EMB-145 - AE3007A1 ENGINES - FAA CERTIFICATION ALT T/O-1 MODE - NORMAL V2 - FLAPS 9° ANTI-ICE ON OR OFF PRESSURE STATIC AIR TEMPERATURE (° ° C) ALTITUDE (ft)   1000 ...
  • Page 659 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL FLAPS RETRACTION SCHEDULE Takeoff with flaps 9°: Flaps 9° to UP ............... V + 15 KIAS Takeoff with flaps 22°: Flaps 22° to 9°............... V + 5 KIAS Flaps 9° to UP ............... V + 25 KIAS FINAL SEGMENT SPEED WEIGHT...
  • Page 660 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL PITCH TRIM SETTING FOR TAKEOFF LESS ABOVE THAN 27.6 32.6 36.6 POSITION UP TO UP TO UP TO EQUAL EQUAL 32.5 36.5 41.5 TO 41.6 TO 27.5 PITCH TRIM UNITS Page Code 1-04-15 REVISION 26...
  • Page 661 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL CLIMB GRADIENT The climb gradient tables show the climb gradients for several weights, temperatures and altitudes. These tables are published in the following configurations: GRADIENTS FOR TAKEOFF THRUST AND FLAPS 9 The gradients were obtained for a speed equal to V + 10 KIAS and ratio equal to 1.2.
  • Page 662 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL CLIMB GRADIENT - ALL ENGINES OPERATING TAKEOFF RATING - FLAPS 9 AE3007A1 ENGINES ANTI ICE: OFF LANDING GEAR UP T/O-1 MODE AIRSPEED: V2 + 10 KIAS WINGS LEVELED ALTITUDE: 0 FT ISA + ºC WEIGHT (LB) 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000 48000 50000 -30 34.06 31.23 28.67 26.33 24.20 22.31 20.61 19.08 17.70 16.45 15.30 14.26...
  • Page 663 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL CLIMB GRADIENT - ALL ENGINES OPERATING TAKEOFF RATING - FLAPS 9 AE3007A1 ENGINES ANTI ICE: OFF LANDING GEAR UP T/O-1 MODE AIRSPEED: V2 + 10 KIAS WINGS LEVELED ALTITUDE: 6000 FT ISA + ºC WEIGHT (LB) 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000 48000 50000 -30 32.62 29.84 27.32 25.00 22.97 21.15 19.53 18.06 16.74 15.54 14.45 13.46...
  • Page 664 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL CLIMB GRADIENT - ALL ENGINES OPERATING TAKEOFF RATING - FLAPS 9 AE3007A1 ENGINES ANTI ICE: OFF LANDING GEAR UP T/O-1 MODE AIRSPEED: V2 + 10 KIAS WINGS LEVELED ALTITUDE: 12000 FT ISA + ºC WEIGHT (LB) 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000 48000 50000 -30 26.15 23.60 21.38 19.42 17.72 16.20 14.84 13.62 12.51 11.51 10.61...
  • Page 665 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL CLIMB GRADIENT - ALL ENGINES OPERATING TAKEOFF RATING - FLAPS UP AE3007A1 ENGINES ANTI ICE: OFF LANDING GEAR UP T/O-1 MODE AIRSPEED: 200 KIAS WINGS LEVELED ALTITUDE: 0 FT ISA + ºC WEIGHT (LB) 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000 48000 50000 -30 29.37 27.14 25.17 23.42 21.86 20.44 19.15 17.97 16.89 15.89 14.96 14.10 -20 29.38 27.15 25.19 23.44 21.87 20.45 19.16 17.98 16.90 15.90 14.97 14.11...
  • Page 666 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL CLIMB GRADIENT - ALL ENGINES OPERATING TAKEOFF RATING - FLAPS UP AE3007A1 ENGINES ANTI ICE: OFF LANDING GEAR UP T/O-1 MODE AIRSPEED: 200 KIAS WINGS LEVELED ALTITUDE: 6000 FT ISA + ºC WEIGHT (LB) 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000 48000 50000 -30 28.34 26.18 24.27 22.57 21.05 19.68 18.43 17.28 16.23 15.26 14.36 13.52 -20 28.33 26.17 24.26 22.56 21.04 19.67 18.42 17.28 16.22 15.25 14.35 13.51...
  • Page 667 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL CLIMB GRADIENT - ALL ENGINES OPERATING TAKEOFF RATING - FLAPS UP AE3007A1 ENGINES ANTI ICE: OFF LANDING GEAR UP T/O-1 MODE AIRSPEED: 200 KIAS WINGS LEVELED ALTITUDE: 12000 FT ISA + ºC WEIGHT (LB) 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000 48000 50000 -30 21.93 20.20 18.66 17.30 16.07 14.95 13.94 13.01 12.15 11.36 10.62 9.93...
  • Page 668 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL CLIMB GRADIENT - ALL ENGINES OPERATING CLIMB RATING - FLAPS UP AE3007A1 ENGINES ANTI ICE: OFF LANDING GEAR UP CLB MODE WINGS LEVELED SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 300 KIAS AT 12000 FT, MAINTAINING 300 KIAS UP TO 20000 FT.
  • Page 669 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL CLIMB GRADIENT - ALL ENGINES OPERATING CLIMB RATING - FLAPS UP AE3007A1 ENGINES ANTI ICE: OFF LANDING GEAR UP CLB MODE WINGS LEVELED SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 300 KIAS AT 12000 FT, MAINTAINING 300 KIAS UP TO 20000 FT.
  • Page 670 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL CLIMB GRADIENT - ALL ENGINES OPERATING CLIMB RATING - FLAPS UP AE3007A1 ENGINES ANTI ICE: OFF LANDING GEAR UP CLB MODE WINGS LEVELED SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 300 KIAS AT 12000 FT, MAINTAINING 300 KIAS UP TO 20000 FT.
  • Page 671 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL CLIMB GRADIENT - ALL ENGINES OPERATING CLIMB RATING - FLAPS UP AE3007A1 ENGINES ANTI ICE: OFF LANDING GEAR UP CLB MODE WINGS LEVELED SPEED SCHEDULE: 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 300 KIAS AT 12000 FT, MAINTAINING 300 KIAS UP TO 20000 FT.
  • Page 672 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-04-15 REVISION 28...

  • Page 673: Supplementary Takeoff Information

    PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL SUPPLEMENTARY TAKEOFF INFORMATION TURN ANALYSIS The method below presents the criteria for transforming a takeoff flight path with turns in an equivalent straight one to allow the use of the AFM charts or runway analysis software to determine obstacle clearance.
  • Page 674 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL The equivalent obstacle height to be used in a obstacle clearance calculation is: + ΔH + ΔH + ..+ ΔH where: = equivalent obstacle height = actual obstacle height ΔH = height increments for each distance portion flown in 1, 2, n turn to the obstacle.
  • Page 675 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL ΔD = Δt x V ΔD = trajectory displacement in the wind component direction. Δt = elapsed time in turning flight (obtained from the Horizontal Distance and Time to Complete chart) wind speed b2) Distance Flown Compensation The wind takes the same effect as mentioned in item 2a.
  • Page 676 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL For turning flight: Δ Where: Dm = distance flown along the actual trajectory Δt = elapsed time in turning flight PERFORMANCE CHARTS PRESENTATION GRADIENT LOSS DUE TO A STEADY TURN This chart shows the gradient loss due to a steady turn as a function of the bank angle.
  • Page 677 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL GRADIENT LOSS DUE TO A STEADY TURN ONE ENGINE INOPERATIVE TAKEOFF FLAPS 9° ALL ENGINES MODELS Φ ΔV (KIAS) BANK ANGLE - deg Page Code 1-04-20 REVISION 40...
  • Page 678 PERFORMANCE PERFORMANCE AIRPLANE AIRPLANE EMB-145 LB EMB-145 LB OPERATIONS OPERATIONS MANUAL MANUAL GRADIENT LOSS DUE TO A STEADY TURN GRADIENT LOSS DUE TO A STEADY TURN ONE ENGINE INOPERATIVE ONE ENGINE INOPERATIVE TAKEOFF FLAPS 18° TAKEOFF FLAPS 18° ALL ENGINES MODELS ALL ENGINES MODELS Φ...
  • Page 679 PERFORMANCE PERFORMANCE AIRPLANE AIRPLANE EMB-145 LB EMB-145 LB OPERATIONS OPERATIONS MANUAL MANUAL GRADIENT LOSS DUE TO A STEADY TURN GRADIENT LOSS DUE TO A STEADY TURN ONE ENGINE INOPERATIVE ONE ENGINE INOPERATIVE TAKEOFF FLAPS 22° TAKEOFF FLAPS 22° ALL ENGINES MODELS ALL ENGINES MODELS BANK ANGLE - deg BANK ANGLE - deg...
  • Page 680 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-04-20 REVISION 40...
  • Page 681 AIRPLANE PERFORMANCE EMB-145 LB OPERATIONS MANUAL Page Code 1-04-20 REVISION 40...
  • Page 682 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-04-20 REVISION 40...
  • Page 683 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL Page Code 1-04-20 REVISION 40...
  • Page 684 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-04-20 REVISION 40...
  • Page 685 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL AIRCRAFT CLASSIFICATION NUMBER - ACN The Pavement Classification Number (PCN) reported shall indicate that an airplane with ACN equal to or less than the reported PCN can operate on that pavement. PCN - PAVEMENT CLASSIFICATION NUMBER Example: PCN 50 / F / A / X / T 1 - Type of pavement: R = Rigid (concrete)
  • Page 686 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL EMB-145ER - ACN FLEXIBLE PAVEMENT D (CBR = 3%) C (CBR = 6%) B (CBR = 10%) A (CBR = 15%) 24000 26000 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000 48000 50000 WEIGHT (lb) Page Code...
  • Page 687 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL EMB-145EU - ACN FLEXIBLE PAVEMENT D (CBR = 3%) C (CBR = 6%) B (CBR = 10%) A (CBR = 15%) 24000 26000 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000 48000 50000 WEIGHT (lb) Page Code...
  • Page 688 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL EMB-145EP/MP - ACN FLEXIBLE PAVEMENT D (CBR = 3%) C (CBR = 6%) B (CBR = 10%) A (CBR = 15%) 24000 26000 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000 48000 50000 WEIGHT (lb) Page Code...
  • Page 689 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL EMB-145LR/LU - ACN FLEXIBLE PAVEMENT D (CBR = 3%) C (CBR = 6%) B (CBR = 10%) A (CBR = 15%) 26000 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000 48000 50000 52000 WEIGHT (lb) Page...
  • Page 690 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL EMB-145ER - ACN RIGID PAVEMENT D (K = 20 MN/m C (K = 40 MN/m3) B (K = 80 MN/m3) A (K = 150 MN/m3) 2400 0 26000 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000 48000 50000 WEIGHT (lb) Page Code...
  • Page 691 PERFORMANCE PERFORMANCE AIRPLANE AIRPLANE EMB-145 LB EMB-145 LB OPERATIONS OPERATIONS MANUAL MANUAL EMB-145EU - ACN RIGID PAVEMENT EMB-145EU - ACN RIGID PAVEMENT D (K = 20 MN/m D (K = 20 MN/m C (K = 40 MN/m3) C (K = 40 MN/m3) B (K = 80 MN/m3) B (K = 80 MN/m3) A (K = 150 MN/m3)
  • Page 692 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL EMB-145EP/MP - ACN RIGID pavement D (K = 20 MN/m C (K = 40 MN/m3) B (K = 80 MN/m3) A (K = 150 MN/m3) 24000 28000 32000 36000 40000 44000 48000 52000 WEIGHT (lb) Page Code 1-04-20...
  • Page 693 PERFORMANCE PERFORMANCE AIRPLANE AIRPLANE EMB-145 LB EMB-145 LB OPERATIONS OPERATIONS MANUAL MANUAL EMB-145LR/LU - ACN RIGID PAVEMENT EMB-145LR/LU - ACN RIGID PAVEMENT D (K = 20 MN/m D (K = 20 MN/m C (K = 40 MN/m3) C (K = 40 MN/m3) B (K = 80 MN/m3) B (K = 80 MN/m3) A (K = 150 MN/m3)
  • Page 694 Although the AFM presents all the required performance data for takeoff, the amount of options and charts presented, makes their use very difficult. In order to help operators, EMBRAER developed a runway analysis software for determination of the limiting weights.
  • Page 695 PERFORMANCE AIRPLANE EMB-145 LB OPERATIONS MANUAL Level off altitude and height (ft) Wind (in knots) EMB-145 TAKEOFF ANALYSIS, ALLISON AE3007A1 ENGINES, FAA CERTIFICATION ---------------------------------------------------------------------------------------------------------------------------- Airport: AIRPORT NAME ICAO: KLAX Runway: 04 Level Off Height: 400 ft FLAP 9 Elevation: 5000 ft TORA: 2000 m Clearway: 0 m Stopway: 0 m...
  • Page 696 PERFORMANCE AIRPLANE EMB-145 LB OPERATION MANUAL Level off altitude and height (ft) Wind (in knots) EMB-145 TAKEOFF ANALYSIS, ALLISON AE3007A1 ENGINES, FAA CERTIFICATION --------------------------------------------------------------------------------------------------- Airport: AIRPORT NAME ICAO: ABCD Runway: 04 Level Off Height: 400 ft FLAP Elevation: 5000 ft TORA: 2000 m Clearway:...

  • Page 697: Approach

    AIRPLANE PERFORMANCE EMB-145 A1 FAA OPERATIONS MANUAL APPROACH APPROACH CLIMB SPEED - FLAPS 9° APPROACH WEIGHT CLIMB SPEED (lb) (KIAS) 27000 28000 29000 30000 31000 32000 33000 34000 35000 36000 37000 38000 39000 40000 41000 42000 43000 44000 45000 46000 47000 48000 49000...
  • Page 698 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL LANDING CLIMB AND REFERENCE SPEEDS - KIAS WEIGHT (lb) FLAPS 45° FLAPS 22° 27000 28000 29000 30000 31000 32000 33000 34000 35000 36000 37000 38000 39000 40000 41000 42000 43000 44000 45000 46000 47000 48000 49000...
  • Page 699 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL FLAP MANEUVERING SPEED These speeds allow for an inadvertent 15° overshoot beyond the normal 30° bank over stick shaker actuation. FLAP MANEUVERING SPEED (KIAS) BELOW MSLW* ABOVE MSLW* NO ICING WITH ICING NO ICING WITH ICING FLAPS GEAR CONDITIONS...
  • Page 700 PERFORMANCE AIRPLANE EMB-145 A1 FAA OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-04-25 REVISION 36...

  • Page 701: Landing

    1.917. NOTE: The landing distance correction factors mentioned in some emergency or abnormal procedures must be applied to the flap 45 unfactored landing distance. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 702 2974 2815 29000 3415 2919 2762 2609 3490 2988 2829 2673 27000 3250 2768 2615 2466 3320 2832 2677 2527 NOTE: Landing distance in ft. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 703 34000 4307 3728 3546 3368 32000 4106 3547 3371 3199 30000 3912 3371 3200 3034 28000 3711 3189 3024 2863 NOTE: Landing distance in ft. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 704 2328 2199 29000 2701 2293 2164 2039 2756 2345 2214 2088 27000 2578 2179 2052 1929 2630 2227 2099 1976 NOTE: Landing distance in ft. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 705 34000 3370 2894 2743 2598 32000 3225 2762 2616 2477 30000 3076 2629 2491 2358 28000 2918 2495 2361 2231 NOTE: Landing distance in ft. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 706 In order to find the contaminated landing distance, enter the table with the current contaminant, flaps configuration and actual landing weight and obtain a reference contaminated unfactored landing distance (CULD Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 707 Additional Distance = 2000 ft x (12% + 0%+ 9%) = 2000 ft x 21% = 420 ft CULD = 2000 ft + 420 ft = 2420 ft Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 708 LANDING DISTANCE + 3% per 1000 ft ALTITUDE above sea level. LANDING DISTANCE + 11% per 5 kt WIND tailwind. LANDING DISTANCE + 9% per 5 kt above OVERSPEED Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 709 LANDING DISTANCE + 3% per 1000 ft ALTITUDE above sea level. LANDING DISTANCE + 11% per 5 kt WIND tailwind. LANDING DISTANCE + 8% per 5 kt above OVERSPEED Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 710 LANDING DISTANCE + 3% per 1000 ft ALTITUDE above sea level. LANDING DISTANCE + 10% per 5 kt WIND tailwind. LANDING DISTANCE + 8% per 5 kt above OVERSPEED Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 711 LANDING DISTANCE + 3% per 1000 ft ALTITUDE above sea level. LANDING DISTANCE + 11% per 5 kt WIND tailwind. LANDING DISTANCE + 7% per 5 kt above OVERSPEED Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 712 LANDING DISTANCE + 3% per 1000 ft ALTITUDE above sea level. LANDING DISTANCE + 24% per 5 kt WIND tailwind. LANDING DISTANCE + 5% per 5 kt above OVERSPEED Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 713 LANDING DISTANCE + 4% per 1000 ft ALTITUDE above sea level. LANDING DISTANCE + 12% per 5 kt WIND tailwind. LANDING DISTANCE + 8% per 5 kt above OVERSPEED Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 714 LANDING DISTANCE + 4% per 1000 ft ALTITUDE above sea level. LANDING DISTANCE + 12% per 5 kt WIND tailwind. LANDING DISTANCE + 8% per 5 kt above OVERSPEED Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 715 LANDING DISTANCE + 3% per 1000 ft ALTITUDE above sea level. LANDING DISTANCE + 11% per 5 kt WIND tailwind. LANDING DISTANCE + 8% per 5 kt above OVERSPEED Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 716 LANDING DISTANCE + 3% per 1000 ft ALTITUDE above sea level. LANDING DISTANCE + 11% per 5 kt WIND tailwind. LANDING DISTANCE + 8% per 5 kt above OVERSPEED Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 717 LANDING DISTANCE + 3% per 1000 ft ALTITUDE above sea level. LANDING DISTANCE + 24% per 5 kt WIND tailwind. LANDING DISTANCE + 6% per 5 kt above OVERSPEED Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 718 Wing Anti-Icing Asymmetry 1.48 Flaps 22° - V + 30 kt REF 45 Wing Anti-Icing Failure 1.48 Flaps 22° - V + 30 kt REF 45 Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 719 NOTE: If the tires are not flat after 36 minutes (or 33 minutes) this is a positive indication that the wheel thermal plugs have not melted. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 720 33359 33852 34374 34916 35386 34522 35039 35572 36131 36619 33136 33625 34144 34682 35149 34285 34797 35328 35884 36368 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 721 32734 33214 33729 34262 34723 33859 34362 34889 35438 35915 32515 32991 33504 34033 34491 33627 34126 34650 35195 35670 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 722 32337 32809 33320 33847 34302 33438 33933 34455 34998 35469 32118 32586 33095 33618 34070 33206 33696 34216 34755 35223 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 723 31718 32178 32683 33200 33646 32782 33264 33779 34312 34774 31503 31959 32461 32976 33418 32554 33031 33544 34074 34533 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 724 31321 31773 32274 32785 33225 32361 32834 33346 33873 34328 31107 31555 32053 32561 32998 32134 32603 33112 33635 34087 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 725 30709 31149 31643 32145 32576 31712 32172 32677 33194 33640 30498 30933 31425 31924 32352 31488 31944 32446 32960 33402 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 726 30314 30745 31236 31732 32157 31293 31744 32245 32756 33196 30101 30527 31016 31510 31931 31067 31514 32012 32520 32956 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 727 29700 30119 30603 31091 31506 30642 31080 31574 32076 32505 29490 29904 30386 30871 31283 30419 30852 31344 31842 32268 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 728 29306 29717 30197 30679 31089 30224 30653 31143 31639 32062 29096 29502 29980 30459 30865 30001 30425 30913 31405 31825 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 729 29042 29448 29925 30403 30809 29945 30368 30855 31346 31765 28849 29250 29725 30201 30604 29739 30158 30643 31132 31547 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 730 35909 36362 36843 37290 37750 37242 37712 38206 38669 39147 35669 36119 36598 37041 37498 36989 37456 37947 38407 38882 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 731 35235 35679 36153 36592 37043 36532 36993 37479 37934 38403 35000 35441 35913 36349 36796 36284 36742 37226 37677 38143 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 732 34805 35244 35714 36147 36592 36079 36534 37016 37465 37928 34569 35005 35473 35903 36345 35831 36283 36763 37208 37668 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 733 34148 34578 35042 35467 35903 35386 35833 36308 36749 37202 33923 34350 34812 35235 35667 35150 35593 36067 36504 36954 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 734 33731 34156 34616 35036 35466 34948 35388 35860 36295 36742 33508 33930 34388 34805 35232 34712 35150 35619 36051 36495 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 735 33090 33506 33960 34373 34794 34272 34704 35169 35596 36034 32870 33283 33735 34144 34563 34040 34469 34932 35356 35790 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 736 32678 33089 33539 33945 34361 33838 34263 34725 35145 35576 32458 32866 33313 33717 34130 33606 34028 34487 34905 35333 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 737 32054 32456 32893 33292 33699 33172 33589 34044 34456 34879 31845 32244 32672 33069 33473 32945 33359 33811 34221 34640 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 738 31660 32057 32477 32871 33272 32744 33155 33606 34013 34429 31449 31842 32254 32646 33044 32514 32923 33371 33775 34188 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 739 31360 31752 32160 32551 32947 32417 32825 33271 33675 34087 31152 31541 31940 32329 32722 32193 32598 33040 33441 33850 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 740 42275 42874 43527 44219 44818 43607 44223 44892 45604 46219 41984 42579 43229 43917 44512 43301 43913 44578 45285 45897 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 741 41458 42046 42690 43370 43959 42747 43352 44011 44710 45315 41173 41758 42398 43074 43659 42448 43049 43704 44399 44999 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 742 40938 41519 42157 42829 43411 42200 42798 43450 44141 44739 40655 41232 41867 42535 43113 41902 42496 43145 43831 44425 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 743 40138 40709 41337 41997 42569 41358 41945 42587 43266 43853 39863 40430 41055 41711 42280 41069 41652 42291 42965 43549 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 744 39623 40188 40810 41463 42028 40817 41397 42033 42703 43284 39342 39903 40522 41170 41732 40521 41097 41730 42396 42973 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 745 38819 39373 39986 40627 41183 39971 40540 41166 41824 42394 38543 39094 39704 40340 40892 39681 40246 40869 41522 42089 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 746 38298 38845 39452 40085 40634 39422 39984 40604 41254 41817 38018 38562 39165 39794 40340 39128 39686 40303 40948 41508 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 747 37500 38036 38634 39255 39795 38583 39134 39744 40381 40934 37227 37760 38355 38972 39508 38296 38843 39450 40083 40633 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 748 36988 37518 38110 38723 39256 38045 38589 39193 39822 40368 36716 37243 37831 38440 38970 37759 38299 38899 39524 40067 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 749 36210 36730 37313 37914 38438 37226 37759 38354 38971 39507 35944 36460 37040 37638 38158 36946 37476 38067 38680 39213 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 750 35710 36224 36800 37395 37912 36700 37227 37815 38424 38954 35445 35955 36529 37119 37633 36421 36944 37529 38134 38661 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 751 45194 45781 46334 47008 47530 46671 47274 47844 48539 49067 44892 45475 46025 46695 47215 46354 46952 47519 48210 48737 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 752 44341 44919 45462 46125 46642 45774 46367 46927 47609 48133 44046 44620 45160 45819 46334 45463 46053 46609 47287 47810 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 753 43797 44368 44905 45561 46075 45201 45788 46341 47016 47537 43500 44068 44601 45253 45765 44889 45472 46021 46692 47212 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 754 42954 43517 44044 44687 45197 44315 44892 45435 46097 46614 42663 43223 43746 44386 44895 44009 44583 45122 45780 46296 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 755 42413 42969 43490 44126 44634 43745 44316 44852 45507 46021 42122 42675 43193 43825 44331 43439 44007 44540 45190 45702 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 756 41581 42129 42640 43265 43768 42871 43432 43958 44601 45111 41298 41842 42350 42971 43473 42572 43131 43653 44292 44800 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 757 41047 41589 42093 42711 43211 42308 42864 43383 44018 44525 40762 41301 41803 42416 42915 42009 42561 43077 43708 44213 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 758 40231 40765 41260 41866 42363 41451 41997 42506 43130 43632 39952 40483 40975 41577 42072 41157 41700 42206 42825 43326 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 759 39706 40233 40723 41322 41815 40898 41438 41941 42557 43056 39427 39952 40437 41033 41525 40604 41142 41641 42253 42751 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 760 38907 39426 39906 40494 40984 40057 40589 41082 41686 42182 38633 39150 39626 40211 40699 39770 40298 40788 41388 41882 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 761 38390 38904 39378 39959 40446 39514 40040 40527 41123 41616 38117 38627 39098 39675 40161 39226 39748 40232 40824 41316 NOTE: Quick Turn Around Weight in lb. Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 762 PERFORMANCE AIRPLANE EMB-145/135 FAA OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 763 Although the AFM presents all the required performance data for takeoff, the amount of options and charts presented, makes its use very difficult. In order to help operators, EMBRAER developed a runway analysis software for determination of the limiting weights.
  • Page 764 Limit weight (in pounds), limiting factor, approach climb speed (in knots), reference speed (in knots), and Temperature (in degrees Celsius) quick turn around weight (in pounds) EXAMPLE Page Code 1-04-30 REVISION 41 Copyright © by Embraer. Refer to cover page for details.
  • Page 765 AIRPLANE FLIGHT PLANNING OPERATIONS MANUAL SECTION 1-05 FLIGHT PLANNING TABLE OF CONTENTS Page Block Introduction .................1-05-00 Simplified Flight Planning ............1-05-05 APU and Engine Fuel Consumption...........1-05-07 Climb...................1-05-10 Cruise ..................1-05-15 Descent..................1-05-20 Holding..................1-05-25 One Engine Inoperative Performance ........1-05-30 Flight with Landing Gear Down (*)..........1-05-35 Flight with Flaps Locked at 9°...

  • Page 766: Introduction

    AIRPLANE FLIGHT PLANNING OPERATIONS MANUAL INTRODUCTION This section presents climb, cruise, descent and holding performance data. In addition, simplified flight planning and one engine inoperative are included. NOTE: Airplanes equipped with Rolls Royce AE3007A1P engines should use the same simplified flight planning, climb, cruise, descent, holding, one engine inoperative performance, flight with landing gear down, flight with flaps locked at 9°...

  • Page 767: Simplified Flight Planning

    AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL SIMPLIFIED FLIGHT PLANNING Simplified flight planning charts allow quick determination of estimated trip fuel and time from brake release to landing. The following phases are included: takeoff, climb, cruise, descent, approach and landing. Charts are provided for Long Range Cruise (LRC) and Maximum Speed Cruise (MSC) at constant altitude.
  • Page 768 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL The reserve fuel is also dependant on national regulations and normally is the fuel required for flying 10% of the trip time (based on the latest fuel flow) or is equivalent to 5% of the trip fuel. The allowances below may be used: PHASE OF FLIGHT FUEL CONSUMPTION...
  • Page 769 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL RESULTS From Simplified Flight Planning Chart - Long Range Cruise: Trip Fuel ................2900 lb From Simplified Flight Planning Chart - Long Range Cruise: Fuel to Alternate ..............1600 lb Reserve Fuel ..............
  • Page 770 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL EMB-145 SIMPLIFIED FLIGHT PLANNING AE3007A1 AND AE3007A1P ENGINES LONG RANGE CRUISE ISA CONDITION 9500 FL150 FL200 FL250 FL300 9000 BASED ON: 240/270/M0.56 CLIMB 8500 MMO/250/240 DESCENT 8000 7500 FL350 & ABOVE 7000 6500 6000...
  • Page 771 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL EMB-145 SIMPLIFIED FLIGHT PLANNING AE3007A1 AND AE3007A1P ENGINES MAXIMUM SPEED CRUISE ISA CONDITION 9500 FL150 FL200 FL250 FL300 9000 BASED ON: 240/270/M0.56 CLIMB 8500 MMO/250/240 DESCENT 8000 FL350 & ABOVE 7500 7000 6500...
  • Page 772 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL EMB-145 FLIGHT TIME AE3007A1 AND AE3007A1P ENGINES LONG RANGE CRUISE LONG RANGE CRUISE ISA CONDITION FL150 FL200 FL250 FL300 BASED ON: 240/270/M0.56 CLIMB MMO/250/240 DESCENT FL350 & ABOVE REF. LINE 1000 1200 1400...
  • Page 773 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL EMB-145 FLIGHT TIME AE3007A1 AND AE3007A1P ENGINES MAXIMUM SPEED CRUISE MAXIMUM SPEED CRUISE ISA CONDITION BASED ON: 240/270/M0.56 CLIMB MMO/250/240 DESCENT FL350 FL150 REF. LINE 1000 1200 1400 1600 TRIP DISTANCE - NM 145AOM004 - 15JUN1999 Page Code...
  • Page 774 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CRUISE - FLIGHT LEVEL TABLE The table below permits quick determination of the cruise flight level for minimum fuel consumption, based on the trip distance and takeoff weight. For each takeoff weight two different flight levels are calculated (A or B) based on the following assumptions: −...
  • Page 775 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL The table data are presented for ISA condition, all engine operating and Maximum Speed Cruise schedule. FLIGHT LEVEL - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES MAX SPEED CRUISE AND ISA CONDITIONS TRIP DISTANCE (NM) TOW (LB) 48501 (1)
  • Page 776 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CRUISE - ALTITUDE CAPABILITY TABLE The table below permits quick determination of the altitude capability, based on the initial cruise weight. The table data are presented for various ISA conditions, all engines operating and Maximum Speed Cruise schedule.
  • Page 777 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CRUISE - WIND ALTITUDE TRADE The following tables allow the determination of the break-even wind in order to maintain the same ground specific range at another altitude than the one planned initially. Long Range Cruise or Maximum Speed Cruise tables are provided.
  • Page 778 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CRUISE WIND ALTITUDE TRADE LONG RANGE CRUISE SPEED AE3007A1 AND AE3007A1P ENGINES, ALL ENGINES OPERATING PRESSURE ALTITUDE (x 1000 FT) WEIGHT (LB) 26000 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000...
  • Page 779 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CRUISE WIND ALTITUDE TRADE MAXIMUM SPEED CRUISE AE3007A1 AND AE3007A1P ENGINES, ALL ENGINES OPERATING PRESSURE ALTITUDE (x 1000 FT) WEIGHT (LB) 26000 28000 30000 32000 34000 36000 38000 40000 42000 44000 46000 48000...
  • Page 780 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-05-05 REVISION 40...
  • Page 781 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL FLIGHT PLANNING – FUEL TANKERING Fuel price variations at different airports may require carrying more fuel than the minimum required on a flight leg. The procedure of loading this extra amount of fuel (or surplus fuel) in order to minimize fuel costs is known as Fuel Tankering.
  • Page 782 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL FUEL TANKERING LONG RANGE CRUISE SPEED AE3007A1 AND AE3007A1P ENGINES, ALL ENGINES OPERATING FUEL SURPLUS RATIO TRIP DISTANCE 32000 FT 33000 FT (NM) AND BELOW AND ABOVE 1.02 1.02 1.04 1.04 1.06 1.06...

  • Page 783: Apu And Engine Fuel Consumption

    FLIGHT PLANNING AIRPLANE EMB-135/145 LB OPERATIONS ERJ-140 LB MANUAL EMB-145 XR APU AND ENGINE FUEL CONSUMPTION APU FUEL CONSUMPTION The table below shows the APU fuel consumption on the ground and during level flight at 5000 ft, 25000 ft and 37000 ft altitudes. The data is calculated for different airspeeds, APU air bleeds, and electrical loads.
  • Page 784 FLIGHT PLANNING AIRPLANE EMB-135/145 LB OPERATIONS ERJ-140 LB MANUAL EMB-145 XR ENGINE FUEL CONSUMPTION The following values established for taxi, take-off, approach and go around fuel consumption should be considered when calculating detailed flight plans. FUEL CONSUMPTION FUEL CONSUMPTION ENGINE PHASE OF FLIGHT lb/min TAXI...

  • Page 785: Climb

    AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB CLIMB SPEEDS MAXIMUM ANGLE SPEED This speed is recommended for obstacle clearance in order to reach an altitude on minimum ground distance. The recommended maximum angle speed is related to flaps up, all engines operating and is approximately VFS for all gross weights and altitudes (see Final Segment Speed table on section 1-04-15).
  • Page 786 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB TABLES The climb planning tables show fuel consumption, distance, and time considering the airplane in climb configuration from the Sea Level up to the top of climb. Data are shown for various takeoff weights, ISA deviations and cruise altitudes.
  • Page 787 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL EXAMPLE: Given: Departure Airport Elevation ........ 2100 ft Takeoff weight ............ 40000 lb ISA Condition Cruise Altitude ............ 33000 ft RESULTS Data for 3600 ft (2100 ft + 1500 ft above departure airport) obtained from interpolation from the Sea Level to 5000 ft climb table: Fuel: 93.6 lb Distance: 4.3 NM...
  • Page 788 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-05-10 REVISION 40...
  • Page 789 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 5000 AND 6000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 790 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 7000 AND 8000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 791 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 9000 AND 10000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 792 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 11000 AND 12000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 793 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 13000 AND 14000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 794 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 15000 AND 16000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 795 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 17000 AND 18000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 796 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 19000 AND 20000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 797 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 21000 AND 22000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 798 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 23000 AND 24000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 799 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 25000 AND 26000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 800 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 27000 AND 28000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 801 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 29000 AND 30000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 802 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 31000 AND 32000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 803 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 33000 AND 34000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 804 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 35000 AND 36000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 805 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE: SEA LEVEL TO 37000 FT SPEED SCHEDULE : 240 KIAS UP TO 10000 FT, INCREASING LINEARLY TO 270 KIAS AT 12000 FT, MAINTAINING 270 KIAS UP TO 17400 FT AND M = 0.56 ABOVE 17400 FT CRUISE CONFIGURATION BLEED: OPEN...
  • Page 806 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-05-10 REVISION 40...

  • Page 807: Cruise

    AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CRUISE MANEUVER CAPABILITY NOTE: The recommended cruise altitude must ensure a maneuver load factor of 1.3 g before buffet onset. 20000 ft 48501 lb 45450 lb 25000 ft 42000 lb 38000 lb 30000 ft 34000 lb...
  • Page 808 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-05-15 REVISION 40...
  • Page 809 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL CRUISE TABLES The long range cruise and maximum speed cruise tables show N1, fuel flow, indicated airspeed, true airspeed, indicated Mach number, buffet margin and specific range. Data are presented for various weights ISA conditions and corrections for ISA deviation.
  • Page 810 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE : 5000 FT TO 18000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 10000 11000 12000 13000 14000 15000 16000 17000 18000 66.7 71.6 72.2...
  • Page 811 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE : 5000 FT TO 18000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 10000 11000 12000 13000 14000 15000 16000 17000 18000 64.6 67.8 68.4...
  • Page 812 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE : 5000 FT TO 18000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 10000 11000 12000 13000 14000 15000 16000 17000 18000 60.1 63.2 63.8...
  • Page 813 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE : 19000 FT TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000 22000 23000 24000 25000 26000 27000 28000 77.7 78.5 79.3...
  • Page 814 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE : 19000 FT TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000 22000 23000 24000 25000 26000 27000 28000 72.8 73.5 74.3...
  • Page 815 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE : 19000 FT TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000 22000 23000 24000 25000 26000 27000 28000 68.4 69.5 70.1...
  • Page 816 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE : 29000 FT TO 37000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 29000 30000 31000 32000 33000 34000 35000 36000 37000 84.9 85.6 86.3...
  • Page 817 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE : 29000 FT TO 37000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 29000 30000 31000 32000 33000 34000 35000 36000 37000 80.5 81.2 82.8...
  • Page 818 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES ALTITUDE : 29000 FT TO 37000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 29000 30000 31000 32000 33000 34000 35000 36000 37000 75.6 76.4 77.2...
  • Page 819 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES PRESSURE ALTITUDE: 5000 FT TO 18000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 10000 11000 12000 13000 14000 15000 16000 17000 18000 66.7 78.1 78.9...
  • Page 820 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES PRESSURE ALTITUDE: 5000 FT TO 18000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS WEIGHT ALTITUDE (FT) (LB) 5000 10000 11000 12000 13000 14000 15000 16000 17000 18000 64.6 76.7 77.4...
  • Page 821 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES PRESSURE ALTITUDE: 5000 FT TO 18000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS WEIGHT ALTITUDE (FT) (LB) 5000 10000 11000 12000 13000 14000 15000 16000 17000 18000 62.5 75.3 76.0...
  • Page 822 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES PRESSURE ALTITUDE: 19000 FT TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITIONS WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000 22000 23000 24000 25000 26000 27000 28000 85.2 85.9 86.5...
  • Page 823 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES PRESSURE ALTITUDE: 19000 FT TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000 22000 23000 24000 25000 26000 27000 28000 83.8 84.4 85.1...
  • Page 824 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES PRESSURE ALTITUDE: 19000 FT TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000 22000 23000 24000 25000 26000 27000 28000 82.3 83.6 84.2...
  • Page 825 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES PRESSURE ALTITUDE: 29000 FT TO 37000 FT CRUISE CONFIGURATION BLEED: OPEN WEIGHT ALTITUDE (FT) (LB) 29000 30000 31000 32000 33000 34000 35000 36000 37000 87.9 87.9 88.3...
  • Page 826 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES PRESSURE ALTITUDE: 29000 FT TO 37000 FT CRUISE CONFIGURATION BLEED: OPEN WEIGHT ALTITUDE (FT) (LB) 29000 30000 31000 32000 33000 34000 35000 36000 37000 87.8 87.8 87.8...
  • Page 827 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES PRESSURE ALTITUDE: 29000 FT TO 37000 FT CRUISE CONFIGURATION BLEED: OPEN WEIGHT ALTITUDE (FT) (LB) 29000 30000 31000 32000 33000 34000 35000 36000 37000 86.9 86.8 86.7...
  • Page 828 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-05-15 REVISION 40...

  • Page 829: Descent

    AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL DESCENT The descent table shows fuel consumption, distance and time from the top of descent to sea level for various cruise altitudes. The data are calculated for flight idle thrust setting, maintaining 250 KIAS up to 10000 ft and 240 KIAS below 10000 ft.
  • Page 830 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL EXAMPLE: Given: Arrival Airport Elevation ........3500 ft Top of Descent Weight ........38000 lb ISA Condition Cruise Altitude.............35000 ft RESULTS Data provided from 35000 ft (Top of Descent) to Sea Level table: Fuel: 227 lb Distance: 87 NM Time: 16 min...
  • Page 831 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL DESCENT - ALL ENGINES OPERATING AE3007A1 AND AE3007A1P ENGINES CRUISE CONFIGURATION BLEED : OPEN FLIGHT IDLE AIRSPEED : MMO / 250 KIAS / 240 KIAS ISA CONDITIONS WEIGHT TOP OF DESCENT (LB) (FT) 5000 10000 15000 20000 25000 30000 35000 37000...
  • Page 832 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-05-20 REVISION 40...

  • Page 833: Holding

    AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING The holding tables show indicated airspeed, Mach number, N1, fuel flow and fuel consumption for various weights, altitudes, anti-ice on (with and without ice accretion) and off condition. Data are presented in ISA condition for all engines operating configuration.
  • Page 834 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - ALL ENGINES AE3007A1 AND AE3007A1P ENGINES CRUISE CONFIGURATION BLEED: OPEN ANTI-ICE: OFF MINIMUM FUEL CONSUMPTION SPEED STANDARD ATMOSPHERE WEIGHT ALTITUDE (FT) (LB) 1500 5000 10000 15000 20000 25000 30000 37000 50000 MACH 0.272 0.277 0.290 0.313 0.342 0.379 0.426 0.487 0.581...
  • Page 835 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - ALL ENGINES AE3007A1 AND AE3007A1P ENGINES CRUISE CONFIGURATION BLEED: OPEN ANTI-ICE: OFF MINIMUM FUEL CONSUMPTION SPEED STANDARD ATMOSPHERE WEIGHT ALTITUDE (FT) (LB) 1500 5000 10000 15000 20000 25000 30000 37000 164.9 166.6 171.0 178.9 189.0 202.3 219.6 242.3 287.7 38000 MACH...
  • Page 836 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - ALL ENGINES AE3007A1 AND AE3007A1P ENGINES CRUISE CONFIGURATION BLEED: OPEN ANTI-ICE: ON (WITHOUT ICE ACCRETION) STANDARD ATMOSPHERE WEIGHT ALTITUDE (FT) (LB) 1500 5000 10000 15000 20000 25000 30000 37000 200.4 204.7 215.4 232.0 250.4 271.0 293.9 319.5 361.8 49000 MACH...
  • Page 837 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - ALL ENGINES AE3007A1 AND AE3007A1P ENGINES CRUISE CONFIGURATION BLEED: OPEN ANTI-ICE: ON (WITHOUT ICE ACCRETION) STANDARD ATMOSPHERE WEIGHT ALTITUDE (FT) (LB) 1500 5000 10000 15000 20000 25000 30000 37000 199.5 203.9 214.5 231.1 249.5 269.9 292.8 318.2 360.4 38000 MACH...
  • Page 838 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - ALL ENGINES AE3007A1 AND AE3007A1P ENGINES CRUISE CONFIGURATION BLEED: OPEN ANTI-ICE: ON (WITH ICE ACCRETION) STANDARD ATMOSPHERE WEIGHT ALTITUDE (FT) (LB) 1500 5000 10000 15000 20000 25000 30000 37000 200.4 204.7 215.4 232.0 250.4 271.0 293.9 319.5 361.8 49000 MACH...
  • Page 839 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - ALL ENGINES AE3007A1 AND AE3007A1P ENGINES CRUISE CONFIGURATION BLEED: OPEN ANTI-ICE: ON (WITH ICE ACCRETION) STANDARD ATMOSPHERE WEIGHT ALTITUDE (FT) (LB) 1500 5000 10000 15000 20000 25000 30000 37000 199.5 203.9 214.5 231.1 249.5 269.9 292.8 318.2 360.4 38000 MACH...
  • Page 840 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-05-25 REVISION 40...

  • Page 841: One Engine Inoperative Performance

    AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL ONE ENGINE INOPERATIVE PERFORMANCE CRUISE TABLES The one engine inoperative long range cruise tables show N1, fuel flow, indicated airspeed, true airspeed, indicated Mach number, buffet margin and specific range. Data are presented for various weights, altitudes and corrections for ISA deviation.
  • Page 842 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ONE ENGINE INOPERATIVE AE3007A1 AND AE3007A1P ENGINES ALTITUDE: 5000 FT TO 14000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 7000 9000 10000 11000 12000...
  • Page 843 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ONE ENGINE INOPERATIVE AE3007A1 AND AE3007A1P ENGINES ALTITUDE: 5000 FT TO 14000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 7000 9000 10000 11000 12000...
  • Page 844 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ONE ENGINE INOPERATIVE AE3007A1 AND AE3007A1P ENGINES ALTITUDE: 15000 FT TO 22000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 15000 16000 17000 18000 19000 20000 21000...
  • Page 845 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ONE ENGINE INOPERATIVE AE3007A1 AND AE3007A1P ENGINES ALTITUDE: 15000 FT TO 22000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 15000 16000 17000 18000 19000 20000 21000...
  • Page 846 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ONE ENGINE INOPERATIVE AE3007A1 AND AE3007A1P ENGINES ALTITUDE: 23000 FT TO 30000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 23000 24000 25000 26000 27000 28000 29000...
  • Page 847 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ONE ENGINE INOPERATIVE AE3007A1 AND AE3007A1P ENGINES ALTITUDE: 23000 FT TO 30000 FT CRUISE CONFIGURATION BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 23000 24000 25000 26000 27000 28000 29000...
  • Page 848 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL DRIFTDOWN TABLE In the event of an engine failure during cruise it will generally be necessary to reduce speed and descent to a lower altitude. Immediately after engine failure set maximum continuous N1 and allow the airplane to decelerate from the cruise speed to the initial drift down speed shown in the driftdown table.
  • Page 849 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL DRIFTDOWN TABLE EMB-145 - AE3007A1 AND AE3007A1P ENGINES - FAA CERTIFICATION BLEEDS ON/ANTI ICE OFF GROSS LEVEL OFF ALTITUDE - FT WEIGHT (LB) INITIAL (NET LEVEL OFF ALTITUDE - FT) DRIFTDOWN SPEED START...
  • Page 850 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL DRIFTDOWN TABLE EMB-145 - AE3007A1 AND AE3007A1P ENGINES - FAA CERTIFICATION BLEEDS ON/ANTI ICE ON GROSS LEVEL OFF ALTITUDE - FT WEIGHT (LB) INITIAL DRIFT (NET LEVEL OFF ALTITUDE - FT) DOWN SPEED START...
  • Page 851 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING The holding tables show indicated airspeed, mach number, N1, fuel flow and fuel consumption for various weights and altitudes. Data are presented in ISA condition for all engines operating and one engine inoperative configuration.
  • Page 852 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - ONE ENGINE INOPERATIVE AE3007A1 AND AE3007A1P ENGINES CRUISE CONFIGURATION BLEED: OPEN ANTI-ICE: OFF MINIMUM FUEL CONSUMPTION SPEED STANDARD ATMOSPHERE WEIGHT ALTITUDE (FT) (LB) 5000 10000 15000 20000 25000 30000 35000 37000 178.6 187 197.8 211.7 49000...
  • Page 853 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - ONE ENGINE INOPERATIVE AE3007A1 AND AE3007A1P ENGINES CRUISE CONFIGURATION BLEED: OPEN ANTI-ICE: OFF MINIMUM FUEL CONSUMPTION SPEED STANDARD ATMOSPHERE WEIGHT ALTITUDE (FT) (LB) 5000 10000 15000 20000 25000 30000 35000 37000 162.2 167.7 175 184.6 197 213.3...
  • Page 854 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - ONE ENGINE INOPERATIVE AE3007A1 AND AE3007A1P ENGINES CRUISE CONFIGURATION BLEED: OPEN ANTI-ICE: ON (WITH ICE ACCRETION) STANDARD ATMOSPHERE WEIGHT ALTITUDE (FT) (LB) 5000 10000 15000 20000 25000 30000 35000 37000 200.3 215.3 231.9 250.4 49000 Mach...
  • Page 855 AIRPLANE FLIGHT PLANNING EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - ONE ENGINE INOPERATIVE AE3007A1 AND AE3007A1P ENGINES CRUISE CONFIGURATION BLEED: OPEN ANTI-ICE: ON (WITH ICE ACCRETION) STANDARD ATMOSPHERE WEIGHT ALTITUDE (FT) (LB) 5000 10000 15000 20000 25000 30000 35000 37000 199.1 214 230.5 248.9 269.3 36000...
  • Page 856 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-05-30 REVISION 40...

  • Page 857: Flight With Landing Gear Down

    FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL FLIGHT WITH LANDING GEAR DOWN This section presents climb, cruise, descent and holding data for flight with all engines operating and the landing gear locked down. This set of data may be used in the following situations: −...
  • Page 858 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL EMERGENCY AND ABNORMAL PROCEDURES The Emergency and Abnormal Procedures remain unchanged, except that all procedures will be performed with landing gear down. NORMAL PROCEDURES The Normal Procedures remain unchanged, except that all procedures will be performed with the landing gear down and during the cruise phase the fuel quantity should be monitored throughout the flight.
  • Page 859 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 5000 AND 6000 FT SPEED SCHEDULE: 150 KIAS ALL ENGINES OPERATING BLEED: OPEN 5000 FT 6000 FT WEIGHT ISA +...
  • Page 860 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 7000 AND 8000 FT SPEED SCHEDULE: 150 KIAS ALL ENGINES OPERATING BLEED: OPEN 7000 FT 8000 FT WEIGHT ISA +...
  • Page 861 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 9000 AND 10000 FT SPEED SCHEDULE: 150 KIAS ALL ENGINES OPERATING BLEED: OPEN 9000 FT 10000 FT WEIGHT ISA +...
  • Page 862 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 11000 AND 12000 FT SPEED SCHEDULE: 150 KIAS ALL ENGINES OPERATING BLEED: OPEN 11000 FT 12000 FT WEIGHT ISA +...
  • Page 863 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 13000 AND 14000 FT SPEED SCHEDULE: 150 KIAS ALL ENGINES OPERATING BLEED: OPEN 13000 FT 14000 FT WEIGHT ISA +...
  • Page 864 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 15000 AND 16000 FT SPEED SCHEDULE: 150 KIAS ALL ENGINES OPERATING BLEED: OPEN 15000 FT 16000 FT WEIGHT ISA +...
  • Page 865 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 17000 AND 18000 FT SPEED SCHEDULE: 150 KIAS ALL ENGINES OPERATING BLEED: OPEN 17000 FT 18000 FT WEIGHT ISA +...
  • Page 866 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 19000 AND 20000 FT SPEED SCHEDULE: 150 KIAS ALL ENGINES OPERATING BLEED: OPEN 19000 FT 20000 FT WEIGHT ISA +...
  • Page 867 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 21000 AND 22000 FT SPEED SCHEDULE: 150 KIAS ALL ENGINES OPERATING BLEED: OPEN 21000 FT 22000 FT WEIGHT ISA +...
  • Page 868 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 23000 AND 24000 FT SPEED SCHEDULE: 150 KIAS ALL ENGINES OPERATING BLEED: OPEN 23000 FT 24000 FT WEIGHT ISA +...
  • Page 869 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 25000 FT SPEED SCHEDULE: 150 KIAS ALL ENGINES OPERATING BLEED: OPEN 25000 FT WEIGHT ISA + (LB) FUEL...
  • Page 870 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CRUISE - FLIGHT WITH LANDING GEAR DOWN The Long Range Cruise and Maximum Speed Cruise tables show N1, fuel flow, indicated airspeed, true airspeed, indicated Mach number, buffet margin and specific range. Data is presented for ISA conditions and various weights, with corrections for ISA deviations.
  • Page 871 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: 5000 FT TO 11000 FT BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 6000 7000...
  • Page 872 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: 12000 FT TO 18000 FT BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 12000 13000 14000...
  • Page 873 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: 19000 FT TO 25000 FT BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000...
  • Page 874 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: 5000 FT TO 11000 FT BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 6000 7000...
  • Page 875 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: 5000 FT TO 11000 FT BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 6000 7000...
  • Page 876 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: 12000 FT TO 18000 FT BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 12000 13000 14000...
  • Page 877 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: 12000 FT TO 18000 FT BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 12000 13000 14000...
  • Page 878 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES ALTITUDE: 19000 FT TO 25000 FT BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000...
  • Page 879 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL DESCENT - FLIGHT WITH LANDING GEAR DOWN The descent table shows fuel consumption, distance and time from the top of descent to sea level for various cruise altitudes. The data is calculated based on flight idle thrust and a fixed airspeed of 240 KIAS.
  • Page 880 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL DESCENT - ALL ENGINES OPERATING FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES BLEED: OPEN AIRSPEED: 240 KIAS ISA CONDITIONS WEIGHT TOP OF DESCENT (FT) (LB) 5000 10000 15000 20000 25000 FUEL...
  • Page 881 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - FLIGHT WITH LANDING GEAR DOWN The holding tables show indicated airspeed, Mach number, N1, fuel flow and fuel consumption for various weights and altitudes. Data is presented for ISA condition and all engines operating. The associated conditions are: - Flaps........UP - Landing Gear......DOWN...
  • Page 882 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - ALL ENGINES OPERATING FLIGHT WITH LANDING GEAR DOWN AE3007A1 and A1P ENGINES BLEED: OPEN ANTI ICE: OFF MINIMUM FUEL CONSUMPTION SPEED STANDARD ATMOSPHERE WEIGHT ALTITUDE (FT) (LB) 1500 5000 10000 15000...
  • Page 883 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL FLIGHT WITH FLAPS LOCKED AT 9° This section presents climb, cruise, descent and holding data for flight with all engines operating and the flaps locked at 9°. This set of data may be used in the following situations: −...
  • Page 884 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 5000 AND 6000 FT SPEED SCHEDULE: 190 KIAS ALL ENGINES OPERATING BLEED: OPEN 5000 FT 6000 FT WEIGHT...
  • Page 885 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 7000 AND 8000 FT SPEED SCHEDULE: 190 KIAS ALL ENGINES OPERATING BLEED: OPEN 7000 FT 8000 FT WEIGHT...
  • Page 886 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 9000 AND 10000 FT SPEED SCHEDULE: 190 KIAS ALL ENGINES OPERATING BLEED: OPEN 9000 FT 10000 FT WEIGHT...
  • Page 887 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 11000 AND 12000 FT SPEED SCHEDULE: 190 KIAS ALL ENGINES OPERATING BLEED: OPEN 11000 FT 12000 FT WEIGHT...
  • Page 888 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 13000 AND 14000 FT SPEED SCHEDULE: 190 KIAS ALL ENGINES OPERATING BLEED: OPEN 13000 FT 14000 FT WEIGHT...
  • Page 889 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 15000 AND 16000 FT SPEED SCHEDULE: 190 KIAS ALL ENGINES OPERATING BLEED: OPEN 15000 FT 16000 FT WEIGHT...
  • Page 890 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 17000 AND 18000 FT SPEED SCHEDULE: 190 KIAS ALL ENGINES OPERATING BLEED: OPEN 17000 FT 18000 FT WEIGHT...
  • Page 891 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CLIMB PLANNING - FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES ALTITUDE: SEA LEVEL TO 19000 AND 20000 FT SPEED SCHEDULE: 190 KIAS ALL ENGINES OPERATING BLEED: OPEN 19000 FT 20000 FT WEIGHT...
  • Page 892 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CRUISE - FLIGHT WITH FLAPS LOCKED AT 9° The Long Range Cruise and Maximum Speed Cruise tables show N1, fuel flow, indicated airspeed, true airspeed, indicated Mach number, buffet margin and specific range. Data is presented for ISA conditions and various weights, with corrections for ISA deviations.
  • Page 893 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES ALTITUDE: 5000 FT TO 12000 FT BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 6000...
  • Page 894 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES ALTITUDE: 13000 FT TO 20000 FT BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 13000 14000 15000 16000 17000 18000 19000 20000 72.3...
  • Page 895 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES ALTITUDE: 5000 FT TO 12000 FT BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 6000...
  • Page 896 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES ALTITUDE: 13000 FT TO 20000 FT BLEED: OPEN ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 13000 14000 15000 16000 17000 18000 19000 20000 75.6...
  • Page 897 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-05-40 MARCH 28, 2002...
  • Page 898 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL DESCENT - FLIGHT WITH FLAPS LOCKED AT 9° The descent table shows fuel consumption, distance and time from the top of descent to sea level for various cruise altitudes. The data is calculated based on flight idle thrust and a fixed airspeed of 240 KIAS.
  • Page 899 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL DESCENT - ALL ENGINES OPERATING FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES BLEED: OPEN AIRSPEED: 240 KIAS ISA CONDITIONS WEIGHT TOP OF DESCENT (FT) (LB) 5000 10000 15000 20000 FUEL...
  • Page 900 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - FLIGHT WITH FLAPS LOCKED AT 9° The holding tables show indicated airspeed, Mach number, N1, fuel flow and fuel consumption for various weights and altitudes. Data is presented for ISA condition and all engines operating. The associated conditions are: - Flaps ........
  • Page 901 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL HOLDING - ALL ENGINES OPERATING FLIGHT WITH FLAPS LOCKED AT 9° AE3007A1 and A1P ENGINES BLEED: OPEN ANTI ICE: OFF MINIMUM FUEL CONSUMPTION SPEED STANDARD ATMOSPHERE WEIGHT ALTITUDE (FT) (LB) 1500 5000 10000...
  • Page 902 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-05-40 MARCH 28, 2002...
  • Page 903 FLIGHT PLANNING AIRPLANE EMB-145 A1 LB FAA OPERATIONS MANUAL INFLIGHT DIVERSION These charts are provided for the pilots to determine if the fuel remaining is enough to complete the trip at Long Range Cruise (LRC) mode from one point in cruise to an alternate airport. The charts also enable rapid determination of fuel and time required to proceed to an alternate airport.
  • Page 904 FLIGHT PLANNING AIRPLANE EMB-145 A1 LB FAA OPERATIONS MANUAL EMB-145 INFLIGHT DIVERSION AE3007A1 ENGINE LONG RANGE CRUISE ISA CONDITION 9500 9000 BASED ON: MMO/250/240 DESCENT 8500 8000 7500 7000 FL200 FL250 6500 FL300 FL350 & ABOVE 6000 5500 5000 4500 4000 3500 3000...
  • Page 905 FLIGHT PLANNING AIRPLANE EMB-145 A1 LB FAA OPERATIONS MANUAL EMB-145 INFLIGHT DIVERSION TIME AE3007A1 ENGINE LONG RANGE CRUISE ISA CONDITION BASED ON: MMO/250/240 DESCENT FL200 FL250 FL300 FL350 & ABOVE REF. LINE 1000 1200 1400 1600 DISTANCE FROM POINT OF DIVERSION TO ALTERNATE - NM 145AOM1054503B - 22FEB2001 Page Code...
  • Page 906 FLIGHT PLANNING AIRPLANE EMB-145 A1 LB FAA OPERATIONS MANUAL FLIGHT OVER MOUNTAINOUS AREA Two situations must be considered when flying over mountainous areas, in order to clear route obstacles: Engine Failure For most normal cruise weights and altitudes, an airplane will not be able to maintain its cruise altitude following an engine failure, and will begin to descend (driftdown).
  • Page 907 FLIGHT PLANNING AIRPLANE EMB-145 A1 LB FAA OPERATIONS MANUAL Regulations (FAR 121.191 / EU OPS 1.500) require that the airplane be able to clear all terrain by a given margin when an engine fails. Two means of compliance for en-route obstacle clearance are allowed: –...
  • Page 908 FLIGHT PLANNING AIRPLANE EMB-145 A1 LB FAA OPERATIONS MANUAL Depressurization The following charts present the passenger chemical oxygen generator descent profile. In case of an emergency descent, the airplane path must be at or below the generator profile in order to ensure sufficient supplemental breathing oxygen to the passengers.
  • Page 909 FLIGHT PLANNING AIRPLANE EMB-145 A1 LB FAA OPERATIONS MANUAL 22 MINUTE CHEMICAL OXYGEN GENERATOR DESCENT PROFILE 38000 36000 34000 32000 30000 28000 26000 24000 22000 20000 18000 16000 14000 12000 10000 11 12 Time (min) EM145AOM050046A.DGN Page Code 1-05-45 REVISION 39...
  • Page 910 FLIGHT PLANNING AIRPLANE EMB-145 A1 LB FAA OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-05-45 REVISION 39...
  • Page 911 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL FLIGHT WITH ENGINE ANTI ICE VALVE LOCKED OPEN This section presents altitude capability and cruise data for flight with all engines operating and the Engine Anti Ice Valve Locked Open according to DDPM procedure (30-21-01).
  • Page 912 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CRUISE - ALTITUDE CAPABILITY TABLE The table below permits quick determination of the altitude capability, based on the initial cruise weight. The table data are presented for various ISA conditions, all engines operating and Maximum Speed Cruise schedule.
  • Page 913 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL CRUISE TABLES The long range cruise and maximum speed cruise tables show N1, fuel flow, indicated airspeed, true airspeed, indicated Mach number, buffet margin and specific range. Data are presented for various weights in ISA conditions and corrections for ISA deviation.
  • Page 914 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 5000 FT TO 18000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 10000 11000 12000 13000 14000 15000 16000 17000 18000...
  • Page 915 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 5000 FT TO 18000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 10000 11000 12000 13000 14000 15000 16000 17000 18000...
  • Page 916 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 5000 FT TO 18000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 10000 11000 12000 13000 14000 15000 16000 17000 18000...
  • Page 917 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 19000 FT TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000 22000 23000 24000 25000 26000 27000 28000...
  • Page 918 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 19000 FT TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000 22000 23000 24000 25000 26000 27000 28000...
  • Page 919 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 19000 FT TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000 22000 23000 24000 25000 26000 27000 28000...
  • Page 920 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 29000 FT TO 37000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 29000 30000 31000 32000 33000 34000 35000 36000 37000...
  • Page 921 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 29000 FT TO 37000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 29000 30000 31000 32000 33000 34000 35000 36000 37000...
  • Page 922 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL LONG RANGE CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 29000 FT TO 37000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 29000 30000 31000 32000 33000 34000 35000 36000 37000...
  • Page 923 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 5000 FT TO 18000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 10000 11000 12000 13000 14000 15000 16000 17000 18000...
  • Page 924 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 5000 FT TO 18000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 10000 11000 12000 13000 14000 15000 16000 17000 18000...
  • Page 925 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 5000 FT TO 18000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 5000 10000 11000 12000 13000 14000 15000 16000 17000 18000...
  • Page 926 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 19000 FT TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000 22000 23000 24000 25000 26000 27000 28000...
  • Page 927 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 19000 FT TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000 22000 23000 24000 25000 26000 27000 28000...
  • Page 928 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 19000 FT TO 28000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 19000 20000 21000 22000 23000 24000 25000 26000 27000 28000...
  • Page 929 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 29000 FT TO 37000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 29000 30000 31000 32000 33000 34000 35000 36000 37000...
  • Page 930 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 29000 FT TO 37000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 29000 30000 31000 32000 33000 34000 35000 36000 37000...
  • Page 931 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL MAXIMUM SPEED CRUISE - ALL ENGINES OPERATING AE3007A1 and AE3007A1P ENGINES ALTITUDE: 29000 FT TO 37000 FT CRUISE CONFIGURATION BLEED: OPEN ANTI ICE: ON (Engine or all) ISA CONDITION WEIGHT ALTITUDE (FT) (LB) 29000 30000 31000 32000 33000 34000 35000 36000 37000...
  • Page 932 FLIGHT PLANNING AIRPLANE EMB-145 A1 and A1P LB OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-05-50 REVISION 38...
  • Page 933 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL SECTION 1-06 WEIGHT AND BALANCE TABLE OF CONTENTS Page Block Introduction ................1-06-00 Standard Terms and Definitions ..........1-06-10 General Data................1-06-15 Index System ................1-06-30 Center of Gravity Curtailments........... 1-06-40 Balance Chart ................1-06-50 Sample Balance Chart (*) ............
  • Page 934 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL INTRODUCTION This Section contains information equivalent to the Weight and Balance manual and is intended to assist the operator in defining the weight and balance system and constrained CG limits. Page Code 1-06-00 REVISION 17...
  • Page 935 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL STANDARD TERMS AND DEFINITIONS EQUIPPED EMPTY WEIGHT (EEW) OR MANUFACTURER EMPTY WEIGHT (MEW) It is the weight of structure, power plant, instruments, interior furnishings, systems, optional, portable, and emergency equipment and other items of equipment that are an integral part of the airplane configuration.
  • Page 936 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL PAYLOAD OR TOTAL TRAFFIC LOAD This is the weight of passengers, baggage and cargo. MAXIMUM ALLOWABLE PAYLOAD It is the maximum approved weight that can be loaded into the airplane. Maximum payload is the Maximum Zero Fuel Weight (MZFW) less Operational Empty Weight (OEW).
  • Page 937 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL MEAN AERODYNAMIC CHORD (MAC) This is the chord of an imaginary rectangular airfoil with the same area of the actual wing and which produces the same resulting force vectors of the actual wing. The aircraft forward and aft CG limits are referred to in terms of %MAC.
  • Page 938 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-06-10 SEPTEMBER 20, 1999...
  • Page 939 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL GENERAL DATA The general data presented in this section is intended to be used for specific weight and balance calculations and is equivalent to the information contained in the Weight & Balance Manual. MAXIMUM GROSS WEIGHTS...
  • Page 940 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL BALANCE REFERENCE SYSTEM (EMB-145 MODELS) BALANCE ARMS/BODY STATION Longitudinal location of the Centers of Gravity (CG) identified throughout this Manual regarding airplane and components will be referred to as Balance Arms. Balance Arms are the distance in inches from the Airplane Datum which is located at the zero station of the fuselage.
  • Page 941 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL BALANCE REFERENCE SYSTEM (ERJ-140 ER AND LR MODELS) BALANCE ARMS/BODY STATION Longitudinal location of the Centers of Gravity (CG) identified throughout this Manual regarding airplane and components will be referred to as Balance Arms. Balance Arms are the distance in inches from the Airplane Datum which is located at the zero station of the fuselage.
  • Page 942 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL BALANCE REFERENCE SYSTEM (EMB-135 ER AND LR MODELS) BALANCE ARMS/BODY STATION Longitudinal location of the Centers of Gravity (CG) identified throughout this Manual regarding airplane and components will be referred to as Balance Arms. Balance Arms are the distance in inches from the Airplane Datum which is located at the zero station of the fuselage.
  • Page 943 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL FUEL DATA FUEL DEFINITIONS USABLE FUEL - Is the fuel to be effectively consumed by the engines. UNUSABLE FUEL - Is the fuel remaining after total usable fuel has been consumed. DRAINABLE FUEL - Is that portion of fuel which can be drawn off through fuel drains with the airplane leveled.
  • Page 944 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL EMB-145 XR Model: Wing Tank VOLUME WEIGHT CG BALANCE ARM FUEL CATEGORY (US Gal) (lb) (in) UNUSABLE UNDRAINABLE 17.6 580.31 UNUSABLE DRAINABLE 60.8 580.31 TOTAL UNUSABLE 11.6 78.4 580.31 USABLE 1689.8 11434.8 596.57...
  • Page 945 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL ERJ-140 LR Model: VOLUME WEIGHT CG BALANCE ARM FUEL CATEGORY (US Gal) (lb) (in) UNUSABLE UNDRAINABLE 17.6 544.29 UNUSABLE DRAINABLE 60.8 544.29 TOTAL UNUSABLE 11.6 78.4 544.29 USABLE 1689.8 11434.8 560.55 NOTE: Fuel density may range from 6.550 to 6.770 lb/US Gal.
  • Page 946 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL MISCELLANEOUS FLUIDS (EMB-145 MODELS) WEIGHT BALANCE ARM FLUID (lb) (in) ENGINE OIL 53.0 879.13 APU OIL 1070.47 HYDRAULIC • 79.4 735.43 WITH THRUST REVERSER • 72.8 716.54 WITHOUT THRUST REVERSER LAVATORY CHEMICAL FLUID 15.4 810.24...
  • Page 947 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL PITCH TRIM SETTING NOTE: For takeoff when setting pitch trim to 8, first select 7 and stop trimming immediately when the value 8 is displayed. When setting pitch trim to 4, first select 5 and stop trimming immediately when the value 4 is displayed.
  • Page 948 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL PASSENGERS PASSENGER LOCATION The passenger location and respective balance arm are shown in the applicable Interior Arrangement (Section 1-07-30). Page Code 1-06-15 REVISION 37...
  • Page 949 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL PASSENGER WEIGHT Actual or average passenger weights may be used to compute passenger loads. Actual passenger weights should be used in case of flights carrying large groups of passengers whose average weight obviously does not conform with the normal standard weight such as athletic squads or other groups which are smaller or larger than the local average.
  • Page 950 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL FLIGHT CREW ITEMS (EMB-145 MODELS) WEIGHT BALANCE ARM ITEM (lb) (in) PILOT 145.08 COPILOT 145.08 OBSERVER 167.64 FWD ATTENDANT 185.00 AFT ATTENDANT 787.44 PILOT FLIGHT BAG 152.87 (ERJ-140 MODELS) WEIGHT BALANCE ARM ITEM (lb)
  • Page 951 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL (EMB-135 MODELS) WEIGHT BALANCE ARM ITEM (lb) (in) PILOT 145.08 COPILOT 145.08 OBSERVER 167.64 FWD ATTENDANT 185.00 AFT ATTENDANT 646.46 PILOT FLIGHT BAG 152.87 NOTE: - The adopted flight crew items are in accordance with the approved average weight, not including the respective carry- on baggage.
  • Page 952 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL INTENTIONALLY BLANK Page Code 1-06-15 REVISION 37...
  • Page 953 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL INDEX SYSTEM When determining the aircraft center of gravity position it is necessary to make calculations adding and/or subtracting the moment caused by each individual item loaded in the aircraft. Moment, per definition, is weight multiplied by the distance to a reference point.
  • Page 954 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL The Embraer recommended Index System formulas are: × − EMB-145 Models: 17400 × − ERJ-140 Models: 17400 × − EMB-135 Models: 17400 INDEX INFLUENCE Index influence is the variation of index when a body is loaded or unloaded from the aircraft.
  • Page 955 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL The following tables show the index influence for various items: INDEX INFLUENCE FOR EMB-145 MODELS Item Reference Index (in) Weight (lb) Influence Cargo / Baggage 889.76 + 0.017 IU/lb Forward Galley (*) 218.50 - 0.021 IU/lb Aft Galley (*)
  • Page 956 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL INDEX INFLUENCE FOR ERJ-140 MODELS Item Reference Index (in) Weight (lb) Influence Cargo / Baggage 833.66 + 0.016 IU/lb Forward Galley (*) 208.58 - 0.020 IU/lb Aft Galley (*) 258.26 - 0.017 IU/lb Wardrobe (*) 190.55...
  • Page 957 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL INDEX INFLUENCE FOR EMB-135 MODELS Item Reference Index (in) Weight (lb) Influence Cargo / Baggage 750.00 + 0.014 IU/lb Forward Galley (*) 190.55 - 0.019 IU/lb Aft Galley (*) 216.54 - 0.017 IU/lb Wardrobe (*) 216.54...
  • Page 958 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL FUEL INDEX VARIATION EMB-145 ER, EP AND MP MODEL Volume Weight Index (US Gal) (lb) (in) (IU) 575.28 -0.3 577.01 -0.5 1005 578.43 -0.7 1340 579.61 -0.8 1675 580.67 -0.9 2010 581.65 -1.0...
  • Page 959 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL EMB-145 LR MODEL Volume Weight Index (US Gal) (lb) (in) (IU) 570.00 -0.4 570.89 -0.7 1005 571.77 -1.1 1340 572.55 -1.3 1675 573.34 -1.6 2010 574.01 -1.8 2345 574.78 -2.1 2680 575.44 -2.2...
  • Page 960 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL EMB-145 XR MODEL Wing Tank Volume Weight Index (US Gal) (lb) (in) (IU) 570.00 -0.4 570.89 -0.7 1005 571.77 -1.1 1340 572.55 -1.3 1675 573.34 -1.6 2010 574.01 -1.8 2345 574.78 -2.1 2680...
  • Page 961 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL EMB-145 XR MODEL Ventral Tank Volume Weight Index (US Gal) (lb) (in) (IU) 689.17 1340 691.73 2010 693.78 12.0 2680 696.38 16.4 3350 696.85 20.6 4020 697.72 24.9 4690 698.31 29.2 5360 698.70...
  • Page 962 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL ERJ-140 ER MODEL Volume Weight Index (US Gal ) (lb) (in) (IU) 539.32 -0.2 540.95 -0.3 1005 542.36 -0.4 1340 543.55 -0.5 1675 544.62 -0.5 2010 545.59 -0.5 2345 546.49 -0.5 2680 547.34...
  • Page 963 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL ERJ-140 LR MODEL Volume Weight Index (US Gal) (lb) (in) (IU) 534.00 -0.3 534.83 -0.6 1005 535.68 -0.8 1340 536.50 -1.0 1675 537.30 -1.2 2010 538.02 -1.4 2345 538.73 -1.5 2680 539.40 -1.6...
  • Page 964 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL EMB-135 ER MODEL Volume Weight Index (US Gal) (lb) (in) (IU) 496.37 -0.4 498.00 -0.7 1005 499.41 -0.9 1340 500.60 -1.1 1675 501.67 -1.3 2010 502.64 -1.4 2345 503.54 -1.5 2680 504.39 -1.6...
  • Page 965 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL EMB-135 LR MODEL Volume Weight Index (US Gal) (lb) (in) (IU) 491.05 -0.5 491.88 -0.9 1005 492.73 -1.3 1340 493.55 -1.7 1675 494.35 -2.0 2010 495.07 -2.3 2345 495.78 -2.6 2680 496.45 -2.9...
  • Page 966 WEIGHT AND BALANCE AIRPLANE 145 140 135 LB OPERATIONS MANUAL OEW/OEI DETERMINATION The OEW (Operational Empty Weight) is the BEW plus the weight of the operational items (crew, catering, lavatory fluid, etc.). The OEI (Operational Empty Index) is the index for the OEW. In order to determine the OEW and OEI, it is necessary to add to the BEW all the weight and moment variations referent to the operational items.
  • Page 967 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL CENTER OF GRAVITY CURTAILMENTS The airplane weight and balance calculations are normally performed assuming that passengers are evenly distributed along the airplane cabin and that the crew, passengers and movable items are fixed in a pre-determined position.
  • Page 968 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL NOTE: For Ferry and Training flights, in which passenger or flight attendant movement is not an issue, a constrained center of gravity envelope without the seat and flight allowances may be used so as not to limit these types of flight unnecessarily. For flights with more than 33 or 45 passengers (with the unoccupied seats at the forward portion of the cabin), for EMB-135 and EMB-145, respectively, a constrained center of...
  • Page 969 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL EMB-145LR Forward Allowance Weight from Arm to Arm Moment (lb) (in) (in) (lb.in) Fwd attendant to cockpit 188.98 165.35 - 4017 AFT FLIGHT ALLOWANCES A reasonable aft flight allowance is to consider the movement of the forward flight attendant and a trolley to the aftermost row combined with the movement of a mid cabin passenger to the lavatory.
  • Page 970 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL EMB-145LR Aft Allowance Weight from Arm to Arm Moment (lb) (in) (in) (lb.in) Mid cabin pax to lavatory 170 * 522.83 811.02 +48992 attendant 188.98 748.02 +95037 cabin Trolley to aft cabin 218.50 767.72 +48331 Total = +192360...
  • Page 971 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL The seating allowance applied to the CG envelope is the sum of the largest moment variation of each cabin zone. The moment variation is defined by the difference between the actual pax distribution moment and the moment of the same amount of passengers concentrated in the centroid of the cabin zone considered.
  • Page 972 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL FUEL ALLOWANCES There are some conditions under which it is possible to have both ZFW-CG and TOW-CG located inside the CG envelope and the LW-CG outside of the CG envelope. This behavior is caused by the particular fuel loading characteristics of the aircraft, where the initial fuel loaded causes a forward moment and then higher fuel loading causes an aft moment (see the fuel index tables, where light fuel loads...
  • Page 973 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL EXAMPLE 1 (EMB-135 MODEL LR): For the EMB-135 LR on an option 1 configuration (37 seats), with the passenger cabin divided in three sections. Section A refers to rows 1 to 4, section B refers to rows 5 to 8 and section C refers to rows 9 to 13.
  • Page 974 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL FORWARD SEATING ALLOWANCE: Seat type & Arm Cab Arm Weight PAX Moment Accumul. Minimum row number (in) (in) (lb) Total (lb.in) (lb.in) Accumul. Windows 01 261.23 327.64 0.00 0.00 Windows 02 292.48 327.64 -6681.38 -6681.38 Windows 03 323.72...
  • Page 975 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL AFT SEATING ALLOWANCE: Seat type & Arm Cab Arm Weight PAX Moment Accumul. Maximum row number (in) (in) (lb) Total (lb.in) (lb.in) Accumul. Windows 13 645.42 598.53 17817.01 17817.01 Windows 12 614.17 598.53 5944.03 23761.05 Windows 11 582.89...
  • Page 976 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL FUEL ALLOWANCES: There are some conditions under which it is possible to have both ZFW-CG and TOW-CG located inside the CG envelope and the LW- CG outside of the CG envelope (see Figure 1). 48000 46000 44000...
  • Page 977 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL Forward limits Weight Index (lb) (in) (IU) 25353 529.67 30.0 34.3 27558 512.75 15.0 31967 512.75 15.0 35274 514.44 16.5 11.9 44092 519.63 21.1 24.7 Aft limits Weight Index (lb) (in) (IU) 25353 529.67 30.0 34.3 26455...
  • Page 978 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL EMB-135LR Constrained CG Envelope (Standard) 48000 46000 44000 42000 40000 38000 36000 34000 32000 30000 28000 26000 INDEX Figure 2 CONSTRAINED CENTER OF GRAVITY LIMITS In order to determine the constrained CG envelope, the allowances must be added to the certified CG envelope.
  • Page 979 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL Forward Center of Gravity Limits: AFM values Allow- Constrained values Mom. ance Mom. (lb) (in) (lb.in) (lb.in) (lb.in) (in) Takeoff & Landing & In-flight limits: 25353 30.0 529.67 13428724 -10155 13438879 530.07 30.4 27558 15.0 512.75 14130365 -83802 14214167 515.79 17.7 31967 15.0 512.75 16391079...
  • Page 980 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL EMB-135LR - CONSTRAINED ENVELOPE 45000 40000 35000 30000 25000 CG (%) Figure 3 The complete constrained CG envelope for the EMB-135LR is shown in Figure 4: Page Code 1-06-40 REVISION 29...
  • Page 981 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL EMB-135LR Constrained CG Envelope (Standard) 48000 46000 MTOW = 19990 lb 44000 42000 MLW = 18500 lb 40000 38000 MZFW = 16000 lb 36000 34000 32000 30000 28000 26000 INDEX Figure 4 1 - TOW limit (more than 33 paxs). 2 - TOW limit (with 33 paxs or less).
  • Page 982 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL EXAMPLE 2 (EMB-145 MODEL LR): For the EMB-145LR on a standard configuration (50 seats) with the passenger cabin divided in three sections. Section A refers to rows 1 to 6, section B refers to rows 7 to 12 and section C refers to rows 13 to 18.
  • Page 983 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL FORWARD SEATING ALLOWANCE: Seat type & Arm Cab Arm Weight PAX Moment Accumul. Maximum row number (in) (in) (lb) Total (lb.in) (lb.in) Accumul. Windows 01 245.87 341.89 -18243.21 -18243.21 Windows 02 277.11 341.89 -12306.71 -30549.92 Windows 03 308.40...
  • Page 984 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL AFT SEATING ALLOWANCE: Seat type & Arm Cab Arm Weight PAX Moment Accumul. Maximum row number (in) (in) (lb) Total (lb.in) (lb.in) Accumul. Windows 18 786.36 708.22 29692.51 29692.51 Windows 17 755.11 708.22 17819.53 47512.04 Windows 16 723.87...
  • Page 985 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL FUEL ALLOWANCES: There are some conditions under which it is possible to have both ZFW-CG and TOW-CG located inside the CG envelope and the LW-CG outside of the CG envelope (see Figure 1). 52000 50000 48000 46000...
  • Page 986 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL Forward limits Weight Index (lb) (in) (IU) 27337 608.64 30.0 42.3 29542 588.34 12.0 10.2 34170 588.34 12.0 38000 588.34 12.0 48501 595.56 18.4 28.5 Aft limits Weight Index (lb) (in) (IU) 27337 608.64 30.0 42.3 29542...
  • Page 987 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL EMB-145LR Constrained CG Envelope 52000 50000 48000 46000 44000 42000 40000 38000 36000 34000 32000 30000 28000 26000 INDEX Figure 2 CONSTRAINED CENTER OF GRAVITY LIMITS In order to determine the constrained CG envelope, the allowances must be added to the certified CG envelope.
  • Page 988 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL Forward Center of Gravity Limits: AFM values Allow- Constrained values Mom. ance Mom. (lb) (in) (lb.in) (lb.in) (lb.in) (in) Takeoff & Landing & In-flight limits: 27337 30.0 608.64 16638392 -10155 16648547 609.01 30.3 29542 12.0 588.34 17380740 -166944 17547684 593.99 17.0 34170 12.0 588.34 20103578 -166944 20270522 593.23 16.3...
  • Page 989 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL EMB-145LR - CONSTRAINED ENVELOPE 50000 45000 40000 35000 30000 25000 CG (%) Figure 3 The complete constrained CG envelope for the EMB-145LR is shown in Figure 4: Page Code 1-06-40 REVISION 29...
  • Page 990 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL EMB-145LR Constrained CG Envelope 52000 50000 MTOW = 48501 lb 48000 46000 44000 MLW = 42549 lb 42000 MZFW = 39462 lb 40000 38000 36000 34000 32000 30000 28000 26000 INDEX Figure 4 1 - TOW limit (more than 45 paxs). 2 - TOW limit (with 45 paxs or less).
  • Page 991 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL BALANCE CHART The balance chart is a document used to check whether the aircraft center of gravity is located within the approved limits. Balance charts may be prepared in two basic formats: • Diagram format: is a balance chart with vertical lines for the moment scales, in which the pitch between each line refers to a predetermined load.
  • Page 992 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL 6. Enter the Fuel Index table with the fuel weight and read the fuel index. 7. Enter the Fuel box with the fuel weight and index and draw the CG shift from the last position determined in step 3. 8.
  • Page 993 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL SAMPLE EMB-145 EP BALANCE CHART Page Code 1-06-50 JUNE 28, 2002...
  • Page 994 WEIGHT AND AIRPLANE BALANCE OPERATIONS MANUAL THIS PAGE IS LEFT BLANK INTENTIONALLY Page Code 1-06-50 SEPTEMBER 20, 1999...
  • Page 995 LOADING AIRPLANE OPERATIONS MANUAL SECTION 1-07 LOADING Introduction .................1-07-00 External Dimensions..............1-07-10 Cabin Cross Section ..............1-07-20 Interior Arrangement..............1-07-30 Carry-on baggage...............1-07-50 Baggage Door................1-07-60 Baggage Compartment...............1-07-70 Cargo Nets..................1-07-80 Live Animals Transportation ............1-07-90 Dry Ice Transportation ..............1-07-95 Page Code 1-07-00 REVISION 38...
  • Page 996 LOADING AIRPLANE OPERATIONS MANUAL INTRODUCTION This Section contains airplane dimensions, interior arrangement data for loading purposes and loading capacity information in the passenger cabin and baggage compartment. Instructions for loading and unloading the airplane, live animals and dry ice transportation are also included in this Section. Page Code 1-07-00...
  • Page 997 LOADING AIRPLANE OPERATIONS MANUAL EXTERNAL DIMENSIONS EMB-145 THREE VIEW DRAWING Page Code 1-07-10 REVISION 23...
  • Page 998 LOADING AIRPLANE OPERATIONS MANUAL EMB-145 GROUND CLEARANCES Vertical Clearance Maximum Minimum Fuselage Angle 1° 21’ 24” 0° 52’ 00” 1.598 m 1.481 m Main Door 5 ft 3 in 4 ft 10 in 0.480 m 0.360 m Main Door Open (1st step) 1 ft 7 in 1 ft 2¼...
  • Page 999 LOADING AIRPLANE OPERATIONS MANUAL EMB-145 DOOR CLEARANCES 145APM020052 Page Code 1-07-10 MARCH 30, 2001...
  • Page 1000 LOADING AIRPLANE OPERATIONS MANUAL EMB-145 DOOR CLEARANCES Page Code 1-07-10 JUNE 28, 2002...
  • Page 1001 LOADING AIRPLANE OPERATIONS MANUAL CABIN CROSS SECTION Page Code 1-07-20 SEPTEMBER 20, 1999...

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