Boeing 737-800 Flight Crew Operations Manual
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Boeing 737-800 Flight Crew Operations Manual

Boeing 737-800 Flight Crew Operations Manual

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Table of Contents

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Title Page
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Title Page
Volume 1
Title Page
This document has EAR data with Export Control Classification Numbers (ECCN) of: 9E991.
Export of this technology is controlled under the United States Export Administration
Regulations (EAR) (15 CFR 730-774). An export license may be required before it is used for
development, production or use by foreign persons from specific countries. The controller of this
data has the individual responsibility to abide by all export laws.
Copyright © 2006-2016 The Boeing Company. All rights reserved.
Boeing claims copyright in each page of this document only to the extent that the page contains
copyrightable subject matter. Boeing also claims copyright in this document as a compilation
and/or collective work.
This document includes proprietary information owned by The Boeing Company and/or one or
more third parties. Treatment of the document and the information it contains is governed by
contract with Boeing. For more information, contact The Boeing Company, P.O. Box 3707,
Seattle Washington 98124.
September 15, 2016
2
737-800
Flight Crew
Operations Manual
Egyptair
BOEING PROPRIETARY
Document Number D6-27370-866-EGP
Revision Number: 21
Revision Date: September 15, 2016

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Questions and answers

fox
March 6, 2025

apu shutdown procedures

0
1 comments:
Mr. Anderson
March 6, 2025

The APU shutdown procedures for the Boeing 737-800 are as follows:

1. Operate the APU for one full minute with no bleed air load before shutdown. This cooling period helps extend the APU's service life.
2. When the APU switch is moved to OFF:
- The APU generator is tripped.
- The APU bleed air valve closes.
- The APU GEN OFF BUS light extinguishes.
3. Shutdown occurs automatically after these steps.

These procedures ensure proper cooling and system protection.

This answer is automatically generated

0

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Summary of Contents for Boeing 737-800

  • Page 1 BOEING PROPRIETARY Copyright © 2006-2016 The Boeing Company. All rights reserved. Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter. Boeing also claims copyright in this document as a compilation and/or collective work.
  • Page 2 Intentionally Blank...
  • Page 3 Landing Gear ..........14 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 4 Warning Systems ......... 15 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 5 40757 YK993 SU-GDY 40758 YK994 SU-GDZ 40759 YK995 SU-GEA 40760 YK996 SU-GEB 40800 YK997 SU-GEC 40801 YK998 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.1.1...
  • Page 6 Registry Number Serial Number Number SU-GED 40802 YK999 SU-GEE 40803 YQ456 YW273 63692 YW273 YW274 63799 YW274 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 0.1.2 D6-27370-866-EGP September 15, 2016...
  • Page 7 Volume 2 contains systems information. The QRH contains all checklists necessary for normal and non-normal procedures as well as inflight performance data. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP...
  • Page 8 Quick Reference Handbook (QRH) – The QRH covers normal checklists, non– normal checklists, operational information, performance information necessary for inflight use (PI) on an expedited basis, and maneuvers. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 0.2.2...
  • Page 9 Note: An operating procedure, technique, etc., considered essential to emphasize. Information contained in notes may also be safety related. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 26, 2015 D6-27370-866-EGP 0.2.3...
  • Page 10 Example (without subordinate items): YZ008 - YZ014 CABIN TEMPERATURE selector.......... As needed CABIN AIR CONDITIONING..........As needed Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 0.2.4 D6-27370-866-EGP...
  • Page 11 In the following example, the PACK checklist is applicable to YZ008 - YZ014 only: PACK YZ008 - YZ014 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP 0.2.5...
  • Page 12 MOTOR DRIVEN POWER TRANSFER HYDRAULIC PUMP HYDRAULIC PUMP UNIT SPEAKER CLACKER WHEEL TURBINE THERMOSTAT DIAPHRAGM HORN BELL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 0.2.6 D6-27370-866-EGP...
  • Page 13 METER METER (PNEUMATIC) (FUEL) CHECK MANUALLY CONTROLLED VALVES SHUTTLE REMOTELY RELIEF REGULATED CONTROLLED RELIEF & RELIEF BYPASS Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 0.2.7...
  • Page 14 Preface - Introduction 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 18, 2011 0.2.8 D6-27370-866-EGP...
  • Page 15 Available Airplane Flight Manual (FAA approved) Above Ground Level Back Course Anti-Ice BARO Barometric Aileron BAT/BATT Battery Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.3.1...
  • Page 16 Descent FCTL Flight Control DISC Disconnect FCTM Flight Crew Training Distance Measuring Manual Equipment Force Fight Monitor Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 0.3.2 D6-27370-866-EGP...
  • Page 17 IDENT Identification Mode Control Panel Instrument Landing System Minimum Descent Altitude Inches MAX Display System INBD Inboard Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.3.3...
  • Page 18 OVRD Override Step Climb PASS Passenger Stabilized Approach Power Control Unit Monitor PERF INIT Performance Select Initialization Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 0.3.4 D6-27370-866-EGP...
  • Page 19 Trailing Edge Traffic THR HOLD Throttle Hold Takeoff TO/GA Takeoff/Go–Around UPR DSPL Upper Display Universal Time Coordinated Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.3.5...
  • Page 20 Preface - Abbreviations 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 26, 2015 0.3.6 D6-27370-866-EGP...
  • Page 21 The Boeing Company issues FCOM revisions to provide new or revised procedures and information. Formal revisions also incorporate appropriate information from previously issued FCOM bulletins. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 22 Preface - Model Identification page, or to show service bulletin airplane effectivity. Highlights are not supplied. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 0.4.2...
  • Page 23 Added text describing the updated Runway Surface Condition Correlation table, which now also shows the Runway Condition Code in reference to FAA AC 25-32. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 24 Preface - Revision Record 737 flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 0.4.4 D6-27370-866-EGP...
  • Page 25 L.10.3 - Added a note pointing out that the maximum weight values can be further limited per the AFM. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.4.5...
  • Page 26 NP.21.33 - Added configuration with auto T/O thrust reduction and without VNAV armed for takeoff. Approach Procedure NP.21.42 - Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 0.4.6 D6-27370-866-EGP...
  • Page 27 The autopilot is normally used per Boeing procedures, and so recommending autopilot use is redundant. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.4.7...
  • Page 28 SP.16.11 - Changed “may” to “can” for Boeing standardization. SP.16.11 - Changed “prior to” to “before” for Boeing standardization. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 0.4.8...
  • Page 29 ‘When maintaining an ATC assigned flight level (FL)’ and ‘While under ATC radar vectors’”. Also re-organized for better clarity. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 30 Section 10 - Takeoff 737-800WSFP1 CFM56-7B26 C M KG FAA CATC/N (FMC Model 737-800W.1) was added as Section 10. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 0.4.10...
  • Page 31 Section 16 - Gear Down, Engine Inop Added section "16". Section 17 - Text Added section "17". Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.4.11...
  • Page 32 1.40.2 - Added text which describes the Landing, Taxi, and Runway Turnoff Lights. 1.40.4 - Added a graphic which depicts the exterior lighting. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 0.4.12...
  • Page 33 4.10.19 - Added MCP panel with aural and visual indications when an autopilot engage attempt is made and is unsuccessful. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.4.13...
  • Page 34 6.10.4 - Added LED cabin lights for addition of Boeing Sky interior. 6.10.4 - Added flight deck door surveillance system to the list of IFE/PASS SEAT switch equipment. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 0.4.14...
  • Page 35 9.20.22 - Changed sentence from Wing LE and TE position indications come from the FSEU to Wing TE position indications come from the FSEU. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.4.15...
  • Page 36 10.16.9 - Added bullet about the inboard MFD switch position. 10.16.10 - Added bullet about the inboard MFD switch position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 0.4.16...
  • Page 37 11.32.5 - Deleted U10.5 and earlier FMC Alerting Message. Section 33 - Company Data Link Uplinks 11.33.5 - Added ACARS message annunciation option. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.4.17...
  • Page 38 11.60.3 - Deleted U10.5A and earlier FMC Alerting Message. 11.60.5 - Revised to include FMC U10.8A and later. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 0.4.18...
  • Page 39 15.20.29 - Deleted TCAS resolution advisory aural warnings no longer applies. TCAS resolution advisory aural warnings was applicable to airplanes equipped with TCAS 7.0. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 40 Preface - Revision Highlights 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 0.4.20 D6-27370-866-EGP...
  • Page 41 September 15, 2016 * 0.4.13 September 15, 2016 L.10.1 March 31, 2016 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.5.1...
  • Page 42 March 28, 2013 * NP.21.29 September 15, 2016 SP.4.1 September 24, 2015 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 0.5.2 D6-27370-866-EGP September 15, 2016...
  • Page 43 September 15, 2016 * SP.16.32 September 15, 2016 * SP.11.16 September 15, 2016 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.5.3...
  • Page 44 September 15, 2016 * PD.14.2 September 15, 2016 * PI.10.36 September 15, 2016 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 0.5.4 D6-27370-866-EGP September 15, 2016...
  • Page 45 September 15, 2016 * PI.12.24 September 15, 2016 * PI.12.25 September 15, 2016 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.5.5...
  • Page 46 September 15, 2016 * 1.40.39 September 15, 2016 * 1.30.17 September 15, 2016 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 0.5.6 D6-27370-866-EGP September 15, 2016...
  • Page 47 September 15, 2016 2.40.6 March 28, 2013 * 4.20.5 September 15, 2016 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.5.7...
  • Page 48 September 18, 2008 * 5.20.6 September 15, 2016 7.11.13 September 18, 2008 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 0.5.8 D6-27370-866-EGP September 15, 2016...
  • Page 49 September 15, 2016 8.20.1 September 18, 2008 9.20.19 September 26, 2013 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.5.9...
  • Page 50 September 15, 2016 * 10.11.39 September 15, 2016 * 10.16.14 September 15, 2016 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 0.5.10 D6-27370-866-EGP September 15, 2016...
  • Page 51 September 26, 2013 10.31.3 September 26, 2013 10.42.20 September 26, 2013 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.5.11...
  • Page 52 September 15, 2016 * 11.10.4 September 15, 2016 * 11.31.5 September 15, 2016 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 0.5.12 D6-27370-866-EGP September 15, 2016...
  • Page 53 September 15, 2016 * 11.33.4 September 15, 2016 * 11.33.51 September 15, 2016 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.5.13...
  • Page 54 September 15, 2016 11.34.30 September 24, 2015 * 11.34.77 September 15, 2016 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 0.5.14 D6-27370-866-EGP September 15, 2016...
  • Page 55 September 28, 2006 11.40.42 September 24, 2015 * 11.42.3 September 15, 2016 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.5.15...
  • Page 56 September 24, 2015 * 11.42.50 September 15, 2016 * 11.43.41 September 15, 2016 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 0.5.16 D6-27370-866-EGP September 15, 2016...
  • Page 57 September 26, 2013 14.20.8 September 26, 2013 12.10.3 September 23, 2010 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.5.17...
  • Page 58 September 15, 2016 * 15.20.27 September 15, 2016 * 15.20.28 September 15, 2016 * = Revised, Added, or Deleted Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 0.5.18 D6-27370-866-EGP September 15, 2016...
  • Page 59 QRH, the included pages should be filed as instructed in the Flight Crew Operations Manual Information section of the bulletin. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.6.1...
  • Page 60 Constraints following a runway change with a Standard Terminal Arrival (STAR) and the previous runway already executed in the Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 0.6.2 D6-27370-866-EGP September 15, 2016...
  • Page 61 Preface - Bulletin Record 737 Flight Crew Operations Manual Number Subject Date Status Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 0.6.3...
  • Page 62 Preface - Bulletin Record 737 Flight Crew Operations Manual Number Subject Date Status Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 0.6.4 D6-27370-866-EGP September 15, 2016...
  • Page 63 HUD indication of VREF+15 for a one engine inoperative flaps 15 landing. Use the EFIS Mach/Airspeed Indicator or PFD speed tape indication of VREF+20. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015...
  • Page 64 Bulletin status, to the 737 Manager, Flight Technical Data, through the Service Requests Application (SR App) on the MyBoeingFleet home page. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. B-2 Page 2 of 2...
  • Page 65 Service Bulletin information will be provided as soon as it is available. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015...
  • Page 66 Bulletin status, to the 737 Manager, Flight Technical Data, through the Service Requests Application (SR App) on the MyBoeingFleet home page. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. B-8 Page 2 of 2...
  • Page 67 Mod A MCU starting at Production Line Number 2169. .Boeing Service Letter 737-SL-34-191 provides information on the upgrade that corrects this anomaly. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 68 Bulletin status, to the 737 Manager, Flight Technical Data, through the Service Requests Application (SR App) on the MyBoeingFleet home page. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. B-16 Page 2 of 2...
  • Page 69 Insert this bulletin behind the Bulletin Record page in Volume 1 of your Flight Crew Operations Manual (FCOM). Amend the FCOM Bulletin Record page to show bulletin EGP-17 "In Effect" (IE). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 70 Bulletin status, to the 737 Manager, Flight Technical Data, through the Service Requests Application (SR App) on the MyBoeingFleet home page. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. B-17 Page 2 of 2...
  • Page 71 This design change is now available on production airplanes. Service bulletin information to support the planned AD will become available in mid- 2009. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 72 4. Reference to the steady horn in the condition statement will be deleted. The corresponding step in the procedure will be deleted. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. B-18 Page 2 of 4...
  • Page 73 AD. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 74 Bulletin status, to the 737 Manager, Flight Technical Data, through the Service Requests Application (SR App) on the MyBoeingFleet home page. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. B-18 Page 4 of 4...
  • Page 75 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015...
  • Page 76 Bulletin status, to the 737 Manager, Flight Technical Data, through the Service Requests Application (SR App) on the MyBoeingFleet home page. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. B-24 Page 2 of 2...
  • Page 77 With U10.8 or 10.8A installed, if unstable weather conditions are present prior to takeoff, consider not arming VNAV for takeoff. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015...
  • Page 78 Bulletin status, to the 737 Manager, Flight Technical Data, through the Service Requests Application (SR App) on the MyBoeingFleet home page. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. B-26 Page 2 of 2...
  • Page 79 This condition has been reported to occur during operation of the FMC FANS-1 ATS data link. The following is required for the condition to occur: Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 80 4. If HF datalink is present, select the HF radio to VOICE mode from DATA mode 5. Do not use ATS or AOC Datalink for the rest of the flight Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. B-27 Page 2 of 4 D6-27370-866-EGP...
  • Page 81 Bulletin status, to the 737 Manager, Flight Technical Data, through the Service Requests Application (SR App) on the MyBoeingFleet home page. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015...
  • Page 82 Flight Crew Operations Manual Bulletin No. EGP-27 R1, Dated June 5, 2013 (continued) Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. B-27 Page 4 of 4 D6-27370-866-EGP September 24, 2015...
  • Page 83 60 seconds. Slowing the acceleration rate of a heat soaked engine improves engine operability (stall margin) characteristics. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 84 Control Unit (73-21-60) - New Software Versions 7.B.WF3 for SAC and DAC Engines and 7.B.WF2 for SAC Engines” or Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. B-28 Page 2 of 4...
  • Page 85 Bulletin status, to the 737 Manager, Flight Technical Data, through the Service Requests Application (SR App) on the MyBoeingFleet home page. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015...
  • Page 86 Flight Crew Operations Manual Bulletin No. EGP-28 R1, Dated January 9, 2015 (continued) Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. B-28 Page 4 of 4 D6-27370-866-EGP September 24, 2015...
  • Page 87 This condition was introduced in U10.2 and is present in all versions of FMC software from U10.2 through U12. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016...
  • Page 88 Bulletin status, to the 737 Manager, Flight Technical Data, through the Service Requests Application (SR App) on the MyBoeingFleet home page. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. B-33 Page 2 of 2...
  • Page 89 QFE Selection ........L.10.7 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 90 Non–AFM Operational Information .....L.10.8 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 91 Assuming that the remaining items are available to the flight crew by reference, they do not need to be memorized. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 31, 2016 D6-27370-866-EGP L.10.1...
  • Page 92 Verify that an operational check of the flight deck door access system has been accomplished according to approved procedures once each flight day. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 L.10.2...
  • Page 93 79,242 Kilograms Maximum Takeoff Weight 79,015 Kilograms Maximum Landing Weight 66,360 Kilograms Maximum Zero Fuel Weight 62,731 Kilograms Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP L.10.3...
  • Page 94 # Autoland capability may only be used with flaps 30 or 40 and both engines operative. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 L.10.4...
  • Page 95 Engines and APU Engine Limit Display Markings Maximum and minimum limits are red. Caution limits are amber. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP L.10.5...
  • Page 96 # Holding in icing conditions with flaps extended is prohibited. In flight, do not extend the SPEED BRAKE lever beyond the FLIGHT DETENT. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 L.10.6...
  • Page 97 Non-AFM Operational Information Note: The following items are not AFM limitations, but are provided for flight crew information. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 98 Note: The following items are not AFM limitations, but are provided for flight crew information. Do not apply brakes until after touchdown. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 L.10.8...
  • Page 99 Descent Procedure ........NP.21.40 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 100 Secure Procedure ........NP.21.55 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 101 After engine start, the master caution system alerts the crew to warnings or cautions away from the normal field of view. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP NP.11.1...
  • Page 102 • airplane configuration • navigation. The general PM phase of flight responsibilities are: • checklist reading • communications Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 18, 2011 NP.11.2 D6-27370-866-EGP...
  • Page 103 When selecting a value on the MCP, verify that the respective value changes on the flight instruments, as applicable. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 D6-27370-866-EGP NP.11.3...
  • Page 104 Procedures. For example, preflight procedure details are in the Preflight Procedure - Captain and Preflight Procedure - First Officer. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 NP.11.4...
  • Page 105 737 Flight Crew Operations Manual Preflight and Postflight Scan Flow TYPICAL PANEL LOCATIONS ARE SHOWN. CAPTAIN ITEMS FIRST OFFICER ITEMS Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2007 D6-27370-866-EGP NP.11.5...
  • Page 106 LOCATIONS ARE SHOWN. CAPTAIN ITEMS FIRST OFFICER ITEMS INCLUDING: JOINT RESPONSIBILITY - AUDIO CONTROL ITEMS - TRIM Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2009 NP.11.6 D6-27370-866-EGP...
  • Page 107 LOCATIONS ARE SHOWN. FIRST OFFICER ITEMS CAPTAIN ITEMS INCLUDING: JOINT RESPONSIBILITY - AUDIO CONTROL - TRIM ITEMS Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 25, 2009 D6-27370-866-EGP NP.11.7...
  • Page 108 Normal Procedures - Introduction 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 NP.11.8 D6-27370-866-EGP...
  • Page 109 Verify that the ELT light is extinguished. PSEU light ............Verify extinguished GPS light ............Verify extinguished SERVICE INTERPHONE switch .......... OFF Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP NP.21.1...
  • Page 110 Circuit breakers (P6 panel) ..........Check Manual gear extension access door ........Closed Circuit breakers (control stand, P18 panel) ......Check Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 NP.21.2...
  • Page 111 Enter the FLIGHT NUMBER. Activate and execute the route. DEPARTURES page: Select the runway and departure routing. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP NP.21.3...
  • Page 112 Verify or enter an engine out acceleration height. Verify or enter a thrust reduction altitude. Verify that the preflight is complete. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.4...
  • Page 113 • the antennas are not damaged • the light lenses are clean and not damaged For cold weather operations see the Supplementary Procedures. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 114 Gear strut and doors ............... Check Nose wheel steering assembly ............Check Nose gear steering lockout pin ..........As needed Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.6...
  • Page 115 Leading edge flaps and slats ............Check Fuel measuring sticks ............Flush and secure Wing Surfaces ................Check Fuel tank vent ................Check Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.7...
  • Page 116 Probes, sensors, ports, vents, and drains (as applicable) ....Check APU air inlet ..................Open Tail Vertical stabilizer and rudder ............Check Elevator feel probes................ Check Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.8 D6-27370-866-EGP...
  • Page 117 Static discharge wicks ..............Check Position and strobe lights ............... Check Left Wing and Leading Edge Fuel tank vent ................Check Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.9...
  • Page 118 Flight SPOILER switches – Guards closed YAW DAMPER switch – ON Verify that the YAW DAMPER light is extinguished. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.10...
  • Page 119 Verify that the main tank fuel pump LOW PRESSURE lights are illuminated. Electrical panel ..................Set BATTERY switch – Guard closed CAB/UTIL power switch – ON Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.11...
  • Page 120 APU running. This can be mistaken by the ground crew as an APU fire. TEST switch – Hold to OVHT/FIRE Verify that the fire warning bell sounds. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.12 D6-27370-866-EGP...
  • Page 121 453 kgs. CAUTION: Do not operate the center tank fuel pumps with the flight deck unattended. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 122 ENGINE ANTI–ICE switches ............OFF Verify that the COWL ANTI–ICE lights are extinguished. Verify that the COWL VALVE OPEN lights are extinguished. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.14...
  • Page 123 Verify that the MANUAL light is extinguished. Lighting panel ..................Set YK981 - YQ456 LANDING light switches – RETRACT and OFF Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.15...
  • Page 124 TRAFFIC switch – As needed WEATHER RADAR – Off Verify that the weather radar indications are not shown on the MAP. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.16 D6-27370-866-EGP...
  • Page 125 MAIN PANEL DISPLAY UNITS selector – NORM LOWER DISPLAY UNIT selector – NORM TAKEOFF CONFIG light (if installed and operative) ........Verify extinguished Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.17...
  • Page 126 YK995 - YQ456 RUNWAY INHIBIT switch – Guard closed Verify that the GROUND PROXIMITY INOP light is extinguished. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.18...
  • Page 127 Master FIRE WARN light – Push Verify that the master FIRE WARN lights are extinguished. Verify that the fire warning bell cancels. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 128 Adjust the rudder pedals to allow full rudder pedal and brake pedal movement. Seat belt and shoulder harness ............Adjust Do the PREFLIGHT checklist on the captain’s command. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.20 D6-27370-866-EGP...
  • Page 129 FLIGHT DIRECTOR switch – ON Move the switch for the pilot flying to ON first. Bank angle selector – As needed Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 130 MAIN PANEL DISPLAY UNITS selector – NORM LOWER DISPLAY UNIT selector – NORM TAKEOFF CONFIG light (if installed and operative) ........Verify extinguished Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.22 D6-27370-866-EGP...
  • Page 131 Verify that the flight instrument indications are correct. Verify that no flags or messages are shown. Standby RMI ..................Set Select either VOR or ADF. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.23...
  • Page 132 Whenever the seat is adjusted, verify a positive horizontal (fore and aft) seat lock by pushing against the seat. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.24...
  • Page 133 Taxi and Takeoff briefings ........Complete C, F/O The pilot who will do the takeoff does the taxi and takeoff briefings. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.25...
  • Page 134 AFT and FORWARD FUEL PUMPS switches – ON Verify that the LOW PRESSURE lights are extinguished. Hydraulic panel ............... Set Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.26...
  • Page 135 Pushback or Towing Procedure The Engine Start procedure may be done during pushback or towing. Establish communications with ground handling personnel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 136 • if fuel is shutoff accidentally (by closing the engine start lever) do not reopen the engine start lever in an attempt to restart the engine Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.28...
  • Page 137 1% in approximately 5 seconds. Engine start lever ........IDLE detent Monitor fuel flow and EGT indications. C, F/O Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.29...
  • Page 138 Make slow and deliberate inputs, one direction at a time. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.30...
  • Page 139 • run the engines for at least 2 minutes • use a thrust setting normally used for taxi operations. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.31...
  • Page 140 Set the weather radar display as needed. Set the terrain display as needed. Call “BEFORE TAKEOFF Do the BEFORE TAKEOFF checklist. CHECKLIST.” Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.32 D6-27370-866-EGP...
  • Page 141 Call "THRUST SET". After takeoff thrust is set, the captain’s hand must be on the thrust levers until V1. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.33...
  • Page 142 “VNAV.” Push the VNAV switch. Engage the autopilot when above the minimum altitude for autopilot engagement. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.34 D6-27370-866-EGP...
  • Page 143 CAUTION: Do not allow the shoulder harness straps to retract quickly. Buckles can pull or damage circuit breakers. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 144 Call "THRUST SET". After takeoff thrust is set, the captain’s hand must be on the thrust levers until V1. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.36...
  • Page 145 Set the FLAP lever as directed. Engage the autopilot when above the minimum altitude for autopilot engagement. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.37...
  • Page 146 “5” “1” V2 + 15 “1” “1” Limit bank angle to 15° until reaching V2 + 15 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.38 D6-27370-866-EGP...
  • Page 147 SP.1. Before the top of descent, modify the active route as needed for the arrival and approach. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.39...
  • Page 148 Enter VREF on the APPROACH REF page. page. Set the RADIO/BARO minimums as needed for the approach. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.40 D6-27370-866-EGP...
  • Page 149 Set the AUTO BRAKE select switch to the needed brake setting. Do the approach briefing. Call “DESCENT CHECKLIST.” Do the DESCENT checklist. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.41...
  • Page 150 Update the arrival and approach, as needed. Update the approach briefing as needed. Call “APPROACH CHECKLIST.” Do the APPROACH checklist. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.42 D6-27370-866-EGP...
  • Page 151 Selected Flaps “UP” “1” “1” “5” “5” “15” “15” 30 or 40 (VREF30 or VREF40) + wind additives Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.43...
  • Page 152 Verify that the localizer is captured. Verify the final approach course heading. Call “GLIDESLOPE ALIVE.” Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.44 D6-27370-866-EGP...
  • Page 153 For a dual channel approach, disengage the autopilot after touchdown. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.45...
  • Page 154 The airplane can then descend on the VNAV path with the localizer not captured. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.46...
  • Page 155 At the final approach fix: • verify the crossing altitude • crosscheck the altimeters. Verify they agree within 100 feet. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 156 Maintain the glide path to landing. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.48 D6-27370-866-EGP...
  • Page 157 Set the landing gear lever to OFF after landing gear retraction is complete. Set the engine start switches as needed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 158 737 Flight Crew Operations Manual Pilot Flying Pilot Monitoring Call “AFTER TAKEOFF Do the AFTER TAKEOFF checklist. CHECKLIST.” Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.50 D6-27370-866-EGP...
  • Page 159 Before taxi speed, disarm the autobrake. Use manual braking as needed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.51...
  • Page 160 Shutdown Procedure Start the Shutdown Procedure after taxi is complete. Parking brake ..............Set C or F/O Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.52 D6-27370-866-EGP...
  • Page 161 CAUTION: Do not hold or turn the nose wheel steering wheel during pushback or towing. This can damage the nose gear or the tow bar. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 162 After the wheel chocks are in place: Parking brake – Release C or F/O APU switch ............As needed Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.54 D6-27370-866-EGP...
  • Page 163 YK981 - YQ456 EFB POWER switch ............ Push C, F/O Call “SECURE CHECKLIST.” Do the SECURE checklist. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP NP.21.55...
  • Page 164 Normal Procedures - Amplified Procedures 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 NP.21.56 D6-27370-866-EGP...
  • Page 165 Anti–Ice Operation........SP.3.1 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 166 Weight and Balance ....... . .SP.5.1 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 167 Fast Realignment ........SP.11.3 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 168 VNAV Climb ........SP.11.15 Intervention of FMC Cruise Altitude during VNAV Cruise SP.11.16 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. SP.TOC.4...
  • Page 169 Fuel Load Distribution ......SP.12.4 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 170 Hot Weather Operation....... .SP.16.17 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 171 Ice Crystal Icing Suspected ......SP.16.30 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 172 Supplementary Procedures - Table of Contents 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. SP.TOC.8 D6-27370-866-EGP September 15, 2016...
  • Page 173 Supplementary procedures are provided by section. Section titles correspond to the respective chapter title for the system being addressed except for the adverse weather section. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 D6-27370-866-EGP...
  • Page 174 Supplementary Procedures - Introduction 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 SP.05.2 D6-27370-866-EGP...
  • Page 175 Flight deck door lock selector.............UNLKD Flight deck access system switch ............. OFF Verify LOCK FAIL light illuminates. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. May 15, 2008 D6-27370-866-EGP SP.1.1...
  • Page 176 Tank drain valve handle ..........CLOSED Water service panel ...............Close Drain line .......... Disconnect from drain ports Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. May 15, 2008 SP.1.2 D6-27370-866-EGP...
  • Page 177 Unless otherwise authorized, start the APU before the ETOPS segment. The APU must be on for the entire ETOPS segment. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.1.3...
  • Page 178 Verify that the VALVE OPEN light illuminates bright, then dim. Crossfeed selector ..............Close Verify that the VALVE OPEN light illuminates bright, then extinguishes. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.1.4 D6-27370-866-EGP...
  • Page 179 If external air cannot hold 20 psi minimum and the APU is operating: ISOLATION VALVE switch ..........AUTO Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 180 PACK switches ..................OFF Pressurization mode selector ............MAN AUTO FAIL and ALTN lights – extinguished. MANUAL light – illuminated. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.2.2 D6-27370-866-EGP...
  • Page 181 During Descent Thrust lever changes should be made as slowly as possible to prevent excessive pressure bumps. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.2.3...
  • Page 182 PACK switches ................AUTO ISOLATION VALVE switch ............CLOSE Engine BLEED air switches..............OFF APU BLEED air switch ..............OFF Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.2.4 D6-27370-866-EGP...
  • Page 183 APU BLEED air switch ..............ON Engine No. 2 BLEED air switch ............OFF Trim Air Switch .................. ON Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 184 Engine No. 1 BLEED air switch ..........OFF APU BLEED air switch ............ON Engine No. 2 BLEED air switch ..........OFF Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.2.6...
  • Page 185 Surfaces..................Check Visually inspect the lower and upper wing surfaces. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.3.1...
  • Page 186 Exterior Safety Inspection - Airplanes without Defined Cold-Soaked Fuel Frost Area Surfaces ..................Check Visually inspect the lower and upper wing surfaces. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.3.2 D6-27370-866-EGP...
  • Page 187 If any frost is present on the upper wing surface, all snow, ice and frost on the wings must be removed using appropriate deicing/anti-icing procedures. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 188 If any ON light remains extinguished, the window heat system is inoperative. Observe the maximum airspeed limit of 250 kts below 10,000 feet. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 28, 2013 SP.3.4...
  • Page 189 V/S thumbwheel ........Set desired vertical speed Verify FMA display: Thrust mode (climb or descent) – MCP SPD Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.4.1...
  • Page 190 If the airplane is 50 nm or less from T/D, if a lower altitude is selected, an early descent will be started. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.4.2...
  • Page 191 Heading selector ............Set desired heading Heading select switch ............... Push Verify FMA display: Roll mode – HDG SEL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.4.3...
  • Page 192 Note: When using LNAV to intercept a localizer, LNAV might parallel the localizer without capturing it. Use HDG SEL to intercept the final approach course, if needed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.4.4...
  • Page 193 Set desired V/S to descend to MDA(H). Use a V/S that results in no level flight segment at MDA(H). Verify V/S mode annunciates. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 194 Accomplish an instrument approach, establish suitable visual reference and level off at MCP altitude. Verify ALT HLD or VNAV ALT mode annunciates. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.4.6...
  • Page 195 • 2 Radio Altimeters • 2 ADIRUs, IRSs in NAV mode * • 2 EFIS/MAP or PFD/ND displays (as installed) * Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 196 No other lateral or vertical modifications after the IAF may be made. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.4.8 D6-27370-866-EGP...
  • Page 197 One pilot must have the map display in 10 NM range or less to monitor path tracking during the final approach segment. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP SP.4.9...
  • Page 198 At the final approach fix, verify the crossing altitude and crosscheck the altimeters (maximum 100 feet difference between primary altimeters). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 26, 2015 SP.4.10...
  • Page 199 Maintain the glide path to landing. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.4.11...
  • Page 200 Supplementary Procedures - Automatic Flight 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 26, 2015 SP.4.12 D6-27370-866-EGP...
  • Page 201 If the Takeoff Data numeric and alphabetic values are different, the flight crew must not accept the Takeoff Data message. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 25, 2010 D6-27370-866-EGP SP.5.1...
  • Page 202 Hold switch for 5 seconds. Observe that the STATUS light flashes once. A tone may be heard through a headset plugged into the headset jack. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.5.2...
  • Page 203 OVERHEAT DETECTOR switches – NORMAL TEST switch – Hold to FAULT/INOP Verify that the MASTER CAUTION lights are illuminated. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 204 AC powered fuel pump ON. This will extend the service life of the APU fuel control unit. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.6.2...
  • Page 205 Delay approximately 2 minutes after the APU GEN OFF BUS light extinguishes before placing the BATTERY switch OFF. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 206 Note: It may take up to 3 minutes for CDS displays to recover when power is interrupted for more than 2 seconds on the ground. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.6.4...
  • Page 207 TEST switch - Hold to FAULT/INOP TEST switch - Hold to OVHT/FIRE EXTINGUISHER TEST switch - Check Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.7.1...
  • Page 208 When cleared for Engine Start, do the following: Air conditioning PACK switches ..........OFF ANTICOLLISION light switch ..........ON Ignition select switch ............IGN-R Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.7.2 D6-27370-866-EGP...
  • Page 209 PSEU light ............Verify extinguished GPS light ............Verify extinguished SERVICE INTERPHONE switch .......... OFF Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.7.3...
  • Page 210 When cleared to start: APU BLEED air switch ............OFF Engine No. 1 start ............Accomplish Use normal start procedures. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.7.4 D6-27370-866-EGP...
  • Page 211 FMC computed value or 104% if the FMC has not calculated an input since power up. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 212 Supplementary Procedures - Engines, APU 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.7.6 D6-27370-866-EGP...
  • Page 213 Fire and Overheat System Test with an Inoperative Loop YW273, YW274 To determine the specific inoperative loop: OVHT DET switches..............A Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP SP.8.1...
  • Page 214 Test switch ..............OVHT/FIRE If the test is successful leave the fire panel in this configuration for flight. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.8.2...
  • Page 215 Between 29,000 feet and the maximum operating altitude, differences greater than 500 feet should be suspect and verified by ground maintenance checks. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 216 If it is not possible to identify which altimeter is indicating the correct altitude: ATC ..................Notify Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 27, 2012 SP.10.2 D6-27370-866-EGP...
  • Page 217 Speed reference selector (inner) ........Set Set speed as desired. Speed reference selector (outer) ..........SET Digital readout is removed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.10.3...
  • Page 218 Speed reference selector (inner) ........Set Set speed as desired. Speed reference selector (outer) ..........SET Digital readout is removed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.10.4 D6-27370-866-EGP...
  • Page 219 If HUD will be used for approach and landing, accomplish the following steps: Prior to completing the DESCENT checklist: HUD System ................Set Combiner – Lowered, cover removed Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP SP.10.5...
  • Page 220 Accomplish the following step during the Shutdown Procedure: HUD Combiner ................Stowed If the airplane will be secured, install cover before stowing. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.10.6...
  • Page 221 Verify test pattern consisting of the following colors appears: • Green • Yellow • Red • Magenta. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.11.1...
  • Page 222 (approximately 30 seconds.) IRS ..................NAV Rotate IRS Mode Selector to NAV and verify ALIGN light illuminated. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.11.2 D6-27370-866-EGP...
  • Page 223 IRS mode selectors ..............OFF Observe ALIGN lights extinguish. After ALIGN lights extinguish, initiate a full alignment. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.11.3...
  • Page 224 RTE LEGS page ................Select On page 1/XX, line 1L, enter desired waypoint over the presently active waypoint. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.11.4...
  • Page 225 Correct any ROUTE DISCONTINUITY. EXEC key ..................Push Observe MOD RTE or MOD RTE LEGS page changes to ACT. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 226 ACTIVATE line select key ............... Push Correct any ROUTE DISCONTINUITY. EXEC key ..................Push Route Removal RTE page ..................Select Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.11.6 D6-27370-866-EGP...
  • Page 227 Correct by entering a lower CRZ ALT on the CLB page. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 228 LNAV guidance may be temporarily interrupted while sequencing the hold exit waypoint. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.11.8...
  • Page 229 REF NAV DATA pages are stored in the temporary navigation data base for one flight only. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 230 Deleting Created Waypoints on the Nav Data Pages INIT/REF key .................. Push Observe the INDEX prompt displayed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.11.10 D6-27370-866-EGP...
  • Page 231 Observe the MOD RTE LEGS page changes to ACT. Note: These created waypoints are stored in the temporary navigation data base for one flight only. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 232 ARRIVAL page ................Select STAR or PROFILE DESCENT (if required) ......... Select TRANSITION (if required) ............Select Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.11.12 D6-27370-866-EGP...
  • Page 233 GPS-R INVALID messages are shown in the scratch pad, or course deviation is suspected, do the following as necessary to ensure navigation accuracy: Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 234 PROG page ..................Select Observe NAV STATUS prompt displayed. NAV STATUS page ................ Select Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.11.14 D6-27370-866-EGP...
  • Page 235 MCP altitude selector ............. Set new altitude New altitude must be higher than the FMC altitude constraint(s) to be deleted. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 236 If all FMC altitude constraints are deleted, the descent mode will revert to a VNAV speed descent. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.11.16...
  • Page 237 Observe MOD RTE LEGS page changes to ACT and restriction is deleted and replaced with an FMC predicted value (small size characters). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 238 DES, this will result in an idle thrust normal rate of descent. Step Climb or Descent from Cruise MCP altitude selector ................Set Set new level–off altitude. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.11.18 D6-27370-866-EGP...
  • Page 239 Observe the DATA prompt displayed. RTE DATA page ................Select Enter the estimated true wind direction/speed on the appropriate line(s). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.11.19...
  • Page 240 Refer to section 11.41 and 11.42 for a complete description of ENG OUT CLB and ENG OUT CRZ pages. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.11.20...
  • Page 241 Enter desired time error tolerance (5 to 30 seconds) for the RTA waypoint on line 1L (Example: 25). Observe MOD PERF LIMITS page displayed and EXEC key illuminated. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 242 RTE page ................Select RWY..................Enter Reenter runway on RTE page. Check and reenter other performance data as required. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.11.22 D6-27370-866-EGP...
  • Page 243 Engine start lever (second engine) ..........CUTOFF Verify SPAR VALVE CLOSED light transitions from extinguished, to bright and then dim. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 244 [Fuel CONFIG indication may be displayed with fuel in the center tank.] Crossfeed selector ..............Open Fuel pump switches (low tank) ..........OFF Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 31, 2016 SP.12.2 D6-27370-866-EGP...
  • Page 245 Fuel pump switches (low tank) ..........OFF When quantities are balanced: Fuel pump switches ............ON Crossfeed selector ............Close Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 31, 2016 D6-27370-866-EGP SP.12.3...
  • Page 246 Fueling hose nozzle ....Attached to the refueling receptacle Fueling valves ......Open for the tanks to be refueled Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 31, 2016 SP.12.4...
  • Page 247 When the required amount of fuel has been transferred: Center tank fueling valve switch ........CLOSED Manual defueling valve ..............Close Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 31, 2016 D6-27370-866-EGP...
  • Page 248 Verify crossfeed VALVE OPEN light illuminates bright and then dim. Crossfeed selector ................Close Verify crossfeed VALVE OPEN light illuminates bright and then extinguishes. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 31, 2016 SP.12.6 D6-27370-866-EGP...
  • Page 249 • terrain display test pattern shows on navigation displays • “CAUTION TERRAIN” aural sounds and TERRAIN caution message shows on navigation displays Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 250 60 seconds or more, the RUNWAY INOP light will illuminate. If RAAS is needed at the destination: RUNWAY INHIBIT switch ..........NORM Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.15.2 D6-27370-866-EGP...
  • Page 251 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 25, 2014 D6-27370-866-EGP SP.16.1...
  • Page 252 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 25, 2010 SP.16.2...
  • Page 253 Do the following step after completing the normal Preflight Procedure - First Officer: PROBE HEAT switches ............ON Verify that all probe heat lights are extinguished. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.16.3...
  • Page 254 Verify that the COWL VALVE OPEN lights illuminate bright, then dim. Verify that the COWL ANTI-ICE lights are extinguished. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.16.4...
  • Page 255 Verify that the L and R VALVE OPEN lights illuminate bright, then extinguish. Before Taxi Procedure Do the normal Before Taxi Procedure with the following modifications: Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.16.5...
  • Page 256 Taxiing on slippery taxiways or runways at excessive speed or with high crosswinds may start a skid. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.16.6...
  • Page 257 Ingestion of snow, slush, ice, or de-icing/anti-icing fluid can also cause damage to the APU. If de-icing/anti-icing is needed: APU ............As needed Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP SP.16.7...
  • Page 258 BLEED air switches on to ensure all de-icing fluid has been cleared from the engines: Engine BLEED air switches ......ON Flight controls ........ Check, as needed Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 SP.16.8 D6-27370-866-EGP...
  • Page 259 CAUTION: Do not use engine anti-ice when TAT is above 10°C When engine anti-ice is needed: ENGINE START switches ......CONT Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 260 Adjust thrust to 45% N1. After approximately five seconds, increase thrust lever slowly to a minimum of 80% N1. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.16.10...
  • Page 261 WING ANTI-ICE switch ........ON Verify that the L and R VALVE OPEN lights illuminate bright, then dim. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 262 • do not correct altimeter barometric reference settings. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.16.12...
  • Page 263 -30° 15 20 115 170 -40° 15 25 110 145 220 -50° 20 30 135 180 270 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP SP.16.13...
  • Page 264 Engine anti-ice must be selected ON and remain on during all ground operations when icing conditions exist or are anticipated. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.16.14...
  • Page 265 70% N1 for approximately 1 second duration at intervals no greater than 10 minutes should be considered. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 266 Note: The airplane must be parked into the wind when the outflow valve is full open. APU BLEED air switch ........ON Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.16.16...
  • Page 267 • Open all passenger cabin gasper outlets and close all window shades on the sun–exposed side of the passenger cabin. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP SP.16.17...
  • Page 268 APU BLEED air switch ............OFF Engine BLEED 1 air switch ............. ON ISOLATION VALVE switch..........AUTO Temperature selectors ........... As needed Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.16.18 D6-27370-866-EGP...
  • Page 269 Using a slower speed improves engine tolerance to heavy precipitation intake. Consider starting the APU (if available). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP SP.16.19...
  • Page 270 Verify that the cabin pressure outflow valve and both positive pressure relief valves are free of sand and dust. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.16.20...
  • Page 271 APU BLEED air switch ........ON Engine Start Procedure Do the normal Engine Start Procedure with the following modifications: Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 272 • In the event of a crosswind during 180° turns, turn away from the wind if possible to minimize sand and dust ingestion. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.16.22...
  • Page 273 Reverse thrust is most effective at high speed. After Landing Procedure Do the normal After Landing Procedure with the following modifications: Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP SP.16.23...
  • Page 274 Outflow VALVE switch ...........CLOSE Position the outflow valve fully closed to inhibit the intake of sand or dust. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.16.24...
  • Page 275 Set thrust as needed for the phase of flight. Change thrust setting only if needed to modify an unacceptable speed trend. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP SP.16.25...
  • Page 276 The airplane can withstand higher gust loads in the clean configuration. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.16.26...
  • Page 277 • Be alert for any airspeed fluctuations during takeoff and initial climb. Such fluctuations may be the first indication of windshear Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP SP.16.27...
  • Page 278 Recovery Accomplish the Windshear Escape Maneuver found in the Non–Normal Maneuvers section of the QRH. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.16.28 D6-27370-866-EGP...
  • Page 279 • Smell of ozone or sulfur • Humidity increase • Static discharge around the windshield (St. Elmo’s fire) Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 280 Exit the ice crystal icing conditions. Request a route change to minimize the time above red and amber radar returns. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.16.30...
  • Page 281 Supplementary Procedures - Adverse Weather 737 Flight Crew Operations Manual Do the Ice Crystal Icing non-normal checklist. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP SP.16.31...
  • Page 282 Supplementary Procedures - Adverse Weather 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 SP.16.32 D6-27370-866-EGP...
  • Page 283 Model 737-800W.1) - - - - - - - - - - - - - - - - - - - - - - - PD.10.1 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 284 Performance Dispatch - Table of Contents 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. PD.0.2 D6-27370-866-EGP September 15, 2016...
  • Page 285 Takeoff Climb Limit Weight......PD.13.1 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 286 Gear Down ........PD.14.5 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 287 35560 YK984 SU-GCS 35563 YK985 SU-GCZ 35568 YK986 SU-GCR 35562 YK987 SU-GDA 35565 YK988 SU-GDB 35567 YK989 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.ModID.10.1...
  • Page 288 40759 YK995 SU-GEA 40760 YK996 SU-GEB 40800 YK997 SU-GEC 40801 YK998 SU-GED 40802 YK999 SU-GEE 40803 YQ456 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. PD.ModID.10.2 D6-27370-866-EGP September 15, 2016...
  • Page 289 3930 4220 4510 4800 4970 5140 5320 5500 5000 4100 4400 4700 5000 5170 5350 5540 5730 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.10.1...
  • Page 290 With engine and wing anti-ice on (optional system), decrease field limit weight by 950 kg and climb limit weight by 1500 kg. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.10.2...
  • Page 291 With engine and wing anti-ice on (optional system), decrease field limit weight by 950 kg and climb limit weight by 1500 kg. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.10.3...
  • Page 292 With engine and wing anti-ice on (optional system), decrease field limit weight by 950 kg and climb limit weight by 1500 kg. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.10.4...
  • Page 293 3920 4210 4510 4800 5000 5210 5420 5640 5000 4090 4390 4700 5000 5210 5420 5650 5870 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.10.5...
  • Page 294 With engine and wing anti-ice on (optional system), decrease field limit weight by 850 kg and climb limit weight by 1500 kg. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.10.6...
  • Page 295 With engine and wing anti-ice on (optional system), decrease field limit weight by 850 kg and climb limit weight by 1500 kg. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.10.7...
  • Page 296 With engine and wing anti-ice on (optional system), decrease field limit weight by 850 kg and climb limit weight by 1500 kg. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.10.8...
  • Page 297 -18.6 -21.3 -23.9 9000 -11.7 -14.6 -17.6 -20.6 -23.5 -26.5 10000 -12.8 -16.0 -19.3 -22.5 -25.8 -29.0 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.10.9...
  • Page 298 With engine anti-ice on, decrease weight by 300 kg. With engine and wing anti-ice on, decrease weight by 1750 kg (optional system). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.10.10...
  • Page 299 Decrease brake release weight by 550 kg for each knot V1 exceeds VMBE. Determine normal V1, VR, V2 speeds for lower brake release weight. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.10.11...
  • Page 300 Performance Dispatch 737-800WSFP1/CFM56-7B26 Takeoff Category C/N Brakes 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.10.12 D6-27370-866-EGP...
  • Page 301 41000 41000 41000 41000 *Denotes altitude thrust limited in level flight, 100 fpm residual rate of climb. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.11.1...
  • Page 302 4800 4594 4403 4226 4064 3915 6747 6314 5923 5581 5277 5000 4786 4587 4403 4233 4079 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.11.2 D6-27370-866-EGP...
  • Page 303 -2.6 -1.3 14.8 -2.8 -1.4 10.1 16.4 Based on 280/.78 climb, Long Range Cruise and .78/280/250 descent. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.11.3...
  • Page 304 Based on 280/.78 climb, Long Range Cruise and .78/280/250 descent. Valid for all pressure altitudes with 4000 ft step climb to 2000 ft above optimum altitude. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.11.4...
  • Page 305 41000 41000 41000 41000 39000 37000 35000 Based on 280/.78 climb, Long Range Cruise and .78/280/250 descent. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.11.5...
  • Page 306 1450 1410 1400 1370 1420 This table includes 5% additional fuel for holding in a racetrack pattern. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.11.6 D6-27370-866-EGP...
  • Page 307 Required Pressure (PSI) for 114/115 Cubic Ft. Cylinder BOTTLE NUMBER OF CREW USING OXYGEN TEMPERATURE °C °F Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.11.7...
  • Page 308 -1.8 -1.6 -1.5 -1.4 -1.3 -1.2 ENGINE & WING -7.8 -7.3 -6.8 -6.8 -6.6 -6.0 -5.4 -5.0 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.11.8 D6-27370-866-EGP...
  • Page 309 83.4 80.0 2600 84.0 2800 86.4 Decrease field limit weight by 5000 kg when using manual speedbrakes. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.12.1...
  • Page 310 67.2 4200 86.7 81.3 76.3 71.2 4400 85.9 80.5 75.3 4600 84.8 79.2 4800 83.2 5000 87.1 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.12.2 D6-27370-866-EGP...
  • Page 311 84.2 81.0 3000 84.1 3200 86.1 Decrease field limit weight by 5000 kg when using manual speedbrakes. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.12.3...
  • Page 312 80.7 75.7 70.7 5000 84.7 79.4 74.2 5200 83.1 77.7 5400 86.8 81.1 5600 84.5 5800 87.9 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.12.4 D6-27370-866-EGP...
  • Page 313 When operating in icing conditions during any part of the flight with forecast landing temperature below 10 °C, decrease weight by 6850 kg. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.12.5...
  • Page 314 When operating in icing conditions during any part of the flight with forecast landing temperatures below 10°C decrease gradient by 1.0%. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.12.6...
  • Page 315 Note: If any brake temperature display digit is blank or indicates 0.0 or 0.1, then this method cannot be used. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.12.7...
  • Page 316 Note: If any brake temperature display digit is blank or indicates 0.0 or 0.1, then this method cannot be used. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.12.8...
  • Page 317 With engine anti-ice on, decrease weight by 1100 kg. With engine and wing anti-ice on, decrease weight by 5700 kg (optional system). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.13.1...
  • Page 318 When operating in icing conditions during any part of the flight with forecast landing temperature below 10°C, decrease weight by 7000 kg. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.13.2...
  • Page 319 -9.6 -5.0 -5.8 -6.6 -7.5 -8.3 -9.1 -9.9 -10.7 -5.6 -6.5 -7.4 -8.3 -9.2 -10.1 -11.0 -11.9 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.13.3...
  • Page 320 With engine anti-ice on, decrease weight by 2050 kg. With engine and wing anti-ice on, decrease weight by 7700 kg (optional system). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.13.4...
  • Page 321 24400 21800 28600 27100 25300 30800 29600 28100 32900 31900 30700 35100 34100 33000 37500 36500 35400 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.13.5...
  • Page 322 25.4 7:16 23.7 6:55 21.3 6:25 20.0 6:06 2000 26.9 7:37 25.1 7:16 22.5 6:44 21.1 6:24 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.13.6 D6-27370-866-EGP...
  • Page 323 -1.2 -2.6 -1.3 Based on VREF40 + 70 climb, Long Range Cruise and VREF40 + 70 descent. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.13.7...
  • Page 324 2260 2200 2160 2190 2220 This table includes 5% additional fuel for holding in a racetrack pattern. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.13.8 D6-27370-866-EGP...
  • Page 325 PRESSURE ALTITUDE (1000 FT) CONFIGURATION ENGINE ONLY -1.7 -1.3 -1.5 -1.5 -1.3 ENGINE AND WING -6.6 -5.9 -5.6 -5.1 -4.9 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.13.9...
  • Page 326 Performance Dispatch 737-800WSFP1/CFM56-7B26 Gear Down Category C/N Brakes 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.13.10 D6-27370-866-EGP...
  • Page 327 When finding a maximum weight for a wet runway, the dry runway limit weight must also be determined and the lower of the two weights used. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 328 The altitudes shown in the table are limited to the maximum certified altitude of 41000 ft. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.14.2...
  • Page 329 As noted, the fuel flow is based on flight in a racetrack holding pattern. For holding in straight and level flight, reduce table values by 5%. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 330 Now enter the Field Limit Weight table with wind corrected field length and pressure altitude to read field limit weight. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.14.4...
  • Page 331 Except for VNAV, normal autopilot and autothrottle modes will remain available for use during the flight, as will the LNAV mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PD.14.5...
  • Page 332 Takeoff/Landing Climb Limit Weight with gear down. Correct the weight obtained for engine bleed configuration as required. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PD.14.6...
  • Page 333 Model 737-800W.1) - - - - - - - - - - - - - - - - - - - - - - - - PI.10.1 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 334 Performance Inflight - Table of Contents 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. PI.TOC.2 D6-27370-866-EGP September 15, 2016...
  • Page 335 Slippery Runway Takeoff (22K Derate) ....PI.10.38 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 336 MANUAL REVERSION (Flaps 15) ....PI.12.18 One Engine Inoperative Landing (Flaps 15) ..PI.12.19 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. PI.TOC.10.2...
  • Page 337 Driftdown Speed/Level Off Altitude ....PI.16.1 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 338 Gear Down ........PI.17.14 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 339 35560 YK984 SU-GCS 35563 YK985 SU-GCZ 35568 YK986 SU-GCR 35562 YK987 SU-GDA 35565 YK988 SU-GDB 35567 YK989 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.ModID.10.1...
  • Page 340 40759 YK995 SU-GEA 40760 YK996 SU-GEB 40800 YK997 SU-GEC 40801 YK998 SU-GED 40802 YK999 SU-GEE 40803 YQ456 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. PI.ModID.10.2 D6-27370-866-EGP September 15, 2016...
  • Page 341 *V1 not to exceed VR. V1(MCG) Max Takeoff Thrust TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.1...
  • Page 342 *V1 not to exceed VR. V1(MCG) Max Takeoff Thrust TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.2 D6-27370-866-EGP...
  • Page 343 STOPWAY (M) -100 -200 -300 Use of clearway not allowed on wet runways. V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.3...
  • Page 344 4 3/4 4 1/2 3 3/4 2 3/4 2 3/4 2 3/4 2 3/4 2 3/4 2 3/4 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.4 D6-27370-866-EGP...
  • Page 345 Performance Inflight General Category C/N Brakes 737 Flight Crew Operations Manual VREF file Highlight FLAPS WEIGHT (1000 KG) Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.5...
  • Page 346 VREF40 + 50 VREF40 + 30 VREF40 + 30 VREF40 + 20 VREF40 + 10 VREF30 VREF40 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.6 D6-27370-866-EGP...
  • Page 347 V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.7...
  • Page 348 V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.8...
  • Page 349 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slippery runway limited weight is lesser of weights from 1 and 3. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.9...
  • Page 350 V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG).V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.10...
  • Page 351 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slippery runway limited weight is lesser of weights from 1 and 3. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.11...
  • Page 352 V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.12...
  • Page 353 AIRPORT PRESSURE ALTITUDE (FT) BLEED CONFIGURATION -2000 -1000 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 PACKS OFF Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.13...
  • Page 354 100.5 101.0 101.5 MINIMUM ASSUMED TEMP (°C) With engine bleed for packs off, increase %N1 by 1.0. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.14 D6-27370-866-EGP...
  • Page 355 3. Use the difference between assumed temperature and OAT to determine the %N1 adjustment from Table 3. 4. Subtract %N1 adjustment from Maximum %N1 in Table 2. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 356 *V1 not to exceed VR. V1(MCG) TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.16 D6-27370-866-EGP...
  • Page 357 *V1 not to exceed VR. V1(MCG) TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.17...
  • Page 358 STOPWAY (M) -100 -200 -300 Use of clearway not allowed on wet runways. V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.18 D6-27370-866-EGP...
  • Page 359 2 3/4 5 3/4 5 1/4 4 1/4 2 3/4 2 3/4 2 3/4 2 3/4 2 3/4 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.19...
  • Page 360 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slush/standing water limited weight is lesser of weights from 1 and 3. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.20...
  • Page 361 V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.21...
  • Page 362 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slush/standing water limited weight is lesser of weights from 1 and 3. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.22...
  • Page 363 V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.23...
  • Page 364 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slippery runway limited weight is lesser of weights from 1 and 3. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.24...
  • Page 365 V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.25...
  • Page 366 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slippery runway limited weight is lesser of weights from 1 and 3. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.26...
  • Page 367 V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.27...
  • Page 368 AIRPORT PRESSURE ALTITUDE (FT) BLEED CONFIGURATION -2000 -1000 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 PACKS OFF Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.28 D6-27370-866-EGP...
  • Page 369 98.2 99.1 100.0 MINIMUM ASSUMED TEMP (°C) With engine bleed for packs off, increase %N1 by 1.0 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.29...
  • Page 370 3. Use the difference between assumed temperature and OAT to determine the %N1 adjustment from Table 3. 4. Subtract %N1 adjustment from Maximum %N1 in Table 2. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.30...
  • Page 371 *V1 not to exceed VR. V1(MCG) TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.31...
  • Page 372 *V1 not to exceed VR. V1(MCG) TEMP PRESSURE ALTITUDE (FT) °C °F -2000 2000 4000 6000 8000 10000 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.32 D6-27370-866-EGP...
  • Page 373 STOPWAY (M) -100 -200 -300 Use of clearway not allowed on wet runways. V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.33...
  • Page 374 5 1/2 5 1/4 4 1/2 3 1/4 2 3/4 2 3/4 2 3/4 2 3/4 2 3/4 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.34 D6-27370-866-EGP...
  • Page 375 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slush/standing water limited weight is lesser of weights from 1 and 3. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.35...
  • Page 376 V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.36...
  • Page 377 V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.37...
  • Page 378 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slippery runway limited weight is lesser of weights from 1 and 3. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.38...
  • Page 379 V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.39...
  • Page 380 3. Find V1(MCG) limit weight for adjusted field length and pressure altitude. 4. Max allowable slippery runway limited weight is lesser of weights from 1 and 3. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.40...
  • Page 381 V1 speed adjustment. If adjusted V1 is less than V1(MCG), set V1 = V1(MCG). V1 not to exceed VR. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.41...
  • Page 382 AIRPORT PRESSURE ALTITUDE (FT) BLEED CONFIGURATION -2000 -1000 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 PACKS OFF Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.42 D6-27370-866-EGP...
  • Page 383 95.7 96.4 97.1 MINIMUM ASSUMED TEMP (°C) With engine bleed for packs off, increase %N1 by 0.9. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.43...
  • Page 384 3. Use the difference between assumed temperature and OAT to determine the %N1 adjustment from Table 3. 4. Subtract %N1 adjustment from Maximum %N1 in Table 2. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.44...
  • Page 385 -0.9 -0.9 -0.8 -0.8 ENGINE & WING ANTI-ICE* -1.8 -2.1 -2.5 -2.7 -3.0 -3.0 *Dual bleed sources Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.45...
  • Page 386 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 PACKS OFF A/C HIGH -0.1 -0.1 -0.1 -0.1 -0.1 -0.1 -0.1 -0.1 -0.1 -0.1 -0.1 -0.1 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.46 D6-27370-866-EGP...
  • Page 387 -1800 -1700 -1500 PITCH ATT -3.5 -2.5 -1.0 SEA LEVEL V/S (FT/MIN) -2300 -1900 -1700 -1500 -1400 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.10.47...
  • Page 388 PITCH ATT 28.0 22.0 18.0 16.0 14.0 SEA LEVEL V/S (FT/MIN) 5200 4200 3500 2900 2500 KIAS Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.10.48 D6-27370-866-EGP...
  • Page 389 41000 41000 41000 41000 *Denotes altitude thrust limited in level flight, 100 fpm residual rate of climb. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.11.1...
  • Page 390 MACH .538 .561 .584 .602 .619 .637 .665 .699 .732 KIAS FF/ENG Shaded area approximates optimum altitude. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.11.2 D6-27370-866-EGP...
  • Page 391 6:11 11.5 5:34 10.4 5:17 5:05 2000 14.6 6:59 13.6 6:31 12.1 5:53 11.0 5:34 10.2 5:22 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.11.3...
  • Page 392 -0.4 -1.0 -0.5 -1.1 -0.6 -1.2 -0.6 -1.3 -0.7 -1.5 -0.8 -1.6 -0.9 -1.7 -0.9 -1.8 -1.0 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.11.4 D6-27370-866-EGP...
  • Page 393 4800 4583 4381 4196 4026 3873 6892 6417 5990 5621 5295 5000 4773 4562 4368 4191 4031 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.11.5...
  • Page 394 -1.0 -2.4 -1.2 -2.7 -1.4 -3.0 -1.5 -3.4 -1.7 -3.8 -1.8 -4.1 -2.0 -4.5 -2.2 -4.9 -2.4 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.11.6 D6-27370-866-EGP...
  • Page 395 3. Break-even wind at new altitude is present altitude wind plus difference from step 2. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.11.7...
  • Page 396 27000 25000 23000 21000 19000 17000 15000 10000 5000 1500 Allowances for a straight-in approach are included. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.11.8 D6-27370-866-EGP...
  • Page 397 68.6 73.0 80.1 KIAS FF/ENG This table includes 5% additional fuel for holding in a racetrack pattern. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.11.9...
  • Page 398 Performance Inflight 737-800WSFP1/CFM56-7B26 All Engine Category C/N Brakes 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.11.10 D6-27370-866-EGP...
  • Page 399 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.1...
  • Page 400 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.2...
  • Page 401 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.3...
  • Page 402 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.4...
  • Page 403 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.5...
  • Page 404 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.6...
  • Page 405 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.7...
  • Page 406 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.8...
  • Page 407 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.9...
  • Page 408 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.10...
  • Page 409 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.11...
  • Page 410 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.12...
  • Page 411 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.13...
  • Page 412 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.14...
  • Page 413 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.15...
  • Page 414 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.16...
  • Page 415 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.17...
  • Page 416 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.18...
  • Page 417 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.19...
  • Page 418 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.20...
  • Page 419 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.21...
  • Page 420 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.22...
  • Page 421 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.23...
  • Page 422 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.24...
  • Page 423 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.25...
  • Page 424 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.26...
  • Page 425 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.27...
  • Page 426 8000 ft, first apply the STD adjustment to derive a new reference landing distance for 8000 ft then apply the HIGH adjustment to this new reference distance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.28...
  • Page 427 If ground speed is used for brakes on speed, ignore wind and enter table with sea level, 15°C. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.12.29...
  • Page 428 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.12.30...
  • Page 429 -0.8 -0.8 -0.8 -0.8 ENGINE & WING ANTI-ICE -4.2 -4.4 -4.5 -4.7 -5.0 -4.8 -4.8 -4.8 -4.8 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.13.1...
  • Page 430 ENGINE ANTI-ICE ON -0.9 -0.9 -0.8 -0.8 -0.8 ENGINE & WING ANTI-ICE ON -4.1 -4.3 -4.5 -4.7 -4.7 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.13.2 D6-27370-866-EGP...
  • Page 431 ENGINE ANTI-ICE ON -0.9 -0.9 -1.0 -1.0 -1.0 ENGINE & WING ANTI-ICE ON -3.6 -3.8 -3.8 -3.9 -4.0 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.13.3...
  • Page 432 CONFIGURATION ENGINE ANTI-ICE ON -0.9 -0.9 -0.9 -0.9 ENGINE & WING ANTI-ICE ON -3.2 -3.4 -3.4 -3.5 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.13.4 D6-27370-866-EGP...
  • Page 433 CONFIGURATION ENGINE ANTI-ICE ON -0.6 -0.8 -0.8 -0.8 ENGINE & WING ANTI-ICE ON -2.9 -3.0 -2.7 -3.2 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.13.5...
  • Page 434 24700 29100 28100 27000 31200 30400 29400 33300 32600 31700 35600 34900 34000 Includes APU fuel burn. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.13.6 D6-27370-866-EGP...
  • Page 435 4:57 Includes APU fuel burn. Driftdown at optimum driftdown speed and cruise at long range cruise speed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.13.7...
  • Page 436 With engine anti-ice on, decrease altitude capability by 1200 ft. With engine and wing anti-ice on, decrease altitude capability by 5500 ft. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.13.8...
  • Page 437 .502 .525 .548 .571 .589 KIAS FF/ENG 1485 1434 1416 1402 1392 1394 1400 1410 1421 1424 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.13.9...
  • Page 438 -0.4 -1.7 -1.3 -0.9 -0.4 -1.9 -1.4 -0.9 -0.5 -2.0 -1.5 -1.0 -0.5 Includes APU fuel burn. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.13.10 D6-27370-866-EGP...
  • Page 439 1270 1250 1240 1260 1360 This table includes 5% additional fuel for holding in a racetrack pattern. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.13.11...
  • Page 440 Decrease rate of climb 130 ft/min per 5000 kg greater than 60000 kg. Increase rate of climb 160 ft/min per 5000 kg less than 60000 kg. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.13.12...
  • Page 441 AIRPORT PRESSURE ALTITUDE (FT) BLEED CONFIGURATION -2000 -1000 1000 2000 3000 4000 5000 6000 7000 8000 9000 10000 PACKS OFF Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.14.1...
  • Page 442 Performance Inflight 737-800WSFP1/CFM56-7B26 Alternate Mode EEC Category C/N Brakes 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.14.2 D6-27370-866-EGP...
  • Page 443 24400 21800 28600 27100 25300 30800 29600 28100 32900 31900 30700 35100 34100 33000 37500 36500 35400 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.15.1...
  • Page 444 .452 .471 .491 .513 .535 .554 KIAS FF/ENG 1170 1098 1085 1083 1089 1092 1094 1096 1097 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.15.2 D6-27370-866-EGP...
  • Page 445 -0.5 -1.3 -0.7 -1.7 -0.8 -2.0 -1.0 -2.4 -1.2 -2.7 -1.3 -3.0 -1.5 -3.4 -1.7 -3.7 -1.8 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.15.3...
  • Page 446 27000 25000 23000 21000 19000 17000 15000 10000 5000 1500 Allowances for a straight-in approach are included. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.15.4 D6-27370-866-EGP...
  • Page 447 1130 1100 1080 1090 1110 This table includes 5% additional fuel for holding in a racetrack pattern. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.15.5...
  • Page 448 Performance Inflight 737-800WSFP1/CFM56-7B26 Gear Down Category C/N Brakes 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.15.6 D6-27370-866-EGP...
  • Page 449 5900 3400 10600 9200 6900 13300 12300 10600 16200 15400 14500 19300 18300 17500 22200 21400 20500 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.16.1...
  • Page 450 .361 .374 .387 .402 .418 KIAS FF/ENG 2206 2166 2133 2107 2088 2076 2069 2065 2101 2201 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.16.2 D6-27370-866-EGP...
  • Page 451 -0.7 -1.5 -0.7 -1.6 -0.8 -1.8 -0.9 -1.9 -1.0 -2.1 -1.1 -2.3 -1.1 Includes APU fuel burn. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.16.3...
  • Page 452 FF/ENG 2170 2140 2120 2130 This table includes 5% additional fuel for holding in a racetrack pattern. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.16.4 D6-27370-866-EGP...
  • Page 453 Slope and wind adjustments to V1 are obtained by entering the Slope and Wind V1 Adjustment table. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 454 Do not apply a wind correction for tailwinds. The maximum command speed should not exceed landing flap placard speed minus 5 knots. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.17.2...
  • Page 455 V1(MCG) speed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.17.3...
  • Page 456 1800 m. Detailed analysis for the specific case from the Airplane Flight Manual may yield a less restrictive penalty. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.17.4...
  • Page 457 Use of assumed temperature reduced thrust is not recommended if potential windshear conditions exist. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 458 Pitch attitude is shown in bold type for emphasis since altitude and/or vertical speed indications may also be unreliable. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.17.6...
  • Page 459 For example, a favorable wind component may have an effect on ground speed which more than compensates for the loss in air range. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.17.7...
  • Page 460 "good" data is consistent with wet runway testing done on early Boeing jets. The performance level used to calculate "poor" data reflects runways covered with wet ice. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.17.8...
  • Page 461 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 462 Enter the table with pressure altitude, TAT, and IAS or Mach to read %N1. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.17.10...
  • Page 463 Mach number, IAS and fuel flow for the airplane weight and pressure altitude. The fuel flow values in this table reflect single engine fuel burn. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.17.11...
  • Page 464 The data includes engine bleed effects for normal air conditioning operation i.e., two packs on at normal flow all engines operating. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.17.12...
  • Page 465 %N1. For packs off apply the %N1 adjustment provided below the table. No %N1 adjustment is required for engine or wing anti-ice. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP PI.17.13...
  • Page 466 Tables for gear down performance in this section are identical in format and used in the same manner as tables for the gear up configuration previously described. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 PI.17.14...
  • Page 467 Map and Chart Light Controls ......1.30.1 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 468 Flight Deck Lighting ....... . . 1.40.4 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 469 Pilot Seat ......... . . 1.40.48 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 470 Servicing ......... 1.40.51 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 471 47'-2" (14.30m) 18'-8" (5.70m) 41'-2" (12.50m) 21'-1" (6.42m) 51'-1" (15.60m) 124'-9" (38.00m) 129'-6" (39.50m) 737-800 With Winglets Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 15, 2007 D6-27370-866-EGP 1.10.1...
  • Page 472 CAUTION: Do not attempt to make a turn away from an obstacle within (17.8 feet/5.4m) of the wing tip or within (24.3feet/7.4m)of the nose. 737-800 With Winglets Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.10.2...
  • Page 473 Refer to the appropriate chapter system descriptions for current information. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 1.20.1...
  • Page 474 WINDOW HEAT MANUAL GEAR RELEASE P6-4 AIR COND P6-11 WINDOW HEAT & ELECTRICAL AFT FLIGHT DECK OVERVIEW Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 1.20.2 D6-27370-866-EGP...
  • Page 475 SHIELD OUTBD INBD LOWER CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 D6-27370-866-EGP 1.20.3...
  • Page 476 NORM NORM NORM NORM CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 18, 2011 1.20.4 D6-27370-866-EGP...
  • Page 477 ADF 2 ARPT DATA TERR CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 1.20.5...
  • Page 478 230K ALT FLAP EXTEND CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 27, 2012 1.20.6 D6-27370-866-EGP...
  • Page 479 PAGE PAGE PAGE PAGE CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 1.20.7...
  • Page 480 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 1.20.8 D6-27370-866-EGP...
  • Page 481 AUTO RETRACTABLE FIXED START CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 1.20.9...
  • Page 482 SPSEU PSEU GEAR BRIGHT CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 1.20.10 D6-27370-866-EGP...
  • Page 483 CAPT PASS CENTER ADDRESS CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 1.20.11...
  • Page 484 CAPT PASS CENTER ADDRESS CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.20.12 D6-27370-866-EGP...
  • Page 485 WING WING DOWN DOWN CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.20.13...
  • Page 486 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.20.14 D6-27370-866-EGP...
  • Page 487 BOOM MIKE HEAD PHONE CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.20.15...
  • Page 488 TEST SHUTOFF EXIT LIGHTING CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.20.16 D6-27370-866-EGP...
  • Page 489 Touch screen controls various functions such as Lighting, Passenger Services, Environment, Maintenance and Special Functions. A typical Lighting menu is depicted. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 490 Touch screen controls various functions such as Lighting, Passenger Services, Environment, Maintenance and Special Functions. A typical Lighting menu is depicted. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.20.18...
  • Page 491 PUSH TO TALK RESET CIRCLED NUMBERS REFER TO CHAPTERS WHERE INFORMATION ON THE ITEM MAY BE FOUND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.20.19...
  • Page 492 Airplane General, Emergency Equipment, Doors, Windows - Instrument Panels 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.20.20 D6-27370-866-EGP...
  • Page 493 Rotate – adjusts brightness of Captain/First Officer chart lights Main Panel Lighting MAIN PANEL LEFT/RIGHT FORWARD PANELS Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 1.30.1...
  • Page 494 Rotate – controls brightness of lighting directed at AFDS panel. Flood and Aft Electronics Lights Controls FLOOD PANEL AISLE STAND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 1.30.2 D6-27370-866-EGP...
  • Page 495 Rotate – controls P–6 and P–18 circuit breaker panels light brightness. PANEL Light Control Rotate – controls forward and aft overhead panel lights brightness. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP...
  • Page 496 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 1.30.4...
  • Page 497 OFF – nose wheel well taxi light extinguished. AUTO – nose landing gear taxi light automatically extinguishes when the nose landing gear retracts. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 498 AUTO – LED wing strakelet taxi lights are illuminated when the nose landing gear is fully extended and are extinguished when the nose landing gear retracts. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.30.6...
  • Page 499 OFF – red strobe/rotating beacon lights on upper and lower fuselage extinguished. ON – red strobe/rotating beacon lights illuminated. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.30.7...
  • Page 500 INOP. YK993 - YW274 NO SMOKING Switch The No Smoking signs are deactivated and placarded INOP. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.30.8 D6-27370-866-EGP...
  • Page 501 Emergency Locator Transmitter Light Illuminated (amber) – ELT has been activated and is simultaneously transmitting on 121.5, 243.0 and 406.0 MHz. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 502 YK981 - YQ456 Activation Switch OFF - (guarded position) deactivates flight attendant’s EMER EVAC switch to initiate evacuation signals. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.30.10 D6-27370-866-EGP...
  • Page 503 PUSH - silences the horn at that panel only. Horn Sounds when any activation switch is moved to ON. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 504 Decompression Panel Provides emergency egress path and automatically opens during airplane decompression. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.30.12 D6-27370-866-EGP...
  • Page 505 Illuminated (red) - door locked or Flight Deck Access System switch OFF. Illuminated (amber) - correct emergency access code entered. Illuminated (green) - door unlocked. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 506 Illuminated (amber) - correct emergency access code entered in keypad. AUTO UNLK light flashes and continuous chime sounds before timer expires and door unlocks. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.30.14...
  • Page 507 R - provides a general view of the Door 1 Galley area. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 508 • related overwing exit is not closed and locked • related flight lock failed to engage when commanded locked. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.30.16...
  • Page 509 NORMAL – (guarded position) passenger masks drop and passenger oxygen system activated automatically if cabin altitude climbs to 14,000 feet Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.30.17...
  • Page 510 • with the left oxygen mask panel door closed and the OXY ON flag displayed will turn oxygen off and disable the mask microphone and enable the boom microphone. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.30.18...
  • Page 511 • enables the mask microphone when the left oxygen mask panel door is opened • disables the boom microphone. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 512 BELOW AFT ENTRY DOOR Water Quantity Indicator Indicates quantity of water in reservoir. Water System Service Panel Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.30.20 D6-27370-866-EGP...
  • Page 513 OPEN DO NOT OPEN DURING FLIGHT DRAIN VALVE OPERATION SELECTOR VALVE PLACARD TOILET ONLY LAVATORY SINK CABINET Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.30.21...
  • Page 514 OFF – No water is supplied to the lavatory. Drain Valve Handle (red) Located in the forward lavatory only. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.30.22...
  • Page 515 Two fixed landing lights are in the wing leading edge. The lights shine forward and down in a fixed position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.1...
  • Page 516 Wheel Well Lights Lights are installed in the wheel well of the nose gear and each main gear. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.2...
  • Page 517 POSITION LIGHTS (RED AND WHITE) (GREEN AND WHITE) LOGO LIGHT (WHITE) LOGO LIGHT (WHITE) STROBE LIGHT (WHITE) Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.3...
  • Page 518 YK981 - YQ456 The Emergency Evacuation System is powered by the 28V DC hot battery bus. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.4...
  • Page 519 The flight deck aft DOME light contains a separate bulb that is powered by the emergency lighting system to provide for flight deck evacuation. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.5...
  • Page 520 Passengers will shadow the system and are not allowed onboard during charging. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.6 D6-27370-866-EGP...
  • Page 521 Reduced charge time allowed because passengers are seated, meal service ended and little aisle traffic. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.7...
  • Page 522 No limit if lights stay on by having ceiling lights on dim. *Taxi Time can be used for charging credit. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.8 D6-27370-866-EGP...
  • Page 523 Passengers will shadow the system and are not allowed onboard during charging. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.9...
  • Page 524 Passengers will shadow the system and are not allowed onboard during charging. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.10 D6-27370-866-EGP...
  • Page 525 Reduced charge time allowed because passengers are seated, meal service ended and little aisle traffic. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.11...
  • Page 526 No limit if lights stay on by having ceiling lights on dim. *Taxi Time can be used for charging credit. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.12 D6-27370-866-EGP...
  • Page 527 Passengers will shadow the system and are not allowed onboard during charging. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.13...
  • Page 528 15 minute charge charging. b) Cabin activity is limited to minor aisle traffic or crew and personnel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.14 D6-27370-866-EGP...
  • Page 529 Flight duration can be extended continuously. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.15...
  • Page 530 15 minute charge 12.5 charging. b) Cabin activity is limited to minor aisle traffic or crew and personnel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.16 D6-27370-866-EGP...
  • Page 531 15 minute charge meal service by galley cart and flight attendants which are stationary for 5 minutes. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.17...
  • Page 532 Lights are also installed on the fuselage to illuminate the overwing escape routes and ground contact area. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.18...
  • Page 533 These cylinders are normally found in the forward and aft areas of the passenger cabin. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 534 UNITS (2 MASKS) (4 MASKS) CONDITION: NORMAL OXYGEN SOURCE HIGH PRESSURE (IN EACH SERVICE UNIT) LOW PRESSURE Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.20 D6-27370-866-EGP...
  • Page 535 • Release the inflation levers so the harness holds the mask in place. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.21...
  • Page 536 • Grasp the harness and pull it downward so the cross straps are below the facepiece. Allow the excess harness to hang downward. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.22...
  • Page 537 WARNING: Do not squeeze the red inflation levers during stowing. Doing this will inflate the harness and prevent the correct stowing of the mask. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 538 An oxygen source with two masks is located above each attendant station and in each lavatory. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.24...
  • Page 539 Once the oxygen source is activated, the flow of oxygen is constant, whether or not the mask is being worn. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 540 Duration can be determined by dividing capacity by outflow (120 liters divided by 4 liters/minute = 30 minutes). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.26...
  • Page 541 • aim at base of fire and press trigger. CAUTION: Do not use on electrical or grease type fires. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.27...
  • Page 542 The extinguisher is effective on all types of fires, but primarily on electrical, fuel and grease fires. Direction for use of the fire extinguisher is printed on the extinguisher. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.28...
  • Page 543 737 Flight Crew Operations Manual BCF Fire Extinguisher (Halon 1211) LEVER DISCHARGE RING SAFETY NOZZLE PRESSURE GAUGE HANDLE Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.29...
  • Page 544 WATER ON FLAMMABLE LIQUID FIRES SPREAD THE FIRE. WATER ON A LIVE ELECTRICAL FIRE COULD CAUSE SEVERE SHOCK OR DEATH. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.30...
  • Page 545 WARNING: If a fire extinguisher is to be discharged in the flight deck, then all crewmembers are to wear oxygen masks and use 100% oxygen with emergency selected. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 546 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.32 D6-27370-866-EGP...
  • Page 547 FIRST AID PORTABLE RESUSCITATOR MEDICAL KIT EXIT LIGHT NOTE: SOME SYMBOLS DO NOT APPLY TO ALL CONFIGURATIONS. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.33...
  • Page 548 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.34 D6-27370-866-EGP...
  • Page 549 L = LAVATORY G = GALLEY C = CLOSET (2) (2) INFANT (2)DEMO KIT AT EACH ATTENDANT SEAT Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.35...
  • Page 550 A = ATTENDANT SEAT L = LAVATORY G = GALLEY C = CLOSET INFANT (2)DEMO KITS AT EACH ATTENDANT SEAT Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.36 D6-27370-866-EGP...
  • Page 551 L = LAVATORY G = GALLEY C = CLOSET (10) SPARE INFANT (2)DEMO KITS AT EACH ATTENDANT SEAT Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.37...
  • Page 552 A = ATTENDANT SEAT L = LAVATORY G = GALLEY C = CLOSET (4) (2) (4) (2) AT EACH ATTENDANT Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.38 D6-27370-866-EGP...
  • Page 553 Illumination of the amber LOCK FAIL light indicates the door lock has failed or the Access System switch is in the OFF position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.39...
  • Page 554 Flight Deck Number Two Windows HANDLE WITH TRIGGER LATCH MECHANISM CLOTHES GUARD PROTECTOR FLIGHT COMPARTMENT WINDOW NO. 2 (RIGHT SIDE SHOWN) Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.40 D6-27370-866-EGP...
  • Page 555 • emergency evacuation routes • flight deck windows • escape slides • escape straps • emergency exit doors Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.41...
  • Page 556 • exit in accordance with the following illustration. CAUTION: Ensure the escape strap is securely fastened to the airplane. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.42...
  • Page 557 Hand grips are positioned along the sides of the slide. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.43...
  • Page 558 1. LIFT FLAP 2. PULL HANDLE DETACHMENT HANDLE PULL PULL FLOOR BRACKETS GIRT GIRT BAR MANUAL INFLATION HANDLE Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.44 D6-27370-866-EGP...
  • Page 559 ATTACHMENT FITTING OVERWING ESCAPE STRAP ESCAPE STRAP IN STOWED CONDITION STOWAGE TUBE HOOK RETAINER OVERWING ESCAPE STRAP Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.45...
  • Page 560 When the doors are latched and locked and the flight lock is operating properly none of these lights will illuminate. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.46...
  • Page 561 1. PULL INTERIOR HANDLE DOWN AND INWARD. 2. DOOR OPENS OUT AND UP AUTOMATICALLY. CLOSING STRAP PANEL SHOWN OPEN. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.47...
  • Page 562 PILOT SEAT - OUTBOARD SIDE LUMBAR ADJUSTMENT (IN/OUT) THIGH PAD ADJUSTMENT TRACK LOCK LEVER PILOT SEAT - INBOARD SIDE Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.48 D6-27370-866-EGP...
  • Page 563 Storage space, miscellaneous drawers and waste containers are also integrated in the galley units. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.49...
  • Page 564 The drain position of this valve is used to drain all water overboard. Normally, the drain shutoff valves are ON. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.50...
  • Page 565 The drain mast are on the bottom of the fuselage; one forward and one aft. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 1.40.51...
  • Page 566 Airplane General, Emergency Equipment, Doors, Windows - Systems Description 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 1.40.52 D6-27370-866-EGP...
  • Page 567 Zone Temperature Control Modes ..... . 2.31.4 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 568 Manual Mode Operation....... . . 2.40.6 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 569 PACK switches are AUTO or HIGH • opens isolation valve automatically if either engine BLEED air or air conditioning PACK switch positioned OFF. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 27, 2012 D6-27370-866-EGP...
  • Page 570 • related engine bleed air valve opens, or related pack valve opens, or related trim air modulating valve opens Lights remain illuminated until reset. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 28, 2013 2.10.2...
  • Page 571 FORWARD OVERHEAD PANEL Air Temperature (TEMP) Indicator Indicates temperature at location selected with AIR TEMP source selector. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 18, 2011 D6-27370-866-EGP 2.10.3...
  • Page 572 PASS CAB – selects forward or aft passenger cabin temperature PACK – selects left or right pack temperatures. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 2.10.4...
  • Page 573 • related engine bleed air valve opens, or related pack valve opens, or related trim air modulating valve opens Lights remain illuminated until reset. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 27, 2012 D6-27370-866-EGP...
  • Page 574 ALTN – alternate cooling exhaust fan activated. Equipment Cooling Exhaust OFF Light Illuminated (amber) – no airflow from selected cooling exhaust fan. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 2.10.6...
  • Page 575 • cuts out intermittent cabin altitude warning horn • altitude warning horn sounds when cabin exceeds 10,000 feet altitude. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 26, 2015 D6-27370-866-EGP 2.10.7...
  • Page 576 CAB ALT LAND ALT 2000 4000 6000 8000 <FL160 FL220 FL410 FLT ALT FL260 FL320 FORWARD OVERHEAD PANEL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 2.10.8 D6-27370-866-EGP...
  • Page 577 OFF Schedule (SCHED) DESCENT Light Illuminated (amber) – airplane descended before reaching the planned cruise altitude set in the FLT ALT indicator. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 578 • Illumination of both ALTN and AUTO FAIL lights indicates a single controller failure and automatic transfer to ALTN mode • pressurization mode selector in ALTN position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 2.10.10...
  • Page 579 Cabin /Flight Altitude (CAB ALT)(FLT ALT) Placard Used to determine setting for cabin altitude when operating in manual mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 2.10.11...
  • Page 580 Air Systems - Controls and Indicators 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 2.10.12 D6-27370-866-EGP...
  • Page 581 Bleed trip sensors illuminate the respective BLEED TRIP OFF light when engine bleed air temperature or pressure exceeds a predetermined limit. The respective engine bleed air valve closes automatically. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP...
  • Page 582 APU. Therefore, thrust must be limited to idle with the DUAL BLEED light illuminated. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. May 15, 2008 2.20.2...
  • Page 583 AIR VALVE TRIP SENSORS A P U CONDITION: ENGINES OPERATING & SUPPLYING AIR BLEED AIR CONDITIONING PACKS Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 2.20.3...
  • Page 584 LEADING EDGE. LEADING EDGE. LEFT-HAND AIR RIGHT-HAND AIR CONDITIONING BAY. CONDITIONING BAY. KEEL BEAM. BLEED DUCT FROM APU. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2007 2.20.4 D6-27370-866-EGP...
  • Page 585 HIGH. This mode is designed to provide the maximum airflow when the APU is the only source of bleed air. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 25, 2010 D6-27370-866-EGP 2.31.1...
  • Page 586 The pack will continue to operate without control unless excessive temperatures cause the pack to trip off. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 2.31.2...
  • Page 587 ANTI WING-BODY OVERHEAT PACK VALVE CONDITIONED AIR COLD AIR RIGHT HEAT EXCHANGER BLEED COOLED AIR BLEED AIR Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 2.31.3...
  • Page 588 If any individual zone is switched OFF, the Temperature Selector setting will be ignored by the temperature control system. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 2.31.4...
  • Page 589 It extends from the forward to the aft end of the ceiling along the airplane centerline and also supplies the sidewall diffusers. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 2.31.5...
  • Page 590 A ground air conditioning source may be connected to the mix manifold to distribute preconditioned air throughout the airplane. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 2.31.6...
  • Page 591 LEFT RIGHT PACK PACK SHUTOFF VALVE GROUND PRECONDITIONED CONDITIONED AIR CONDITION: IN FLIGHT PACKS ON BLEED AIR Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 2.31.7...
  • Page 592 Air Systems - Air Conditioning System Description 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 2.31.8 D6-27370-866-EGP...
  • Page 593 The automatic controllers also receive throttle position from both stall management computers and signals from the air/ground sensors. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP...
  • Page 594 A small amount is also exhausted through toilet and galley vents, miscellaneous fixed vents, and by seal leakage. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 2.40.2...
  • Page 595 COMPARTMENT LINING ALTN LAND ALT AUTO OUTFLOW EXHAUST PORT FOR VALVE OVERBOARD EXHAUST VALVE AFT LOOKING FORWARD Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 31, 2016 D6-27370-866-EGP 2.40.3...
  • Page 596 Deviations from flight altitude can cause the pressure differential to vary as the controller modulates the outflow valve to maintain a constant cabin altitude. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 2.40.4...
  • Page 597 Moving the pressurization mode selector to the ALTN position extinguishes the AUTO FAIL light, however the ALTN light remains illuminated to indicate single channel operation. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 D6-27370-866-EGP...
  • Page 598 DC standby system, drives the outflow valve at a slower rate than the automatic modes. Outflow valve full range of motion takes up to 20 seconds. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 28, 2013 2.40.6...
  • Page 599 Wing Anti–Ice System Schematic ..... . 3.20.8 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 600 Anti-Ice, Rain - Table of Contents 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 3.TOC.2 D6-27370-866-EGP September 15, 2016...
  • Page 601 OFF – window heat not in use. WINDOW HEAT Test Switch (spring–loaded to neutral) OVHT – simulates an overheat condition. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP...
  • Page 602 PARK – turns off wiper motors and stows wiper blades. INT – seven second intermittent operation. LOW – low speed operation. HIGH – high speed operation. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 3.10.2 D6-27370-866-EGP...
  • Page 603 OFF – power off. YK994 - YW274 PROBE HEAT Switches ON – power is supplied to heat related system. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 3.10.3...
  • Page 604 • related engine anti–ice valve is closed • stick shaker logic returns to normal if wing anti–ice has not been used in flight. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 31, 2016 3.10.4...
  • Page 605 • dim – related wing anti–ice control valve is open (switch ON). Extinguished – related wing anti–ice control valve is closed (switch OFF). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 31, 2016 D6-27370-866-EGP 3.10.5...
  • Page 606 Switch remains ON • switch trips OFF at lift–off. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 31, 2016 3.10.6...
  • Page 607 Flight Deck Window Heat Flight deck windows consist of glass panes laminated to each side of a vinyl core. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 25, 2014 D6-27370-866-EGP 3.20.1...
  • Page 608 Thermal switches, located on window number 3, open and close to maintain the correct temperature of window 3. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 3.20.2...
  • Page 609 THERMAL SWITCH FROM WIND WIND AIR CONDITIONING SHIELD SHIELD SYSTEM CONDITION: WINDOW HEAT ON R SIDE OVERHEATED Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 3.20.3...
  • Page 610 CAUTION: Windshield scratching will occur if the windshield wipers are operated on a dry windshield. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 3.20.4...
  • Page 611 The amber COWL ANTI–ICE light illuminates due to excessive pressure in the duct leading from the cowl anti–ice valve to the cowl lip. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 3.20.5...
  • Page 612 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 3.20.6...
  • Page 613 Duct temperature and thrust setting logic are disabled and have no affect on control valve operation in flight. Valve position is monitored by the blue VALVE OPEN lights. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 614 SLATS CONDITION: ON THE GROUND WING ANTI-ICE ON ENGINES AT IDLE THRUST BLEED AIR DUCT TEMPS LOW Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 3.20.8 D6-27370-866-EGP...
  • Page 615 Automatic Flight Approach and Landing ....4.20.14 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 616 Reversion Modes........4.20.25 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 617 • G/S capture • TO/GA. The indicator light illuminates green when A/T ARM switch is in the ARM position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP 4.10.1...
  • Page 618 Push – (light illuminated) • deselects N1 mode and extinguishes switch light • engages autothrottles in ARM mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 4.10.2...
  • Page 619 • selected speed is reference speed for AFDS and A/T • not operative when IAS/MACH display is blank. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 28, 2013 D6-27370-866-EGP...
  • Page 620 • both flight director switches have been switched on. • VNAV guidance becomes active at 400 feet AGL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 27, 2012 4.10.4...
  • Page 621 LNAV not engaged In the event of glideslope intercept waypoint transition, VNAV can be re-engaged. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 27, 2012 D6-27370-866-EGP 4.10.5...
  • Page 622 The LVL CHG mode coordinates pitch and thrust commands to make automatic climbs and descents to preselected altitudes at selected airspeeds. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 4.10.6...
  • Page 623 ALT HOLD mode commands pitch to hold either: • MCP selected altitude • pitch mode annunciates ALT HOLD • ALT HLD switch light extinguishes. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 4.10.7...
  • Page 624 • new MCP altitude is selected (more than 100 feet from current altitude). With V/S armed, V/S mode is engaged by moving vertical speed thumbwheel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 4.10.8...
  • Page 625 • if all FMC altitude constraints are deleted during VNAV path descent, an automatic transition to a VNAV speed descent is made. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 4.10.9...
  • Page 626 Active route is entered and modified through FMC CDUs and can include SIDs, STARs, and instrument approaches. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 4.10.10...
  • Page 627 The VOR mode provides roll commands to track selected VOR course. The LOC mode provides roll commands to track selected localizer course along inbound front course bearing. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 628 Note: In VOR LOC or APP mode, B A/P and First Officer’s F/D use selected course and navigation data from No. 2 VHF NAV receiver. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.10.12...
  • Page 629 For dual autopilot operation, both VHF NAV receivers must be tuned to the ILS frequency and both autopilots must be selected in CMD prior to 800 feet RA. APP mode operation: Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 630 Note: During a dual autopilot approach and after FLARE ARM annunciation, any attempted manual override of the autopilots may result in an autopilot disconnect. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.10.14...
  • Page 631 • when approaching a selected altitude in CWS P, the pitch mode engages in ALT ACQ and ALT HOLD when reaching selected altitude Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 4.10.15...
  • Page 632 • disengages both A/Ps • prevents A/P engagement. Lift up – • conceals yellow background • enables A/P engagement. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.10.16 D6-27370-866-EGP...
  • Page 633 CONTROL STAND CONTROL WHEELS Autopilot Disengage Switch Push – • disengages both autopilots • A/P disengage lights flash Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 4.10.17...
  • Page 634 P/RST P/RST P/RST TEST LEFT FORWARD PANEL RIGHT FORWARD PANEL STAB OUT OF TRIM LEFT FORWARD PANEL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.10.18 D6-27370-866-EGP...
  • Page 635 TEST 2 – illuminates autopilot/autothrottle disengage lights steady red and FMC alert light steady amber. Spring–loaded to center position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 636 • D-TO 2 – derate two and assumed temperature reduced thrust takeoff • CLB – climb • CLB 1 – derated climb one Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.10.20...
  • Page 637 • FMC SPD (green) Roll Engaged Mode • HDG SEL (green) • LNAV (green) • VOR/LOC (green) Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 4.10.21...
  • Page 638 Pitch Armed Mode • G/S (white) • FLARE (white) • V/S (white) • G/S V/S (white) • VNAV (white) Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.10.22 D6-27370-866-EGP...
  • Page 639 All AFDS modes can be disengaged either by selecting another command mode or by disengaging the A/P and turning the F/Ds off. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP...
  • Page 640 The AFDS will maintain the active pitch and roll modes with flight director guidance. • either left or right IRS system failure or FAULT light illuminated Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.20.2...
  • Page 641 • with one or both A/Ps engaged in CMD, the FCC for the first A/P in CMD is the master FCC, regardless of which F/D is turned on first. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 4.20.3...
  • Page 642 Armed modes are shown in smaller white letters at the bottom of the flight mode annunciation boxes. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.20.4...
  • Page 643 • inflight above 2000 feet radio altitude with flaps not up or G/S captured • not in takeoff mode • either F/D ON or OFF. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 4.20.5...
  • Page 644 50 feet RA. • LNAV (armed) – in the approach phase and a missed approach exists in the flight plan. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.20.6...
  • Page 645 When approaching a selected altitude in CWS P with a CMD engage switch selected, CWS P changes to ALT ACQ. When at the selected altitude, ALT HOLD engages. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 646 MCP SPD or FMC SPD mode. The A/T Arm switch is magnetically held at ARM and releases to OFF when the A/T becomes disengaged. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.20.8...
  • Page 647 N1 thrust limit as selected from the FMC. The autopilot may be engaged after takeoff. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 4.20.9...
  • Page 648 A second press of the TO/GA switch above 800 feet above field elevation, thrust levers advance toward full GA thrust. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.20.10...
  • Page 649 OFF. Above 400 feet RA, selection of another pitch mode or engaging an autopilot will terminate the takeoff mode; other F/D roll modes can be also selected. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 650 84 knots – • A/T THR HLD mode engages TO/GA Push TO/GA Switch (both FD ON and A/T armed) Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.20.12 D6-27370-866-EGP...
  • Page 651 (LNAV) and a vertical navigation track (VNAV) provided by the FMC. Other roll modes available are: • VOR course (VOR/LOC) • heading select (HDG SEL). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 4.20.13...
  • Page 652 1500 RA occurs. The localizer can be intercepted in the HDG SEL, CWS R or LNAV mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.20.14...
  • Page 653 The A/Ps disengage and the F/D command bars retract to indicate an invalid ILS signal. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 4.20.15...
  • Page 654 • A/P status of SINGLE CH is annunciated for the entire approach after localizer capture • an A/P go–around is not available. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.20.16...
  • Page 655 For a single channel or F/D only approach, the autopilot will disconnect and/or the F/D bars will be removed if a persistent localizer/glideslope beam anomaly or ground station failure is detected. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 656 Automatic Flight - System Description 737 Flight Crew Operations Manual Automatic Flight Approach Profile ILS APPROACH Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.20.18 D6-27370-866-EGP...
  • Page 657 With the second push of either TO/GA switch after A/T reaches reduced go– around thrust, the A/T advances to the full go–around N1 limit. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 4.20.19...
  • Page 658 • inflight above 2000 feet RA with flaps not up or G/S captured • not in takeoff mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.20.20...
  • Page 659 • pitch mode engages in TO/GA and the Pitch Engaged Mode annunciation on the FMA indicates TO/GA • the F/D target speed is displayed on IAS/Mach display Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 660 Single channel autopilot minimum engage and use heights are not affected. This feature is recommended to support RNP RNAV operations for terminal procedures requiring definitive course guidance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.20.22...
  • Page 661 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 4.20.23...
  • Page 662 • landing gear placard • minimum speed. The commanded speed can be equal to, but does not exceed a limit speed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.20.24...
  • Page 663 AFDS, if in a V/S mode, will automatically engage to LVL CHG mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 4.20.25...
  • Page 664 ALT HOLD or after G/S capture. Minimum speed reversion is also not available when in VNAV PTH and flying a level segment. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 4.20.26...
  • Page 665 ACARS System ........5.20.6 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 666 Communications - Table of Contents 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 5.TOC.2 D6-27370-866-EGP September 15, 2016...
  • Page 667 • the tuned frequency is displayed in the ACTIVE frequency indicator • the standby frequency is displayed in the STANDBY frequency indicator Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2009 D6-27370-866-EGP...
  • Page 668 AM Switch Push – sets the AM (amplitude modulation) or USB (upper side band) mode for the selected HF. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 18, 2011 5.10.2...
  • Page 669 Note: The selected frequencies may continue to be displayed in the frequency indicator when the radio is not available. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 5.10.3...
  • Page 670 FLIGHT DECK CREW STATIONS YW273, YW274 MIC SELECTOR VHF1 VHF2 VHF3 CABIN 1-NAV-2 1-ADF-2 SPKR NORM FLIGHT DECK CREW STATIONS Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 5.10.4 D6-27370-866-EGP...
  • Page 671 I/C (Intercom) – keys oxygen mask or boom microphone for direct transmission over flight interphone and bypasses transmitter selector. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 5.10.5...
  • Page 672 Alternate–Normal (ALT–NORM) Switch NORM (Normal) – ACP operates normally. ALT (Alternate) – ACP operates in degraded mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 5.10.6 D6-27370-866-EGP...
  • Page 673 Push - resets message light. Test Switch Push - • produces character test pattern • illuminates MSG and FAIL lights. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 5.10.7...
  • Page 674 Illuminated (amber) - printer failure or test in progress. Paper Quantity Indicator Indicates amount of paper remaining. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 5.10.8 D6-27370-866-EGP...
  • Page 675 Standard Microphones Choose desired microphone for voice transmission through selected radio, interphone system, or passenger address (PA). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 5.10.9...
  • Page 676 GLARESHIELD PANEL Glareshield MIC Switch Push - allows oxygen mask or boom microphone transmission on the selected transmitter. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 5.10.10 D6-27370-866-EGP...
  • Page 677 • with SERVICE INTERPHONE switch ON, also used to communicate with any external jack location • bypasses ACP. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 678 FORWARD OVERHEAD PANEL YK996 - YQ456 COCKPIT VOICE RECORDER ERASE TEST HOLD 5 SEC HEADSET FORWARD OVERHEAD PANEL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 5.10.12 D6-27370-866-EGP...
  • Page 679 Illuminated (momentary green) – no faults are detected during recorder TEST. YK996 - YQ456 TEST Light Illuminates (green) - when the TEST switch is depressed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 5.10.13...
  • Page 680 Push – • sounds a two–tone chime in passenger cabin • illuminates both pink master call lights. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 5.10.14 D6-27370-866-EGP...
  • Page 681 IN USE FORWARD OVERHEAD PANEL PA IN USE Light Illuminated (blue) - Passenger Address system is in use. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 5.10.15...
  • Page 682 OVERHEAD PANEL VIDEO ON Light Illuminated (white)–a video system program is being displayed in the passenger cabin. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 5.10.16 D6-27370-866-EGP...
  • Page 683 Headset volume is controlled by the receiver switches. Speaker volume is controlled by the receiver switches and also the speaker switch. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP 5.20.1...
  • Page 684 The control wheel PTT switch INT position and the ACP PTT switch I/C position are not functional since the flight interphone is not functional. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 5.20.2...
  • Page 685 Anyone who picks up a handset/microphone is automatically connected to the system. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 5.20.3...
  • Page 686 The PA speakers also provide an alerting chime signal whenever the NO SMOKING or FASTEN SEAT BELT signs illuminate or extinguish. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 5.20.4...
  • Page 687 Each HF radio can be tuned by any radio tuning panel. HF radio sensitivity can only be set on the on-side radio tuning panel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP 5.20.5...
  • Page 688 (MCDU), and frequently a printer. Data is entered and transmitted to the ground operations center. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 5.20.6...
  • Page 689 Battery Charger Transformer/Rectifier....6.20.9 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 690 Basic Equipment Operating – Captain Instrument Panel ..6.20.16 Basic Equipment Operating – First Officer Instrument Panel 6.20.17 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 6.TOC.2...
  • Page 691 GEN OFF APU GEN GEN OFF OFF BUS GEN 1 APU GEN GEN 2 FORWARD OVERHEAD PANEL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2009 D6-27370-866-EGP 6.10.1...
  • Page 692 Indicates voltage of source selected by DC meters selector. AC Ammeter Indicates amperage of source selected by AC meters selector. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 6.10.2...
  • Page 693 • energizes relays to provide automatic switching of standby electrical system to battery power with loss of normal power. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 6.10.3...
  • Page 694 ON – supplies electrical power to installed components of the passenger seats, in-flight entertainment systems, and other power systems. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 6.10.4...
  • Page 695 Illuminated (amber) – one or more of the following busses are unpowered: • AC standby bus • DC standby bus • battery bus. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 6.10.5...
  • Page 696 GEN OFF APU GEN GEN OFF OFF BUS GEN 1 APU GEN GEN 2 FORWARD OVERHEAD PANEL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. May 15, 2008 6.10.6 D6-27370-866-EGP...
  • Page 697 AC transfer busses • DC cross tie relay opens to isolate DC bus 1 from DC bus 2. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP 6.10.7...
  • Page 698 • other AC transfer bus continues to receive power from the IDG. Ground Service Switch GROUND SERVICE FWD ATTENDANT PANEL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 6.10.8 D6-27370-866-EGP...
  • Page 699 • ON – connects external power to ground service busses • OFF – disconnects external power from ground service busses. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP 6.10.9...
  • Page 700 Electrical - Controls and Indicators 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 6.10.10 D6-27370-866-EGP...
  • Page 701 When connected, external power can supply power to both transfer busses. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP...
  • Page 702 BATTERY SWITCH - ON STANDBY POWER SWITCH - AUTO BUS TRANSFER SWITCH - AUTO ENGINE GENERATOR CONNECTED TO RELATED BUS Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 6.20.2 D6-27370-866-EGP...
  • Page 703 BTBs. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 6.20.3...
  • Page 704 CAB/UTIL Power Switch to OFF, then back ON. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 6.20.4...
  • Page 705 An integral electro–mechanical disconnect device provides for complete mechanical isolation of the IDG. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. May 15, 2008 D6-27370-866-EGP 6.20.5...
  • Page 706 TRs. The standby power and battery bus displays only DC voltage. The TEST position is used by maintenance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. May 15, 2008 6.20.6...
  • Page 707 On the ground, an amber ELEC light comes on to indicate that a fault exists in DC power system or standby power system. The ELEC light is inhibited in flight. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. May 15, 2008 D6-27370-866-EGP 6.20.7...
  • Page 708 The battery must be above minimum voltage to operate units supplied by this bus. An amber BAT DISCHARGE light comes on when excessive battery discharge is detected. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. May 15, 2008 6.20.8...
  • Page 709 DC bus 1, the AC and DC standby busses are powered by the battery/battery charger. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. May 15, 2008 D6-27370-866-EGP...
  • Page 710 BATTERY SWITCH - ON STANDBY POWER SWITCH - AUTO BUS TRANSFER SWITCH - AUTO ENGINE GENERATOR CONNECTED Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 6.20.10 D6-27370-866-EGP...
  • Page 711 Positioning the standby power switch to OFF de–energizes both the AC standby bus and the DC standby bus and illuminates the STANDBY PWR OFF light. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 6.20.11...
  • Page 712 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 6.20.12...
  • Page 713 AUTO HOT BAT BUS AC STANDBY BUS TRANSFER BUSSES POWERED SWITCHED OR NOT POWERED HOT BAT BUS Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 25, 2010 D6-27370-866-EGP 6.20.13...
  • Page 714 • APU and engine fire extinguisher bottles • APU and engine fire detection system • Cargo fire extinguisher bottles Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 6.20.14...
  • Page 715 • inboard antiskid system • ANTISKID INOP light • parking brake • air/ground system • landing gear indicator lights Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 23, 2010 D6-27370-866-EGP 6.20.15...
  • Page 716 BATTERY SWITCH - ON INOPERATIVE WITH ONLY THE BATTERY AND STANDBY POWER SWITCH - AUTO INSTRUMENTS STANDBY BUSSES POWERED. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 23, 2010 6.20.16 D6-27370-866-EGP...
  • Page 717 BATTERY SWITCH - ON INOPERATIVE WITH ONLY THE BATTERIES AND STANDBY POWER SWITCH - AUTO INSTRUMENTS STANDBY BUSSES POWERED. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 25, 2010 D6-27370-866-EGP 6.20.17...
  • Page 718 Electrical - System Description 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 25, 2010 6.20.18 D6-27370-866-EGP...
  • Page 719 Introduction ......... . 7.20.1 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 720 Electronic Control Unit (ECU) ......7.30.3 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 721 APU Automatic Load Shedding ......7.30.3 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 722 Engines, APU - Table of Contents 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 7.TOC.4 D6-27370-866-EGP September 15, 2016...
  • Page 723 FUEL QTY-KGS X 1000 15.4 TOTAL UPPER DISPLAY UNIT Primary Engine Indications Fuel Quantity Indications Refer to Chapter 12, Fuel Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. June 5, 2009 D6-27370-866-EGP 7.11.1...
  • Page 724 • CLB 1 – derated climb one • CLB 2 – derated climb two • CRZ – cruise • G/A – go–around Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. June 5, 2009 7.11.2 D6-27370-866-EGP...
  • Page 725 • respective N1 reference bug and readout manually set by turning N1 SET inner knob • has no effect on A/T operation. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 D6-27370-866-EGP...
  • Page 726 Displays N1% RPM: • displayed (white) – normal operating range • displayed (red) – operating limit exceeded. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 7.11.4 D6-27370-866-EGP...
  • Page 727 Displayed (green) – cowl anti–ice valve(s) open. Displayed (amber) – cowl anti–ice valve is not in position indicated by related engine anti–ice switch. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 D6-27370-866-EGP...
  • Page 728 Exhaust Gas Temperature (EGT) Indications Displayed (white) – normal operating range. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. June 5, 2009 7.11.6...
  • Page 729 OPEN OPEN OIL FILTER OIL FILTER BYPASS BYPASS LOW OIL LOW OIL PRESSURE PRESSURE UPPER DISPLAY UNIT Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 D6-27370-866-EGP 7.11.7...
  • Page 730 • during landing below 200 feet RA until 30 seconds after touchdown • during periods when blinking is inhibited, alerts illuminate steady. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 7.11.8...
  • Page 731 • in flight when an engine start lever moved to CUTOFF • in flight when an engine fails • when a secondary engine parameter exceeds normal operating range. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 D6-27370-866-EGP...
  • Page 732 87.6 LOWER DISPLAY UNIT Crossbleed Start (X–BLD) Indication Displayed (magenta) – crossbleed air recommended for inflight start. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 7.11.10 D6-27370-866-EGP...
  • Page 733 (kilograms per hour x 1000). Fuel Used Readout (digital) Displayed (white) – when FUEL FLOW switch moved to USED or RESET. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP...
  • Page 734 • amber band not displayed below 65% N2. Low Oil Pressure (OIL PRESS) Redline Displayed (red) – oil pressure operating limit. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 7.11.12...
  • Page 735 High Oil Temperature (OIL TEMP) Redline Displayed (red) – oil temperature operating limit. Oil Quantity Indications OIL QTY LOWER DISPLAY UNIT Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 D6-27370-866-EGP 7.11.13...
  • Page 736 High Limit Displays tick mark and thick line. Vibration (VIB) Pointer Displayed (white) – engine vibration level. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 7.11.14 D6-27370-866-EGP...
  • Page 737 The digital readouts display amber or red if limits are exceeded. Vibration (VIB) Indications Displayed as digital readout only. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 27, 2012 D6-27370-866-EGP...
  • Page 738 The color of the outline matches the color of the exceedance - amber, red or white. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 18, 2011 7.11.16...
  • Page 739 IDLE. FLT – provides ignition to both igniters when engine start lever is in IDLE. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 7.15.1...
  • Page 740 Refer to section 20, Engines, APU - Engine System Description MFD System (SYS) Switch Refer to: • Chapter 13, Hydraulics • Chapter 9, Flight Controls Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 7.15.2 D6-27370-866-EGP...
  • Page 741 • when ON is not in view, the EEC has been manually selected to the alternate mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 742 Terminating reverse thrust removes locking pawl and restores forward thrust lever movement ability. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 7.15.4...
  • Page 743 • controls engine thrust • cannot be advanced if the reverse thrust lever is in the deployed position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 744 • electrically opens spar fuel shutoff valve in the wing leading edge outboard of the pylon • electrically opens engine–mounted fuel shutoff valve via the EEC. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 7.15.6...
  • Page 745 APU Exhaust Gas Temperature (EGT) Indicator Displays APU EGT EGT indicator remains powered for 5 minutes after shutdown. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 746 START (momentary) – positioning APU switch from OFF to START and releasing it to ON, initiates an automatic start sequence. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 7.15.8...
  • Page 747 Captain’s or First Officer’s inboard DU, or the lower DU, using the respective display select panel and the ENG switch on the engine display control panel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP...
  • Page 748 15% N2. At 15% N2, the EEC becomes energized and pointers/digits for all engine parameters are displayed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 7.20.2...
  • Page 749 Secondary Eng Primary ENG/ND Comp Eng/ND Comp Eng/ND Comp Eng/ND Comp Eng/ND Primary ENG/ND Comp Eng/ND Comp Eng/ND Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 7.20.3...
  • Page 750 N1 thrust ratings. The EEC compares commanded N1 to actual N1 and adjusts fuel flow to achieve the commanded N1. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 7.20.4...
  • Page 751 The EGT limit must be observed by the crew because the EEC does not provide EGT redline exceedance protection. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 7.20.5...
  • Page 752 In flight, if a fault prevents the EEC from receiving flap or anti–ice signals, approach idle schedule begins below 15,000 feet MSL. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 7.20.6...
  • Page 753 & INDICATORS ENGINE START & IGNITION SYSTEM FROM ELECTRICAL SYSTEM FROM FROM BLEED AIR FUEL SYSTEM SYSTEM Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 7.20.7...
  • Page 754 Prior to returning to the oil tank, the oil passes through the main engine oil cooler where it is cooled by engine fuel to maintain proper oil temperature. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 7.20.8...
  • Page 755 TANK CLOSED) ARE SENSED BY THE CONDITION: EEC, DIGITIZED, AND SENT OPERATION TO THE CDS. NORMAL ENGINE Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 7.20.9...
  • Page 756 If a wet start is detected, the EEC turns off the ignition and shuts off fuel to the engine 15 seconds after the start lever is moved to IDLE. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 7.20.10...
  • Page 757 N2 dial. This indication is based on airplane altitude, airspeed and N2. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP...
  • Page 758 IDLE CUTOFF RIGHT IGNITER CONDITION: ENGINE BEING STARTED BLEED AIR N2 ROTATION BELOW STARTER CUTOUT SPEED. FUEL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 7.20.12 D6-27370-866-EGP...
  • Page 759 IDLE CUTOFF RIGHT IGNITER CONDITION: ENGINE BEING STARTED BLEED AIR N2 ROTATION BELOW STARTER CUTOUT SPEED. FUEL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 7.20.13...
  • Page 760 After the thrust reverser is stowed, the isolation valve closes and the electro–mechanical lock engages. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 7.20.14...
  • Page 761 WARNING: Actuation of the thrust reversers on the ground without suitable precautions is dangerous to ground personnel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 762 (CLOSED) (LOCKED) (UNLOCKED) BLOCKER DOOR FAN FLOW FAN FLOW CASCADE TRANSLATING TRANSLATING VANES SLEEVE CASCADE SLEEVE VANES Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 7.20.16 D6-27370-866-EGP...
  • Page 763 The AVM is also used to balance the low pressure rotor. Balancing reduces high vibration indication or audible noise and tactile vibration. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 764 Engines, APU - Engine System Description 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 7.20.18 D6-27370-866-EGP...
  • Page 765 No. 1 tank. During APU operation, fuel is automatically heated to prevent icing. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 7.30.1...
  • Page 766 The start cycle may take as long as 120 seconds. Automatic shutdown occurs in the event of EGT exceedance. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 7.30.2...
  • Page 767 CAB/UTIL Power Switch to OFF, then back ON. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP 7.30.3...
  • Page 768 Engines, APU - APU System Description 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 7.30.4 D6-27370-866-EGP...
  • Page 769 Lavatory Fire Extinguisher System ..... 8.20.7 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 770 Cargo Fire Extinguisher Test ......8.20.9 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 771 OVHT/FIRE – tests overheat and fire detection loops on both engines and APU, and wheel well fire detector Note: See Fire and Overheat Detection System Fault Test in Section 20. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 18, 2011 D6-27370-866-EGP...
  • Page 772 • deactivates engine driven hydraulic pump LOW PRESSURE light • allows engine fire switch to rotate. Rotate (left or right) – discharges related fire bottle. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 18, 2011 8.10.2...
  • Page 773 • an associated engine fire is detected, or • the fire TEST switch is held to the OVHT/FIRE position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 8.10.3...
  • Page 774 Illuminated (amber) – indicates APU detector loop has failed. Note: MASTER CAUTION and OVHT/DET system annunciator lights illuminate. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 8.10.4...
  • Page 775 Illuminated (amber) - • One or more of the selected detector loop(s) in either cargo compartment has failed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 776 60 minutes to discharge the second extinguisher bottle. Master Fire Warning Light FIRE WARN BELL CUTOUT GLARESHIELD Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 8.10.6 D6-27370-866-EGP...
  • Page 777 Note: Armed only if APU fire control handle is pulled at this panel. APU Fire Control Handle Up – normal position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 778 APU fire indication. Lavatory Fire Lavatory Fire Extinguisher 230° F 180°F 200°F 250°F BLACK WHEN EXPOSED BELOW LAVATORY SINK Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 8.10.8 D6-27370-866-EGP...
  • Page 779 Flat black – normal condition. Aluminum – indicates extinguisher has discharged. Both nozzles discharge toward the towel disposal container. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 780 Fire Protection - Controls and Indicators 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 8.10.10 D6-27370-866-EGP...
  • Page 781 • both MASTER CAUTION lights illuminate • the OVHT/DET system annunciator light illuminates • the related ENG OVERHEAT light illuminates. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 D6-27370-866-EGP...
  • Page 782 The L or R BOTTLE DISCHARGE light illuminates a few seconds after the engine fire switch is rotated, indicating the bottle has discharged. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 8.20.2...
  • Page 783 Engine Fire Extinguisher Schematic DISCH DISCH L BOTTLE R BOTTLE DISCHARGE DISCHARGE LEFT RIGHT FIRE FIRE BOTTLE BOTTLE SQUIB Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 8.20.3...
  • Page 784 • allows the APU fire switch to be rotated for discharge • arms the APU fire extinguisher bottle squib. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 18, 2008 8.20.4...
  • Page 785 • the fire warning bell sounds • both master FIRE WARN lights illuminate • the FWD/AFT cargo fire warning light(s) illuminates. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 786 • an aural warning sounds • the red alarm indicator light on the lavatory smoke detector panel illuminates. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 31, 2016 8.20.6...
  • Page 787 FAULT/INOP and OVHT/FIRE TEST switch in the OVHT/FIRE position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 8.20.7...
  • Page 788 • the fire warning bell sounds • both master FIRE WARN lights illuminate • the extinguisher test lights illuminate Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 8.20.8...
  • Page 789 When the Cargo Fire TEST button is pushed, the green EXT lights illuminate, verifying the fire bottle discharge squib circuit continuity is normal. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 25, 2010 D6-27370-866-EGP 8.20.9...
  • Page 790 Fire Protection - System Description 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 25, 2010 8.20.10 D6-27370-866-EGP...
  • Page 791 Yaw Control Schematic ......9.20.14 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 792 Asymmetry and Skew Detection and Protection ..9.20.22 Uncommanded Motion Detection, Protection and Indication. 9.20.22 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 9.TOC.2...
  • Page 793 OFF - closes flight control shutoff valve isolating ailerons, elevators and rudder from associated hydraulic system pressure. ON (guarded position) - normal operating position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP...
  • Page 794 • Illuminated (amber) - indicates the standby rudder system is commanded on to pressurize the standby rudder power control unit. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 9.10.2...
  • Page 795 • indicates failure of a single FCC channel when MASTER CAUTION light recall is activated and light extinguishes when master caution system is reset. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 796 • indicates failure of a single Stall Management/Yaw Damper (SMYD) computer when illuminated during MASTER CAUTION recall and extinguishes when master caution system is reset. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 9.10.4...
  • Page 797 Indicates units of airplane trim on the adjacent scale. Stabilizer Trim Green Band Range Corresponds to allowable range of trim settings for takeoff. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 798 NORM (guarded position) – normal operating position. Stabilizer Out of Trim (STAB OUT OF TRIM) Light Refer to Chapter 4 – Automatic Flight Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 9.10.6...
  • Page 799 • controls rudder position • permits limited nose gear steering up to 7 degrees each side of center. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 800 YAW DAMPER Indicator • Indicates main yaw damper movement of rudder • pilot rudder pedal inputs are not indicated. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 23, 2010 9.10.8...
  • Page 801 Push/Pull – • operates elevators in the desired direction • movement opposing stabilizer trim stops electric trimming. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 23, 2010 D6-27370-866-EGP 9.10.9...
  • Page 802 Illuminated (green) – indicates valid automatic speed brake system inputs. SPEED BRAKE DO NOT ARM Light Light deactivated when SPEED BRAKE lever is in the DOWN position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 9.10.10...
  • Page 803 Note: On the ground, the SPEEDBRAKES EXTENDED light does not illuminate when hydraulic system A pressure is less than 750 psi. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 23, 2010 D6-27370-866-EGP 9.10.11...
  • Page 804 • provides TE flaps asymmetry and skew indication. FLAPS LIMIT Placard Indicates maximum speed for each flap setting. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 9.10.12...
  • Page 805 • during alternate flap extension until LE devices are fully extended and TE flaps reach flaps 15. Note: Light is inhibited during autoslat operation in flight. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 23, 2010 D6-27370-866-EGP...
  • Page 806 (TE flap positions 1, 2, 5, 10, 15, and 25) • all LE devices fully extended (TE flap positions 30 and 40). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 26, 2015 9.10.14...
  • Page 807 • top mark depicts maximum up position • center mark depicts neutral position • bottom mark depicts maximum down position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 31, 2016 D6-27370-866-EGP...
  • Page 808 • right mark depicts maximum right position. Note: Main and standby yaw damper movement of the rudder are shown on this indicator. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 26, 2015 9.10.16...
  • Page 809 There is a rigid connection between both pairs of rudder pedals. The SPEED BRAKE lever allows manual or automatic symmetric actuation of the spoilers. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP...
  • Page 810 Flight Control Surfaces Location BLENDED WINGLETS RUDDER AILERONS ELEVATORS TE FLAPS FLIGHT SPOILERS STABILIZER GROUND SPOILERS LE FLAPS LE SLATS Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 9.20.2 D6-27370-866-EGP...
  • Page 811 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 9.20.3...
  • Page 812 The flight spoilers rise on the wing with up aileron and remain faired on the wing with down aileron. When the control wheel is displaced more than approximately 10°, spoiler deflection is initiated. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 9.20.4...
  • Page 813 FEEL AND SPOILER SPOILER CENTERING CENTERING MIXER MIXER UNIT UNIT FLIGHT FLIGHT SPOILERS SPOILERS AILERON AILERON SPOILER SPOILER Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 9.20.5...
  • Page 814 FEEL DIFF PRESS light illuminates. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 9.20.6...
  • Page 815 Grasping the stabilizer trim wheel will stop stabilizer motion. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 9.20.7...
  • Page 816 0.60 with a fadeout to zero by • Autopilot not engaged Mach 0.68 • Sensing of trim requirement • 10 seconds after takeoff Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 9.20.8 D6-27370-866-EGP...
  • Page 817 MACH TRIM ACTUATOR ELEVATOR FEEL ELEVATOR FEEL & CENTERING UNIT & CENTERING UNIT STABILIZER STABILIZER TRIM TRIM Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 9.20.9...
  • Page 818 With the column aft, the amount of column force increase with the onset of EFS module is more pronounced. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 9.20.10...
  • Page 819 Monitor. The STBY RUD ON light illumination activates Master Caution and Flight Control warning lights on the Systems Annunciation Panel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 9.20.11...
  • Page 820 • SMYD senses that the yaw damper does not respond to a command, • B FLT CONTROL switch is positioned to OFF or STBY RUD. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 9.20.12...
  • Page 821 PCU to move the rudder. This gives rudder assist to help turn the airplane when control of the ailerons is through manual reversion. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 23, 2010 D6-27370-866-EGP...
  • Page 822 STANDBY YAW DAMPER STANDBY STANDBY RUDDER PCU RUDDER PCU STANDBY STANDBY RUDDER RUDDER SHUTOFF SHUTOFF VALVE VALVE Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 23, 2010 9.20.14 D6-27370-866-EGP...
  • Page 823 • both thrust levers are retarded to IDLE • main landing gear wheels spin up (more than 60 kts). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 9.20.15...
  • Page 824 DOWN detent and all spoiler panels retract. The spoiler panels may also be retracted by manually moving the SPEED BRAKE lever to the DOWN detent. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 9.20.16...
  • Page 825 FLIGHT SPOILERS: 2, 3, 4, 5, 8, 9, 10, 11 GROUND SPOILERS: 1, 6, 7, 12 GROUND SPOILERS: 1, 6, 7, 12 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 826 The LE DEVICES annunciator panel on the aft overhead panel indicates the positions of the individual flaps and slats. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 9.20.18...
  • Page 827 The slats return to the extend position when the pitch angle is sufficiently reduced below the stall critical attitude. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 9.20.19...
  • Page 828 ALTERNATE FLAPS position switch, held in the down position momentarily, fully extends the LE devices. Note: The LE devices cannot be retracted by the standby hydraulic system. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 23, 2010 9.20.20...
  • Page 829 SLATS FLAPS FLAPS TEST TEST SMYD SMYD LE FLAPS LE FLAPS LE FLAPS LE FLAPS TRANSIT TRANSIT Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 23, 2010 D6-27370-866-EGP 9.20.21...
  • Page 830 FSEU maintains pressure on the retract lines and depressurizes the extend and full extend lines. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 9.20.22...
  • Page 831 TE flaps. The shutdown is indicated by the flap position indicator disagreeing with the FLAP lever position. There is no flap needle split. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 23, 2010 D6-27370-866-EGP 9.20.23...
  • Page 832 Flight Controls - System Description 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 23, 2010 9.20.24 D6-27370-866-EGP...
  • Page 833 Display System Annunciations..... . . 10.11.28 Displays Control Panel Annunciation (EFIS CP)..10.11.29 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. D6-27370-866-EGP 10.TOC.1...
  • Page 834 EFIS Control Panel Controls – Flight Instrument Displays . . 10.16.1 EFIS Control Panel Controls – Navigation Displays ..10.16.2 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. 10.TOC.2...
  • Page 835 Inboard Display Switching ......10.21.9 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 836 Approach Minimums ........10.31.3 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 837 Introduction ......... 10.42.1 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 838 Electronic Log Book (Fault Locator) ....10.65.36 Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
  • Page 839 Captain Inboard Display Unit Upper Display Unit First Officer Inboard Display Unit First Officer Outboard Display Unit Lower Display Unit Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 10.11.1...
  • Page 840 Displays current flight modes; refer to Chapter 4, Automatic Flight. Airspeed/Mach Indications Attitude Indications Autopilot, Flight Director System Status Altitude Indications Vertical Speed Indications Heading/Track Indications Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 10.11.2 D6-27370-866-EGP...
  • Page 841 LEFT FORWARD PANEL Navigation Display Displays map, approach, VOR, or plan modes as selected on the EFIS control panel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 10.11.3...
  • Page 842 RIGHT FORWARD PANEL Navigation Display Displays map, approach, VOR, or plan modes as selected on the EFIS control panel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 10.11.4 D6-27370-866-EGP...
  • Page 843 Displays current flight modes; refer to Chapter 4, Automatic Flight. Airspeed/Mach Indications Attitude Indications Autopilot, Flight Director System Status Altitude Indications Vertical Speed Indications Heading/Track Indications Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 10.11.5...
  • Page 844 Tip of arrow indicates predicted airspeed in the next 10 seconds based on the current airspeed and acceleration. Current Airspeed (white) Indicates current calibrated airspeed in knots. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 10.11.6 D6-27370-866-EGP...
  • Page 845 • when transitioning from Mach to groundspeed or from groundspeed to Mach, a white box shows around the numeric value for 10 seconds. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.7...
  • Page 846 5 position or SET position and a value greater than 60 knots has been selected. Not available if the speed reference selector is in the AUTO position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 10.11.8...
  • Page 847 FMC maintenance pages) above approximately 20,000 ft. Note: 1.3g maneuver capability occurs at 40 degrees of bank in level flight. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 D6-27370-866-EGP...
  • Page 848 INVALID ENTRY is displayed • removed when the speed reference selector is moved to the SET position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.10...
  • Page 849 Provides fixed reference for the bank pointer; scale marks are at 0, 10, 20, 30, 45, and 60 degrees. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.11...
  • Page 850 • flight path angle is displayed relative to the horizon line • drift angle is displayed relative to display center. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.12...
  • Page 851 • LOC/VNAV – (ILS localizer course with VNAV deviation) • LNAV/ G/S – (LNAV deviation with glideslope) • ILS – (ILS approach) Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 852 • turn from white to amber if current deviation is within the ANP bar limits for 5 continuous seconds. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.14...
  • Page 853 • in view when the localizer signal is received • fills in solid magenta when within 2 ½ dots from center. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.15...
  • Page 854 Displayed when: • localizer signal usable and pointer is in view. • radio altitude is less than 2500 feet. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.16...
  • Page 855 • box highlighted white for 10 seconds upon descent below 2500 feet • turns amber when below radio altitude minimums. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.17...
  • Page 856 PULL UP GPWS Annunciations (red) Displays WINDSHEAR or Pull UP alert. Refer to Chapter 15, Warning Systems. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.18 D6-27370-866-EGP...
  • Page 857 Metric Digital Readout (readout and box–white, metric symbol–cyan) Displays current altitude in meters when MTRS is selected on the EFIS control panel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 858 Preselected Barometric Setting (white) STD is displayed when the Barometric Standard (STD) switch is selected on the EFIS control panel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.20...
  • Page 859 • the landing altitude for departure runway or airport until 400 NM from departure or one-half the distance to destination, whichever occurs first. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.21...
  • Page 860 • White bar – 500 to 1000 feet above landing altitude • Amber bar – 0 to 500 feet above landing altitude. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.22...
  • Page 861 Vertical speed pointer is red if it is within the vertical speed tape range. Supplements TCAS resolution advisory pitch commands on the attitude indication. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 862 – 800 feet per minute, an amber box is drawn around TRU; the box flashes for 10 seconds, then turns steady amber. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.24...
  • Page 863 The flag replaces the appropriate display to indicate system failure. YK981 - YQ456 SEL SPD PITCH ROLL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.25...
  • Page 864 • if the maximum operating speed has failed, the red and black maximum operating speed bar is removed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.26...
  • Page 865 The attitude display has failed. Landing Altitude Flag (amber) The landing altitude input is not available or invalid. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 866 CDS MAINT (white) – A dispatchable CDS fault has occurred. Displayed on the ground only, prior to start of the second engine. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.28...
  • Page 867 • engagement of the second autopilot is inhibited. Displays Control Panel Annunciation (EFIS CP) 1000 BARO 4750 DISPLAYS CONTROL PANEL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.29...
  • Page 868 Displayed when the IRS switch on the overhead panel is not in the NORMAL position. See Chapter 11, Section 10, for Inertial Reference System Transfer Switch information. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.30...
  • Page 869 Airspeed Disagree Alert (amber) Indicates the Captain’s and F/O’s airspeed indications disagree by more than 5 knots for 5 continuous seconds. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 870 5 continuous seconds. YW273, YW274 Refer to Chapter 15 Warning Systems for the aural alerts associated with RCAS. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.32...
  • Page 871 • slip/skid indication outline will turn amber. • slip/skid indication will fill amber if deflected greater than 25% of its width, Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 872 • is replaced by the active autopilot status annunciation when less than 100% of the autopilot roll authority is required. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.34...
  • Page 873 • when the bank angle is less than 35 degrees for 2 seconds, or; • immediately if the bank angle is less than 10 degrees. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.35...
  • Page 874 ELN01 1432.0 17.1 ELN02 ELN01 APRT WX+T ADF 1 VOR 2 KXYZ FMC L 18.5 CENTER MAP Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.36 D6-27370-866-EGP...
  • Page 875 Vertical Deviation Scale and Pointer Position Trend Vector Magnetic/True Reference Number 2 VOR/ADF Pointer VOR/ADF Selection, Ident/Frequency, VOR DME Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.37...
  • Page 876 Indicates current airplane altitude (bottom of the triangle) and lateral position (point of the triangle) relative to terrain. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.38...
  • Page 877 Displays range in nautical miles. Actual range shown on VSD is one half the range selected on the EFIS control panel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.39...
  • Page 878 Displayed with any altitude constraint directly beneath. Dashed vertical line depicts lateral position. Altitude Constraint Symbol Displayed as triangle(s) on waypoint anchor line. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.40 D6-27370-866-EGP...
  • Page 879 • anchored to the missed approach waypoint, not the runway. • manual altitude corrections do not change the displayed Navigation Database defined glidepath. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 880 Displayed on the FMC approach glide path angle line or 3 degree reference line at 500 feet and 1000 feet above field elevation. Runway Represents the selected runway. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.42 D6-27370-866-EGP...
  • Page 881 Note: See Chapter 15, Section 10, for Terrain Warnings. Vertical Support Lines Vertical terrain vectors placed at constant intervals along the terrain profile line. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 882 28.5 EXPANDED APPROACH MODE ILS 1 IALT 13.5 ADF 1 VOR 2 KXYZ 28.5 CENTER APPROACH MODE Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.44 D6-27370-866-EGP...
  • Page 883 Magnetic/True Reference Track Line Localizer Deviation Indication and Scale Reference ILS Frequency or Ident/Course/DME Glideslope Pointer and Scale Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.45...
  • Page 884 KXYZ 13.5 EXPANDED VOR MODE VOR 1 13.5 ADF 1 VOR 2 KXYZ 13.5 CENTER VOR MODE Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.46 D6-27370-866-EGP...
  • Page 885 Track Line Course Deviation Indication and Scale Reference VOR Receiver/Frequency or Ident/Course/DME TO/FROM Indication and TO pointer Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.47...
  • Page 886 Center Waypoint The waypoint located at the display center is identified as CTR on the CDU RTE LEGS page. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.48...
  • Page 887 RNP. Refer to Chapter 11, Section 60, FMC Messages. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 888 The annunciation is displayed in the expanded APP, center APP, expanded VOR and center VOR modes. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.50...
  • Page 889 TA (amber) or RA (red) is beyond the selected display range and TFC is selected on the EFIS control panel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.51...
  • Page 890 TERR – Terrain display enabled (manual or automatic display). TERR TEST – GPWS is operating in self-test mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.52...
  • Page 891 Predictive Windshear System (PWS) Message PWS FAIL PWS FAIL Annunciation (amber) Predictive windshear alerting and display have failed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.53...
  • Page 892 WXR DSP – Range data input has failed. Only displayed in WXR TEST AUTOTILT FAIL – Automatic radar mode has failed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.54...
  • Page 893 ILS glideslope has failed. ILS Localizer Failure Flag (expanded APP mode) ILS localizer course indication has failed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.11.55...
  • Page 894 EGPWS terrain data is not available. Annunciation is replaced with VSD TERR INHIBIT when GPWS control panel TERR INHIBIT switch is in the inhibit position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.56...
  • Page 895 Reference VOR or ILS DME has failed. ILS Localizer Failure Flag (center APP mode) ILS localizer course indication has failed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 896 PFD/ND – Displays 737 Flight Crew Operations Manual ILS Glideslope Failure Flag (center APP mode) ILS glideslope has failed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.11.58 D6-27370-866-EGP...
  • Page 897 Used for data entry and to select modes of operation. Annunciator Provides system status and warning annunciations during a CAT III approach. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 898 FMC SPD LNAV VNAV SPD H 310 -200 31.2 VOR1 24.6NM FMC L PRI (IN FLIGHT) MODE Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 10.12.2 D6-27370-866-EGP...
  • Page 899 Refer to Chapter 4, Automatic Flight. Airspeed Indications Navigation Indications Attitude Indications Altitude Indications Ground Localizer Line Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 10.12.3...
  • Page 900 Indicates current computed airspeed in knots. Displayed relative to a vertical scale along the edge of the tape and as a digital value. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 10.12.4...
  • Page 901 FMC maintenance pages) above approximately 20,000 ft. Note: 1.3g maneuver capability occurs at 40 degrees of bank in level flight. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 D6-27370-866-EGP...
  • Page 902 If the flight path vector is not displayed, the readout is positioned relative to the airplane reference symbol. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 10.12.6...
  • Page 903 Removed when either of the following occurs: • at first flap retraction • when VREF is entered in the CDU. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 D6-27370-866-EGP...
  • Page 904 Indicates 100 knots: • displayed automatically during preflight • removed at first flap retraction or when VREF is entered. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 10.12.8...
  • Page 905 BARO Minimums Pointer (PRI in flight, PRI ground modes) Displays the barometric minimums selected on the EFIS control panel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 D6-27370-866-EGP 10.12.9...
  • Page 906 Refer to section 42 for symbology descriptions. MCP SPD VOR/LOC -3.00 -3.00 450 B -600 ILS1 IMC MODE Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 10.12.10 D6-27370-866-EGP...
  • Page 907 -600 VMC MODE Mode/Status Digital Selected Airspeed Glideslope Reference Line Digital Airspeed Wind Indications Lateral Deviation Line Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 10.12.11...
  • Page 908 Glideslope Deviation Line Digital Barometric Altitude Digital Vertical Speed Radio Altitude Runway Edge Lines TCAS Resolution Advisory Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 10.12.12 D6-27370-866-EGP...
  • Page 909 HUD System Failure Indications and Flags See section 42 for detailed information on the HUD system failure indications and flags. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 D6-27370-866-EGP...
  • Page 910 Flight Instruments, Displays - Head-Up Display System - Displays 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 10.12.14 D6-27370-866-EGP...
  • Page 911 • blanks minimums display if alert is not active. Meters (MTRS) Switch (momentary action) PUSH – displays altitude indications in meters. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 D6-27370-866-EGP...
  • Page 912 TERR GLARESHIELD VOR/ADF Switch (three position) Displays VOR or ADF information on all navigation modes except PLAN. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2007 10.16.2 D6-27370-866-EGP...
  • Page 913 Range Selector (outer) Selects desired display range in nautical miles for APP, VOR, MAP or PLN mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 27, 2012 D6-27370-866-EGP...
  • Page 914 Display (VSD) when in the VSD mode format. Displayed Route Data can be cycled on or off with the route “DATA” pushbutton. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.16.4...
  • Page 915 Note: These source selectors and switches are normally used while the aircraft is on the ground for maintenance purposes. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.16.5...
  • Page 916 • Inboard Primary Flight Display (INBD PFD) – displays the PFD on the inboard display unit and blanks the outboard display unit Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.16.6...
  • Page 917 • Navigation Display (ND) – displays the navigation display on the lower unit. Speed Reference Selector SPD REF AUTO CENTER FORWARD PANEL Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.16.7...
  • Page 918 Outboard Display Unit Brightness (OUTBD DU BRT) Control (rotary) ROTATE – adjusts the brightness of the Captain outboard display unit. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.16.8...
  • Page 919 ROTATE – adjusts weather radar and terrain display brightness on the lower display unit, adjusts display contrast when MFD is in the video surveillance mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.16.9...
  • Page 920 Outboard Display Unit Brightness (OUTBD DU BRT) Control (rotary) ROTATE – adjusts the brightness of the First Officer outboard display unit. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.16.10...
  • Page 921 OFF – compass light is extinguished. BRT – sets compass light to full brightness. DIM – sets compass light to low brightness. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 922 • Beyond 30 degrees pitch, large red arrowheads (V-shaped) indicate the attitude has become excessive, and the direction to the horizon line. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.16.12...
  • Page 923 • the pointer is in view when the localizer signal is received • the scale is in view when either the APP or BCRS mode is selected Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.16.13...
  • Page 924 • countdown stops if excessive motion is detected • countdown resumes when motion stops • ATT:RST displays if initialization is not complete within six minutes. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.16.14...
  • Page 925 Altitude flag Altitude information has failed. Attitude flag Attitude information has failed. Heading flag Heading data has failed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.16.15...
  • Page 926 • ADF failure or signal unreliable. VOR/ADF Bearing Pointer No. 1 Switch ROTATE – selects VOR or ADF for the bearing pointer. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.16.16...
  • Page 927 • controls the start, stop and reset functions of the CHR display and second hand with successive pushing • overrides any existing ET display. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP...
  • Page 928 • elapsed time continues to run in the background and displays after the chronograph is reset. SET Control Controls the setting of manual time and date: Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.16.18 D6-27370-866-EGP...
  • Page 929 • indicates the recorder is not operating or the test is invalid • may indicate power failure, loss of input data, or electronic malfunction. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.16.19...
  • Page 930 Flight Instruments, Displays - PFD/ND – Controls and Indicators 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.16.20 D6-27370-866-EGP...
  • Page 931 Pilots can also push the "<CLR HGS" line select key on the MCDU HGS Data page to remove all symbology from the Combiner display. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.17.1...
  • Page 932 HGS Modes page to change the HGS modes. To change modes on the HGS Modes page, push the line select key next to the name of the mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 10.17.2...
  • Page 933 These two additional symbols are displayed relative to the airplane reference and the flight path symbols and are removed above 1500 feet. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 D6-27370-866-EGP 10.17.3...
  • Page 934 Approach symbology format for the VMC mode is similar to the IMC mode. However, navigation data is not displayed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 10.17.4...
  • Page 935 ¼ dot and glideslope deviation is less than approximately 1 ¼ dots for at least five seconds. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 D6-27370-866-EGP...
  • Page 936 On the Menu page, push the "HGS" line select key to open the HGS DATA page. The HGS data page gives access to runway length, runway elevation, glideslope, clear headings, and HGS TEST. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 10.17.6...
  • Page 937 3 left. The new glideslope angle then shows on the display and the previous value is erased. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2009 D6-27370-866-EGP 10.17.7...
  • Page 938 • All legends come on and stay on • To end the test, push the "EXIT>" line select key on the MCDU. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 10.17.8...
  • Page 939 • RO ARM (Rollout Guidance Armed) (white) – system capable of providing ground roll guidance during rollout. Displayed prior to touchdown during an AIII approach Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 D6-27370-866-EGP...
  • Page 940 • will not illuminate again until failure is cleared and another failure occurs • resets system for another failure. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 10.17.10...
  • Page 941 Head-Up Display System – Controls 737 Flight Crew Operations Manual Combiner Controls Brightness and Stow Controls OVERHEAD FLIGHT DECK Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 D6-27370-866-EGP 10.17.11...
  • Page 942 To stow the combiner glass, grasp and rotate toward the pilot, aft and up, until it locks in the stowed position. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 10.17.12...
  • Page 943 IMC and VMC modes should not be used. The ALIGN HUD restriction does not apply to use of the HUD in PRI mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 D6-27370-866-EGP 10.17.13...
  • Page 944 Flight Instruments, Displays - Head-Up Display System – Controls 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 10.17.14 D6-27370-866-EGP...
  • Page 945 DU. Brightness controls are used by the pilot to further adjust the intensity of each display unit. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 D6-27370-866-EGP 10.21.1...
  • Page 946 With the switch positioned to either BOTH ON 1 or BOTH ON 2, the selected EFIS control panel provides inputs for both sets of pilot displays. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 25, 2009 10.21.2...
  • Page 947 DUs. The inboard rotary switch controls the display format shown on the lower DU. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 25, 2009 D6-27370-866-EGP 10.21.3...
  • Page 948 All selectors are in NORMAL. Display Units The pilots’ outboard and inboard DUs show the normal PFD/ND displays. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 10.21.4...
  • Page 949 If an inboard display unit fails, the PFD format remains displayed on the outboard display unit and the inboard display unit blanks. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 10.21.5...
  • Page 950 Note: There is no automatic switching for a lower DU failure. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 10.21.6...
  • Page 951 CONTROL PANEL Select Switch BOTH ON 2 The right EFIS control panel controls both pilots’ outboard and inboard display units. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP...
  • Page 952 (OUTBD PFD), the PFD format is displayed on the outboard display unit and the inboard display unit blanks. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 10.21.8...
  • Page 953 MAIN PANEL DUs LOWER DU LOWER DU MAIN PANEL DUs NORM NORM NORM NORM OUTBD OUTBD INBD INBD Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 10.21.9...
  • Page 954 MFD switches on the engine display control unit. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 25, 2009 10.21.10...
  • Page 955 DU and the navigation display is shown on the lower DU. When the MFD ENG switch is selected, the compact engine display is shown on the upper DU. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 D6-27370-866-EGP 10.21.11...
  • Page 956 The ADIRUs are described in Chapter 11, Flight Management, Navigation. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 10.21.12...
  • Page 957 Static air temperature, displayed on the CDU PROGRESS page, comes from the ADIRUs, using total air temperature probe information. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 10.21.13...
  • Page 958 10 seconds may result in an ATT:RST message. If the reset attempt is unsuccessful, the ATT:RST message remains displayed and the ISFD does not enter normal operation. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 10.21.14...
  • Page 959 • Corrosion, fire and impact resistant, survives deep sea pressure to 13,451 feet (4,100 m) Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP...
  • Page 960 • Aircraft Communication Addressing and Reporting System (ACARS). • ACARS air/ground message functionality continuing to expand with additional message formats. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 10.21.16...
  • Page 961 • Shape and position of flight symbols • Airplane sensor status • HUD system status • HUD system mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.22.1...
  • Page 962 • IMC - used for AFDS autopilot/flight director approaches • VMC - used for visual approaches. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 10.22.2...
  • Page 963 If the HUD is in a mode other than primary, depressing a TO/GA switch activates the primary mode independent of the standby mode indicated on the HUD control panel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP...
  • Page 964 LOC and G/S capture in the PRI mode. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 10.22.4...
  • Page 965 APCH WARN annunciation will be displayed on the combiner and on the HUD annunciator panel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP...
  • Page 966 TCAS, and represents the vertical flight path position that is safe. For additional information on TCAS, refer to Chapter 15, Warning Systems. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 10.22.6...
  • Page 967 Data source annunciations are provided in a few cases to annunciate the source of displayed data when other than normal. Dashes replace numbers if there is no computed data. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP...
  • Page 968 Flight Instruments, Displays - Head-Up Display System Description 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 22, 2012 10.22.8 D6-27370-866-EGP...
  • Page 969 Pitch attitude is displayed by an airplane symbol against a pitch scale. The pitch scale is in 2.5 degree increments. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 D6-27370-866-EGP 10.31.1...
  • Page 970 90 degrees (backcourse). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 10.31.2...
  • Page 971 BARO minimums are selected. When RADIO minimums are selected, the pointer is still set at BARO minimums but there is no line. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP...
  • Page 972 Traffic Alert and Collision Avoidance (TCAS) Indications TCAS resolution advisories are displayed in the attitude indication and vertical speed indication areas. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 10.31.4...
  • Page 973 GPWS warnings are displayed in large capital letters between the attitude display and the heading/track compass rose. Refer to Chapter 15, Warning Systems. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 D6-27370-866-EGP 10.31.5...
  • Page 974 Flight Instruments, Displays - PFD/ND – Primary Flight Display 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 28, 2006 10.31.6 D6-27370-866-EGP...
  • Page 975 The PLN mode is presented true north up. The active route may be viewed using the STEP prompt on the CDU LEGS pages. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 30, 2011 D6-27370-866-EGP 10.41.1...
  • Page 976 • reducing range, or • deselecting one or more of the EFIS control panel map switches (STA, WPT, ARPT, DATA, POS). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 22, 2012 10.41.2...
  • Page 977 Expanded MAP, Displays 90 degrees of compass (W) VOR, compass rose. Groundspeed Displays current groundspeed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 D6-27370-866-EGP 10.41.3...
  • Page 978 APP CTR reference, and points to the heading reference heading on the compass rose. (G), heading pointer Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 10.41.4 D6-27370-866-EGP...
  • Page 979 VOR navigation is being used. To/from VOR, Displays VOR to/from FROM indication (W) VOR CTR indication. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 D6-27370-866-EGP 10.41.5...
  • Page 980 VOR 1, 2 annunciation (G) VOR CTR, receiver as the display ILS 1, 2 APP, reference. APP CTR Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 28, 2013 10.41.6 D6-27370-866-EGP...
  • Page 981 (tail) the tuned station, if pointer head and selected on the respective tail EFIS control panel. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 28, 2013 D6-27370-866-EGP 10.41.7...
  • Page 982 ± 400 feet deviation. Digital display is provided when the pointer deviates more than ± 30 feet from center. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.41.8 D6-27370-866-EGP...
  • Page 983 MAP CTR, waypoint. Active waypoint MAP, Indicates FMS–calculated 0835.4z ETA (W) MAP CTR, ETA at the active waypoint. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.41.9...
  • Page 984 DATA switch is selected on, 12000 0835Z inactive (W) entered or procedural altitude and ETAs for route waypoints are displayed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 10.41.10 D6-27370-866-EGP...
  • Page 985 Data within parentheses for conditional waypoints indicates type of conditional waypoint (ALTITUDE, COURSE INTERCEPT, etc.). Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.41.11...
  • Page 986 (W) MAP CTR, the origin or destination and selected range is 80, 160, 320, or 640 NM. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 10.41.12 D6-27370-866-EGP...
  • Page 987 Displays source of FMC data FMC L annunciation (G) MAP CTR, used by CDS for data FMC R presentation. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 D6-27370-866-EGP 10.41.13...
  • Page 988 MAP CTR, option selected. Mode (C), Tilt VOR, CAL or VAR (C), Tilt Mode (C), Gain (C) Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 10.41.14 D6-27370-866-EGP...
  • Page 989 After the pointer is set with the BARO position, moving the Minimums Reference selector to RADIO displays only the pointer. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 D6-27370-866-EGP 10.41.15...
  • Page 990 Vector as an unfilled dot if the target speed will not be achieved within the vector length. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 10.41.16 D6-27370-866-EGP...
  • Page 991 (M), inactive (W) Waypoint Block Altitude example. NOLLA altitude FL200B FL180A constraint: active (M), inactive (W) Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 D6-27370-866-EGP 10.41.17...
  • Page 992 (R). Terrain status Look-ahead terrain alerting TERR FAIL annunciations and display have failed. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 10.41.18 D6-27370-866-EGP...
  • Page 993 MAP/TERR status MAP CTR display output range disagree RANGE DISAGREE annunciations with selected EFIS control panel range. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 D6-27370-866-EGP 10.41.19...
  • Page 994 CTR, VOR, behind rainfall (radar Compensation (A) shadow) is indicated by amber arc on outer range ring. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 24, 2015 10.41.20 D6-27370-866-EGP...
  • Page 995 ND range. Displayed only if the EFIS control panel TFC switch is selected on. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. March 27, 2014 D6-27370-866-EGP 10.41.21...
  • Page 996 Panel. Shows 3 NM range ring oriented to aircraft heading. Displayed at ranges of 80 NM or less. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 10.41.22 D6-27370-866-EGP...
  • Page 997 Airplane is on a surface other ON TAXIWAY MAP CTR, than a runway and ground VOR, speed is greater than 40 knots. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 25, 2014 D6-27370-866-EGP 10.41.23...
  • Page 998 Flight Instruments, Displays - PFD/ND – Navigation Displays 737 Flight Crew Operations Manual Intentionally Blank Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 25, 2014 10.41.24 D6-27370-866-EGP...
  • Page 999 Displays airplane pitch in five flight, degree increments between AIII -20 ° and +25 °. approach, IMC, Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 15, 2016 D6-27370-866-EGP 10.42.1...
  • Page 1000 PRI in Indicates current heading. flight Drift angle PRI in Indicates current drift angle or pointer flight track. Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details. September 26, 2013 10.42.2 D6-27370-866-EGP...

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