Daher TBM 900 Pilot's Information Manual

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PILOT'S INFORMATION

P/N DMHPIPYEEN - Edition 0 - Revision 6

This information manual is a non-official copy of the pilot's operating

handbook and may be used for general information purposes only.

It is not kept current and therefore cannot be used as a substitute for

airworthiness authorities approved manual which is the only one

The list of effective pages in this manual corresponds to that of the

The content of this document is the property of DAHER AEROSPACE. It is

supplied in confidence and commercial security of its contents must be

It must not be used for any purpose other than that for which it is

supplied, nor may information contained in it be disclosed to

unauthorized persons. It must not be reproduced nor transmitted in any

form in whole or in part without permission in writing from the owners of

Information in this document is subject to change without notice.

DAHER AEROSPACE

Customer Care

65921 TARBES CEDEX 9 - FRANCE

PIM - DO NOT USE FOR FLIGHT OPERATIONS

TBM 900

MANUAL

▲

CAUTION

intended for operation of the airplane.

basic Pilot's Operating Handbook.

▲

maintained.

the Copyright.

▲

Printed in FRANCE

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Page 1 The list of effective pages in this manual corresponds to that of the basic Pilot's Operating Handbook. ▲ The content of this document is the property of DAHER AEROSPACE. It is supplied in confidence and commercial security of its contents must be maintained.
Page 2 Section 0 Pilot's Operating Handbook Table of contents Section General Limitations Emergency procedures Normal procedures Performance Weight and balance Description Airplane handling, servicing and maintenance Supplements Page 0.6 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 3 Section 0 Pilot's Operating Handbook List of effective pages and validities Original issue of October 31, 2013 From S/N 1000 to S/N 1049, plus S/N 687 P/N DMHFM00EE0R6EN Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date Title FEB 20 0.18 DEC 17 0.19 DEC 17...
Page 4 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 2.4.2 DEC 17 1.2.1 DEC 17 1.2.2 DEC 17 2.5.1 DEC 17 2.5.2 DEC 17 1.3.1 FEB 20 1.3.2 DEC 17 2.6.1 DEC 17 1.3.3 DEC 17 2.6.2 FEB 20 1.3.4...
Page 5 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 3.A.1 APR 19 3.6.3 DEC 17 3.A.2 APR 19 3.6.4 DEC 17 3.0.1 APR 19 3.7.1 DEC 17 3.0.2 DEC 17 3.7.2 DEC 17 3.0.3 APR 19 3.7.3 DEC 17 3.0.4...
Page 6 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 3.12.19 DEC 17 3.10.1 DEC 17 3.12.20 APR 19 3.10.2 DEC 17 3.12.21 DEC 17 3.10.3 APR 19 3.12.22 DEC 17 3.10.4 FEB 20 3.12.23 APR 19 3.10.5 FEB 20 3.12.24...
Page 7 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 4.4.3 FEB 20 4.4.46 DEC 17 4.4.4 FEB 20 4.4.47 DEC 17 4.4.5 FEB 20 4.4.48 DEC 17 4.4.6 DEC 17 4.4.49 DEC 17 4.4.7 DEC 17 4.4.50 DEC 17 4.4.8...
Page 8 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 4.5.20 FEB 20 5.8.10 FEB 20 4.5.21 FEB 20 4.5.22 FEB 20 5.9.1 DEC 17 4.5.23 FEB 20 5.9.2 FEB 20 4.5.24 FEB 20 5.9.3 FEB 20 4.5.25 FEB 20 5.9.4...
Page 9 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 5.13.1 FEB 20 6.5.1 APR 19 5.13.2 DEC 17 6.5.2 DEC 17 5.14.1 DEC 17 7.0.1 DEC 17 5.14.2 DEC 17 7.0.2 FEB 20 5.14.3 DEC 17 7.0.3 FEB 20 5.14.4...
Page 10 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 7.3.23 DEC 17 7.5.8 DEC 17 7.3.24 DEC 17 7.5.9 FEB 20 7.3.25 DEC 17 7.5.10 DEC 17 7.3.26 DEC 17 7.5.11 FEB 20 7.3.27 DEC 17 7.5.12 DEC 17 7.3.28...
Page 11 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 7.8.14 APR 19 7.11.2 DEC 17 7.8.15 DEC 17 7.11.3 DEC 17 7.8.16 DEC 17 7.11.4 DEC 17 7.8.17 DEC 17 7.11.5 DEC 17 7.8.18 DEC 17 7.11.6 DEC 17 7.8.19...
Page 12 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 8.6.1 DEC 17 8.6.2 DEC 17 8.6.3 DEC 17 8.6.4 DEC 17 8.6.5 DEC 17 8.6.6 DEC 17 8.7.1 DEC 17 8.7.2 DEC 17 8.7.3 DEC 17 8.7.4 DEC 17 8.7.5...
Page 13: Table Of Contents
Section 1 General Pilot's Operating Handbook Section 1 General Table of contents General ..........1.1.1 Three view drawing .
Page 14: General
Section 1 General Pilot's Operating Handbook Intentionally left blank 1.0.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 15 Section 1 General Pilot's Operating Handbook - General This POH contains 9 sections and includes the material required by FAR Part 23 to be furnished to the pilot for operation of the TBM airplane. It also contains supplemental data supplied by the manufacturer, in accordance with GAMA standard. Section 1 provides basic data and information of general interest.
Page 16 Section 1 General Pilot's Operating Handbook Intentionally left blank Page 1.1.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 17: Three View Drawing
Section 1 General Pilot's Operating Handbook - Three view drawing * Airplane on level field with fully extended FWD shock-absorber Figure 1.2.1 (1/2) - Three view drawing Edition 0 - October 31, 2013 Page 1.2.1 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 18 Section 1 General Pilot's Operating Handbook Figure 1.2.1 (2/2) - Three view drawing Page 1.2.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 19: Descriptive Data
Section 1 General Pilot's Operating Handbook - Descriptive data Engine Number of engines : 1 Engine manufacturer : PRATT & WHITNEY CANADA Engine model number : PT6A - 66D Engine type : Free turbine, reverse flow and 2 turbine sections Compressor type : 4 axial stages, 1 centrifugal stage Combustion chamber type : annular Turbine type : 1 gas generator turbine stage, 2 power turbines stages...
Page 20: Fuel
Section 1 General Pilot's Operating Handbook Fuel Total capacity : 301 USG (1140 litres) Total capacity each tank : 150.5 USG (570 litres) Total usable : 292 USG (1106 litres) CAUTION ▲ ▲ The fuel used must contain an anti-ice additive, in accordance with specification MIL-I-27686 or MIL-I-85470.
Page 21: Engine Oil
Section 1 General Pilot's Operating Handbook Engine oil System total capacity : 12.7 Quarts (12 litres) (oil cooler included) Usable capacity : 6 Quarts (5.7 litres) Maximum oil consumption in 10 hour period : 0.14 qt/hr (0.13 l/hr) [0.3 lb/hr (0.136 cc/hr)] Specification Nominal Specification...
Page 22: Cabin And Entry Dimensions
Section 1 General Pilot's Operating Handbook Cabin and entry dimensions Maximum cabin width : 3 ft 11.64 in (1.21 m) Maximum cabin length : 13 ft 3.45 in (4.05 m) Maximum cabin height : 4 ft (1.22 m) Number of cabin entries : 1 (standard) + 1 pilot door (if installed) Entry width (standard) : 3 ft 6.52 in (1.08 m) Entry height (standard) : 3 ft 10.85 in (1.19 m) Pilot entry mean width : 2 ft 3.6 in (0.70 m)
Page 23: Abbreviations And Terminology
Section 1 General Pilot's Operating Handbook - Abbreviations and terminology Meteorological terminology International standard atmosphere Outside air temperature Static air temperature Atmospheric pressure at the airport reference point. Atmospheric pressure at sea level, at airplane position. ● NOTE ● On the ground, the altimeter will indicate zero if it is set to QFE. It will indicate airport altitude if it is set to QNH.
Page 24: Power Terminology
Section 1 General Pilot's Operating Handbook Maximum Landing Gear Operating Speed is the maximum speed at which the landing gear can be safely extended or retracted. Maximum Operating Speed is the speed limit that may not be deliberately exceeded in normal flight operations. Rotation Speed is the speed at which rotation is initiated during takeoff to achieve takeoff safety speed at screen height.
Page 25: Airplane Performance And Flight Planning Terminology
Section 1 General Pilot's Operating Handbook Shaft Horsepower. Torque. Airplane performance and flight planning terminology Climb gradient : Is the ratio of the change in height during a portion of climb, to the horizontal distance traversed in the same time interval. Demonstrated crosswind velocity : Is the velocity of the crosswind component for which adequate control of the airplane during takeoff and landing was actually...
Page 26: General Abbreviations
Section 1 General Pilot's Operating Handbook Maximum ramp weight : Is the maximum weight approved for ground maneuver. It includes the weight of start, taxi and run up fuel. Maximum takeoff weight : Is the maximum weight approved at the beginning of the takeoff run. Maximum landing weight : Is the maximum weight approved for landing touchdown.
Page 27 Section 1 General Pilot's Operating Handbook EGME : Ethylene glycol monomethyl ether : Engine Indication System EMER : Emergency ESHP : Estimated shaft horsepower ESS. BUS TIE : Essential BUS tie EXT. LIGHTS : Exterior lightings ° F : Fahrenheit degree : Fuel control unit : Flight level : Fuel On Board...
Page 28 Section 1 General Pilot's Operating Handbook : Kilogram : Knot (1 nautical mile/hr - 1852 m/hr) : Kilowatt : Litre L or L.H. : Left : Litre / hour lb or lbs : Pound(s) L / D : Lift-to-drag : Landing LDG GR : Landing gear : Landing Field Elevation...
Page 29 Section 1 General Pilot's Operating Handbook : Maximum Ramp Weight : Message MTOW : Maximum Takeoff Weight MXCR : Maximum Cruise MZFW : Maximum Zero Fuel Weight : Nautical mile NOCR : Normal cruise (recommended) NORM : Normal : Primary Flight Display : Plan Horizontal Fixe (Horizontal stabilizer) PRESS : Pressure...
Page 30: Radio-Navigation Abbreviations
Section 1 General Pilot's Operating Handbook TEMP : Temperature : Takeoff TURN COORD : Turn coordinator : Gallon U.S : Volt or Voltage WARN : Warning W / S : Windshield Radio-navigation abbreviations : Automatic Direction Finder System : Attitude Director Indicator AFCS : Automated Flight Control System AHRS...
Page 31 Section 1 General Pilot's Operating Handbook L NAV : Lateral NAVigation : Localizer Precision Vertical : Marker Radio Beacon : Navigation Indicators or Receivers P RNAV : Precision aRea NAVigation RAIM : Receiver Autonomous Integrity and Monitoring RF Leg : Radius to Fix Leg R NAV : Area NAVigation : Required Navigation Performance...
Page 32 Section 1 General Pilot's Operating Handbook Intentionally left blank Page 1.4.10 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 33: Conversion Factors
Section 1 General Pilot's Operating Handbook - Conversion factors Imperial and U.S units to metric units Metric units to Imperial and U.S units Multiply To obtain Multiply To obtain feet 0.3048 metre metre 3.2808 feet inch 25.4 0.03937 Inch Imp.Gal 4.546 litre litre...
Page 34 Section 1 General Pilot's Operating Handbook feet 31000 30000 20000 10000 metres 2500 5000 7500 10000 Figure 1.5.2 - Feet versus metres Page 1.5.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 35 Section 1 General Pilot's Operating Handbook 1000 Figure 1.5.3 - Inches versus millimetres Edition 0 - October 31, 2013 Page 1.5.3 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 36 Section 1 General Pilot's Operating Handbook 8000 6000 4000 2000 1000 2000 3000 4000 Figure 1.5.4 - Pounds versus kilograms Page 1.5.4 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 37: Pressure And Standard Atmosphere
Section 1 General Pilot's Operating Handbook - Pressure and standard atmosphere Standard atmosphere Pressure Pressure altitude °C °F (hPa) (ft) 1013.2 15.0 59.0 2000 942.1 11.0 51.8 4000 875.0 44.6 6000 811.9 37.6 8000 752.6 30.5 10000 696.8 23.4 12000 644.3 16.2 14000...
Page 38: Pressure Conversion Table
Section 1 General Pilot's Operating Handbook Pressure conversion table ● NOTE ● The standard pressure of 1013.2 hPa is equal to 29.92 inches of mercury. ● 28.05 28.08 28.11 28.14 28.17 28.20 28.23 28.26 28.29 28.32 28.35 28.38 28.41 28.44 28.47 28.50 28.53...
Page 39 Section 2 Pilot's Operating Handbook Limitations EASA Approved Section 2 Limitations Table of contents General ..........2.1.1 Airspeed limitations .
Page 40 Section 2 Limitations Pilot's Operating Handbook EASA Approved Miscellaneous limits ........2.7.1 Seating limits C.G.
Page 41: General
EASA Approved - General TBM 900 is the trade name of the TBM 700 N version airplane (TBM 700 type), which is certified in the normal category. This airplane must be flown in compliance with the limits specified by placards or markings and with those given in this section and throughout the POH.
Page 42 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.1.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 43: Airspeed Limitations
Section 2 Limitations Pilot's Operating Handbook EASA Approved - Airspeed limitations Airspeed limitations and their operational significance are shown in figure 2.2.1. Speed KCAS KIAS Remarks Maximum operating speed Do not intentionally exceed this speed in normal flight category Maneuvering speed Do not make abrupt or full control movements above this speed...
Page 44 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.2.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 45: Powerplant Limitations
Section 2 Limitations Pilot's Operating Handbook EASA Approved - Powerplant limitations Engine Number of engines : 1 Engine manufacturer : PRATT & WHITNEY CANADA Engine model number : PT6A - 66D Maximum power : 100 % at Np = 2000 RPM Ng limitation : 104.1 % Np limitation :...
Page 46: Oil
Section 2 Limitations EASA Approved Pilot's Operating Handbook CAUTION ▲ ▲ Do not mix different viscosities or specifications of oil as their different chemical structure can make them incompatible. ▲ Maximum oil temperature : 104 °C Oil pressure : Minimum : 60 psi Maximum : 135 psi, a transient oil pressure up to 170 psi is acceptable for maximum 20 seconds ●...
Page 47: Fuel
Section 2 Limitations Pilot's Operating Handbook EASA Approved Fuel Fuel limitations : 2 tanks : 150.5 USG (570 litres) each Total fuel : 301 USG (1140 litres) Usable fuel : 292 USG (1106 litres) Unusable fuel : 9 USG (34 litres) Maximum fuel imbalance : 15 USG (57 litres) ●...
Page 48: Propeller
Section 2 Limitations EASA Approved Pilot's Operating Handbook US specification French specification English specification NATO code (US) (FR) (UK) ASTM-D1655 JET A F35 without ASTM-D1655 JET A1 AIR 3405C Grade F35 DERD 2494 Issue 9 additive ASTM-D1655 JET B MIL-DTL-5624 DERD 2454 Issue 4 F40 with AIR 3407B...
Page 49: Starter Operation Limits
Section 2 Limitations Pilot's Operating Handbook EASA Approved - Starter operation limits Starter operation sequence is limited as follows : if Ng < 30 % ..........30 seconds if Ng >...
Page 50 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.4.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 51: Weight And C.g. Limits
Section 2 Limitations Pilot's Operating Handbook EASA Approved - Weight and C.G. limits Weight limits Maximum ramp weight (MRW) : 7430 lbs (3370 kg) Maximum takeoff weight (MTOW) : 7394 lbs (3354 kg) Maximum landing weight (MLW) : 7024 lbs (3186 kg) Maximum zero fuel weight (MZFW) : 6032 lbs (2736 kg) Maximum baggage weight : in FWD compartment (non pressurized) : 110 lbs (50 kg)
Page 52: Limits
Section 2 Limitations EASA Approved Pilot's Operating Handbook C.G. limits Center of gravity range with landing gear down and flaps up, attitude 0° : Forward limits : 181.3 in (4.604 m) aft of datum at 4409 lbs (2000 kg) or less (14 % of m.a.c) 183.6 in (4.664 m) aft of datum at 6250 lbs (2835 kg) (18 % of m.a.c) 185.3 in (4.707 m) aft of datum at 6579 lbs (2984 kg) (20.85 % of m.a.c) 187 in (4.752 m) aft of datum at all weights above 7024 lbs (3186 kg) (23.8 % of m.a.c)
Page 53: Operation Limits
Section 2 Limitations Pilot's Operating Handbook EASA Approved - Operation limits Maneuver limits This airplane is certified in the normal category. The normal category is applicable to airplanes intended for non-aerobatic operations. Non-aerobatic operations include any maneuvers incidental to normal flying, stalls (except whip stalls), lazy eights, chandelles, and steep turns in which the angle of bank is no more than 60°.
Page 54: Generator Limits
Section 2 Limitations EASA Approved Pilot's Operating Handbook Generator limits Generator load must be below 200 A when the airplane is on the ground. GFC 700 autopilot limits During autopilot operation, a pilot with seat belt fastened must be seated at the left or right position.
Page 55 Section 2 Limitations Pilot's Operating Handbook EASA Approved ● NOTE ● Depending on the area of navigation, an operational approval may be required to use the navigation performance that are detailed in the table hereafter. The pilot is responsible to ensure compliance with current operational requirements. ●...
Page 56 Section 2 Limitations EASA Approved Pilot's Operating Handbook ICAO Flight Plan Code Approved Approved Reference Reference Phase of flight Phase of flight Operational limitations Operational limitations Notes Notes Item Item Documents Documents Capability Capability Code PBN/ Domestic, RNP 2 GNSS FDE availability Additional com- Offshore, must be verified prior to...
Page 57 Section 2 Limitations Pilot's Operating Handbook EASA Approved ICAO Flight Plan Code Approved Approved Reference Reference Phase of flight Phase of flight Operational limitations Operational limitations Notes Notes Item Item Documents Documents Capability Capability Code PBN/ Approach At a minimum, the flight EASA RF legs may be APCH...
Page 58: Gnss (Gps/Sbas) Navigation System Limitations
Section 2 Limitations EASA Approved Pilot's Operating Handbook GNSS (GPS/SBAS) navigation system limitations Navigation database limitations The pilot must confirm at system initialization that the Navigation database is current. If the AIRAC cycle will change during flight, the pilot must ensure the accuracy of navigation data, including suitability of navigation facilities used to define the routes and procedures for flight.
Page 59: Icing Conditions
Section 2 Limitations Pilot's Operating Handbook EASA Approved GNSS integrity limitations For flight planning purposes, in areas where SBAS coverage is not available, the pilot must check RAIM availability. The availability of GPS integrity RAIM shall be confirmed for the intended route of flight. In the event of a predicted continuous loss of RAIM of more than five minutes for any part of the intended route of flight, the flight should be delayed, cancelled, or re-routed on a track where RAIM requirements can be met.
Page 60: Severe Icing Conditions
Section 2 Limitations EASA Approved Pilot's Operating Handbook Wing and Tail Leading Edge Pneumatic Deicing Boot System must be activated: At the first sign of ice formation anywhere on the aircraft, and The system must either be continued to be operated in the automatic cycling mode, if available;...
Page 61: Flap Operating Envelope
Section 2 Limitations Pilot's Operating Handbook EASA Approved All wing icing inspection lights must be operative prior to flight into icing conditions at night. ● NOTE ● This supersedes any relief provided by the Master Minimum Equipment List (MMEL). ● Refer to the list of equipment required depending on type of operation in this same chapter.
Page 62 Section 2 Limitations EASA Approved Pilot's Operating Handbook Day VFR Pilot instruments Airspeed indicator Sensitive and adjustable altimeter Magnetic compass with built-in compensator CAS warning and caution messages Oil pressure Low fuel pressure Fuel selector OFF Fuel auxiliary pump ON L.H.
Page 63 Section 2 Limitations Pilot's Operating Handbook EASA Approved Various indicators Fuel gauge indicators (2) Voltmeter Ammeter Outside air temperature Installations Fuel mechanical pump (main) Fuel electrical pump (auxiliary) Fuel shut-off valve Fuel timer Starter generator Inertial separator Stall warning Electrical aileron trim Electrical rudder trim Manual elevator pitch trim Engine ignition...
Page 64 Section 2 Limitations EASA Approved Pilot's Operating Handbook Night VFR All equipment required for day VFR Attitude display indicator Instrument lighting Instrument panel lighting Emergency lighting Vertical speed indicator Navigation lights (4) Anticollision lights (2) Landing light All equipment required for day VFR All equipment required for night VFR, if flight is performed during night Taxi light, if flight is performed during night Clock...
Page 65 Section 2 Limitations Pilot's Operating Handbook EASA Approved Pressurized flight Cabin altimeter Cabin vertical speed indication Cabin differential pressure indication Pressurization control valve Safety valve Pressurization control Maximum cabin altitude and pressure warning light Flight into icing conditions All equipment required for IFR flight Propeller deicing L.H.
Page 66: Altitude Operating Limits
Section 2 Limitations EASA Approved Pilot's Operating Handbook Altitude operating limits Maximum altitude : 31000 ft (9449 m) Maximum differential pressure : 6.2 psi Operation in RVSM area This airplane is approved for operations in Reduced Vertical Separation Minimum (RVSM) airspace when required equipment is maintained in accordance with the airplane maintenance manual - refer to section List of equipment, paragraph List of critical RVSM equipment.
Page 67: Enhanced Mode S
Section 2 Limitations Pilot's Operating Handbook EASA Approved Enhanced mode S The installed mode S system satisfies the data requirements of ICAO Doc 7030/4, regional supplementary procedures for SSR mode S enhanced surveillance in designated european airspace. The capability to transmit data parameters is shown in column 2 : Parameter Available (A) / Not available (NA)
Page 68: Chartview System Operating Limitations
Section 2 Limitations EASA Approved Pilot's Operating Handbook Chartview system operating limitations The geographic-referenced airplane symbol on some charts must not be used for navigation. ● NOTE ● The airplane symbol displayed on some charts provides supplemental airplane situational awareness information. It is not intended as a means for navigation or flight guidance.
Page 69: Miscellaneous Limits
Section 2 Limitations Pilot's Operating Handbook EASA Approved - Miscellaneous limits Seating limits C.G. 2 front seats at 178.5 in (4.534 m) >> With 4-seat accommodation or 6-seat accommodation 2 intermediate seats at 224.8 in (5.710 m) >> With 6-seat accommodation Rear bench (2 seats) at 267.1 in (6.785 m) Baggage limits Baggage in pressurized cabin at 303 in (7.695 m)
Page 70: Cargo Net Installation Limits
Section 2 Limitations EASA Approved Pilot's Operating Handbook Cargo net installation limits Small cargo net : maximum loading height = 28 in (710 mm) Large cargo net : maximum loading height = 22 in (565 mm) in cabin, out of baggage compartment.
Page 71: Markings
Section 2 Limitations Pilot's Operating Handbook EASA Approved - Markings Airspeed indicator on PFD(s) Markings and their color code significance are shown in figure 2.8.1. KIAS Marking Significance (Value or range) Red strip Below 65 White strip 65 - 122 Full flap operating range Lower limit is maximum weight in landing configuration.
Page 72: Pressurization
Section 2 Limitations EASA Approved Pilot's Operating Handbook Pressurization Marking Value Significance Red line 6.2 psi Cabin ∆P limit Figure 2.8.3 - Pressurization marking Page 2.8.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 73: Engine Instruments
Section 2 Limitations Pilot's Operating Handbook EASA Approved Engine instruments Engine instrument markings and their color code significance are shown in figure 2.8.4. Yellow Green line or arc line or arc line or arc Red line Indication -------------- --------------- --------------- --------------- Minimum Caution...
Page 74 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.8.4 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 75: Placards
Section 2 Limitations Pilot's Operating Handbook EASA Approved - Placards Under L.H. front side window Calibration chart on compass and on windshield post Steer Steer DATE : RADIO ON On pressurized baggage compartment partition wall 100 kg - - 220 lbs MAXIMUM IT IS THE PILOT’S RESPONSIBILITY TO CHECK THAT ALL THE BAGGAGES ARE PROPERLY SECURED...
Page 76 Section 2 Limitations EASA Approved Pilot's Operating Handbook (3)a For the small cargo net, on frame C13bis (3)b For the large cargo net, on R.H. side upholstery panel, in the rear baggage compartment (3)c On FWD baggage compartment door frame (non pressurized) 50 kg - - 110 lbs MAXIMUM FOR LOADING INSTRUCTIONS SEE WEIGHT AND BALANCE DATA...
Page 77 Section 2 Limitations Pilot's Operating Handbook EASA Approved On pedestal console On fuel selector Near fuel tank caps Edition 0 - October 31, 2013 Page 2.9.3 Rev. 6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 78 Section 2 Limitations EASA Approved Pilot's Operating Handbook On internal face of L.H. engine cowling Oil system capacity 12 l 12.7 qt On landing gear emergency control access door LDG GEAR EMERGENCY ACCESS PULL Under window, at L.H. Intermediate seat (10) On rear passenger's table casing TABLE MUST BE STOWED DURING TAKEOFF AND LANDING...
Page 79 Section 2 Limitations Pilot's Operating Handbook EASA Approved (11) Under R.H. control wheel (12) On nose gear door (13) On nose gear leg NOSE LANDING GEAR TIRE PRESSURE : 6,5 bar 94 psi Edition 0 - October 31, 2013 Page 2.9.5 Rev.
Page 80 Section 2 Limitations EASA Approved Pilot's Operating Handbook (14) On main gear leg MAIN LANDING GEAR TIRE PRESSURE : 8,96 bar 130 psi (15) On engine cowling, in front of compartment door EXTERNAL POWER 28 VOLTS D.C. NOMINAL 800 AMP STARTING CAPACITY MIN DO NOT EXCEED 1000 AMP (16)
Page 81 Section 2 Limitations Pilot's Operating Handbook EASA Approved (17) On access door - External side (18) On outer fuselage skin aft of access door and in the cabin forward of access door (19) On access door - Internal side Edition 0 - October 31, 2013 Page 2.9.7 Rev.
Page 82 Section 2 Limitations EASA Approved Pilot's Operating Handbook (20) On pilot door - Internal side, if installed (21) On emergency exit handle Marking on cover Marking on handle Page 2.9.8 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 83 Section 2 Limitations Pilot's Operating Handbook EASA Approved (22) On last step of stairs STAIRS MAX LOAD : ONE PERSON (23) On R.H. access door jamb (24) On R.H. side at front seat level and on the first rear passengers masks container (R.H.
Page 84 Section 2 Limitations EASA Approved Pilot's Operating Handbook (26) On internal face of the oxygen cylinder service door (27) On the oxygen service door (28) On emergency locator transmitter inspection door (29) On the potty seat curtain, if installed, on pilot's side CURTAIN MUST BE STOWED FOR TAKE- -OFF AND LANDING Page 2.9.10 Edition 0 - October 31, 2013...
Page 85 Section 2 Limitations Pilot's Operating Handbook EASA Approved >> Airplane equipped with coat hanger (Post-MOD70-0557-25C) (30) On the L.H. rear cargo compartment panel upper edge Edition 0 - October 31, 2013 Page 2.9.11 Rev. 6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 86 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.9.12 Edition 0 - October 31, 2013 Rev. 6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 87 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Section 3 CAS messages Table of contents ● NOTE ● CAS MESSAGES are in alphabetical order by either Chapter, Section, Paragraph or Supplement ● ........3.12.18 AP ON YD OFF AURAL WRN 1 CHNL...
Page 88 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook FUEL LOW L ......... 3.8.4 .
Page 89 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Section 3 Emergency procedures Table of contents General ..........3.1.1 Procedure format .
Page 90 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Fire and smoke ......... 3.5.1 Engine fire on ground .
Page 91 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Electrical system ........3.9.1 ESI-2000 failures .
Page 92: Aural Wrn 1 Chnl
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 3.11 Deicing system ......... 3.11.1 Leading edges deicing failure .
Page 93 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved - General The recommended procedures for different failures or emergency situations are provided in this section. Emergency procedures associated with optional or particular equipment that require pilot's operating handbook supplements are provided in section 9 Supplements. The pilot must know procedures given in this section and be prepared to take appropriate action should an emergency arise.
Page 94 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Both indicators/buttons are located on the upper part of the L.H. instrument panel. When either one lights up, press it once to reactivate. It will go out and is ready to signal in the event of another failure.
Page 95 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Procedure format PROCEDURE TITLES Name of the procedure Procedure introduction or description of symptoms associated with the failure are presented like this at the beginning of the procedure. 1/X is written if the procedure extends over 2 pages or more. MEMORY ITEMS The memory items are indicated with a grey border box as shown hereafter : The memory items are written like this.
Page 96 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Continuation of a procedure on several pages is indicated by : ► Continuing Continue ► LANDING DIRECTIVES ► Land as soon as possible ◄ means land on the nearest suitable runway. ►...
Page 97 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved - Rejected takeoff Engine failure at takeoff before rotation THROTTLE ..........Flight IDLE Brakes .
Page 98 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Rejected takeoff for any other reason THROTTLE ..........Flight IDLE Reverse .
Page 99 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved - Engine failures Engine failure before rotation Perform procedure ....Engine failure at takeoff before rotation Refer to chapter 3.2 End of procedure.
Page 100 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Engine failure after rotation ► Continuing FUEL TANK SELECTOR ......Before touch down : FLAPS lever .
Page 101 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Engine failure in flight Symptoms : Loss of power ► Fly the airplane ◄ FUEL TANK SELECTOR ......Switch tanks AUX BP switch .
Page 102 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook OIL PRESS OIL PRESS Indicates that oil pressure is below 100 psi. ► Fly the airplane ◄ ► Land as soon as possible ◄ Oil pressure ..........Monitor .
Page 103 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Engine regulation discrepancy, power loss, throttle control loss Symptoms : power fluctuations, or uncommanded power loss, or bad response to THROTTLE movements. ► Fly the airplane ◄ If circumstances and obtained minimum power allow : CAUTION ▲...
Page 104 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Engine regulation discrepancy, power loss, throttle control loss ► Continuing CAUTION ▲ ▲ When MAN OVRD control is used, the available power may not be sufficient to ensure a go-around in landing configuration, particularly if the weight is near the maximum weight.
Page 105 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Engine regulation discrepancy, power loss, throttle control loss ► Continuing When runway is assured : 17 - THROTTLE ........CUT OFF 18 - FLAPS lever...
Page 106 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Governor control not operating ► Fly the airplane ◄ Continue the flight. If Np < 1960 RPM : ► Do not perform a go around ◄ ► Do not use the reverse ◄ In that case, the go-around performance and the reverse efficiency might be lower than expected.
Page 107 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Engine does not stop on ground If the engine does not stop when the THROTTLE is set to CUT OFF : FUEL TANK SELECTOR ....... . Wait for engine stop due to lack of fuel in the pipes.
Page 108 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook During engine start : Starting procedure ........Abort Refer to procedure Engine start, chapter 4.4 Cancel the flight.
Page 109 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved CHIP Indicates that metallic chips have been detected in the engine oil. In flight : ► Fly the airplane ◄ ► Land as soon as practical ◄ Inform maintenance department. End of procedure ■ On ground : ►...
Page 110 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook OIL TEMP Indicates that oil temperature is below 0°C or above 104°C (possibly with OIL PRESS Oil temperature indicator ........Check If the indicated temperature is in the green sector : ►...
Page 111 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved - Air start Air start envelope ● NOTE ● Air start may be attempted outside of the envelope. However, above 20000 ft or at lower speeds, ITT tends to increase during start and prudence is recommended.
Page 112 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Air start procedures Oxygen masks ..........▲...
Page 113 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Air start procedures ► Continuing When Ng > 50 % : 14 - Starter ....... . Check OFF automatically If starter has not turned off automatically : 15 -...
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Page 115: Fire And Smoke
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved - Fire and smoke Engine fire on ground Symptoms : ITT increasing, , smoke, ... THROTTLE ..........CUT OFF BLEED switch .
Page 116: Cabin Fire On Ground
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Cabin fire on ground THROTTLE ..........CUT OFF Brakes .
Page 117: Engine Fire In Flight
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Engine fire in flight Symptoms : ITT increasing, , smoke, ... WARNING ▲ ▲ No air start attempt after an engine fire. ▲ ► Fly the airplane ◄ Oxygen masks ..........THROTTLE .
Page 118: Cabin Electrical Fire Or Smoke During Flight
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Cabin electrical fire or smoke during flight ► Fly the airplane ◄ Oxygen masks and goggles ........If the origin is known : Defective equipment breaker .
Page 119: Smoke Elimination
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Smoke elimination Oxygen masks and goggles ........BLEED switch .
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Page 121: Emergency Descents
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook - Emergency descents Emergency descents profiles Edition 0 - October 31, 2013 Page 3.6.1 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 122: Maximum Rate Descent
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Maximum rate descent THROTTLE ..........Flight IDLE Oxygen masks .
Page 123: Maximum Range Descent
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Maximum range descent Oxygen masks ..........THROTTLE .
Page 124 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Maximum range descent ► Continuing If icing conditions : 20 - PITOT L HTR switch ....... . 21 - WINDSHIELD switch .
Page 125: Emergency Landings, Flaps, Gear
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved - Emergency landings, flaps, gear Forced landing THROTTLE ..........CUT OFF FUEL TANK SELECTOR .
Page 126: Tire Blowout During Landing
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Tire blowout during landing Control direction with brakes and nose wheel steering. Reverse ..........As required Stop airplane to minimize damages.
Page 127: Flaps Asym
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved FLAPS ASYM Indicates a dissymmetry of flap deflection. This immediately stops the flap motor and prevents further operation of the flaps. ► Fly the airplane ◄ FLAPS breaker ..........Pull FLAPS lever .
Page 128: Flaps Malfunction
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Flaps malfunction In case of blockage of flaps or inoperative flaps control lever between UP and LDG positions, without FLAPS ASYM FLAPS breaker ..........Pull FLAPS lever .
Page 129: Landing Gear Retraction Discrepancy
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Landing gear retraction discrepancy ● NOTE ● Symptoms have to be considered at the end of the sequence. ● Symptoms : GEAR UNSAFE CAS msg and GEAR UNSAFE red warning light are ON, or - amber light flashing and 3 green lights are OFF.
Page 130: Landing Gear Extension Discrepancy
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Landing gear extension discrepancy ● NOTE ● Symptoms have to be considered at the end of the sequence. ● Symptoms : GEAR UNSAFE CAS msg and GEAR UNSAFE red warning light are ON, or - amber light flashing and 0 to 3 green lights are OFF.
Page 131: Emergency Gear Extension
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Emergency gear extension ● NOTE ● Follow this procedure in case of any doubt about the gear extension. ● CAUTION ▲ ▲ Do not enter icing conditions. This could adversely increase drag and weight due to ice accumulation, and lock wheels and struts.
Page 132 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Emergency gear extension ► Continuing If : - GEAR UNSAFE red warning light is OFF and GEAR UNSAFE is OFF and - 3 green lights are ON : Exit and / or remain outside icing conditions. Continue flight at airspeed <...
Page 133 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Emergency gear extension ► Continuing If : - emergency pump remains soft or - one (or more) green light(s) is(are) not ON and / or flickering while pressing the CHECK DOWN push-button : A gear unlock condition is confirmed.
Page 134: Landing With Unlocked Main Landing Gear
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Landing with unlocked main landing gear ▲ CAUTION ▲ If one main landing gear is not down, it is recommended to land with landing gear up - refer to procedure Landing with gear up in the following procedures.
Page 135 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Landing with unlocked main landing gear ► Continuing If landing gear drags during landing : 11 - THROTTLE ........CUT OFF 12 - Crash lever...
Page 136: Landing With Defective Nose Landing Gear (Down Unlocked Or Not Down)
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Landing with defective nose landing gear (down unlocked or not down) Ask ATC or another airplane to visually check landing gear position. If necessary : Transfer passengers to the rear. Perform a normal approach. FLAPS lever .
Page 137: Landing With Gear Up
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Landing with gear up Do a standard final approach. FLAPS lever ..........Airspeed .
Page 138: Ditching
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Ditching ▲ CAUTION ▲ In heavy swell with light wind, land parallel to the swell (rollers). In heavy wind, land facing wind. ▲ LANDING GEAR lever ......... . . FLAPS lever .
Page 139: Landing Without Elevator Control
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Landing without elevator control LANDING GEAR lever ......... . FLAPS lever .
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Page 141: Aux Boost Pmp On
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved - Fuel system FUEL PRESS Indicates a fuel pressure drop at HP engine pump inlet. ► Fly the airplane ◄ Remaining fuel ..........Check FUEL TANK SELECTOR .
Page 142 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook FUEL PRESS ► Continuing FUEL PRESS remains ON : Fullest tank ....... . Select Avoid high power and rapid movements of the THROTTLE.
Page 143 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved AUX BOOST PMP ON Indicates the auxiliary booster pump is running. ► Fly the airplane ◄ If AUX BP switch is in ON position : Indication is normal. End of procedure ■ If AUX BP switch is in AUTO position : Reset AUX BP switch to .
Page 144: Fuel Low L-R
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook FUEL LOW L-R Indicates a level drop in the corresponding tank. Corresponding gage ........Check Check the other tank has been automatically selected.
Page 145: Auto Sel
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved AUTO SEL Indicates that there is no more automatic control mode running. ► Fly the airplane ◄ FUEL SEL switch ........Check AUTO If FUEL SEL switch already on AUTO : Failure is...
Page 146: Fuel Imbalance
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook FUEL IMBALANCE Indicates that fuel tanks are imbalanced by more than 15 USG for more than 30 seconds. If FUEL SEL switch is on AUTO : Fullest tank ......... . . Select By pressing the SHIFT push-button If FUEL SEL switch is on MAN :...
Page 147 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved LOW LVL FAIL L-R Indicates a failure of fuel low level sensor. Remaining fuel in tanks ........Check Take decision.
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Page 149 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved - Electrical system ESI-2000 failures Battery indicator symbol meaning Battery Description indicator Not shown Normal operation - No information needs to be conveyed Green More than one hour of operation remains Amber Less than one hour of operation remains Battery is not available to power unit : overtemperature...
Page 150 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook ESI-2000 failures ► Continuing If in visual meteorological conditions : Cycle power on ESI-2000, including internal power. Maintain straight and level while unit aligns. If red ”X” reappears : Remain clear of IMC. End of procedure ■...
Page 151: Bat Amp
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved BAT AMP Indicates that battery current is over 50 A while on ground. After starting the engine with airplane power, a battery charge over 50 amperes is normal. CAUTION ▲ ▲ Do not take off if battery charge is over 50 A.
Page 152 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook MAIN GEN Indicates that GENERATOR selector has been positioned to OFF or ST-BY, or main generator is cut off. GENERATOR selector ......Check / Correct If necessary If warning persists :...
Page 153 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved LOW VOLTAGE Normal functioning with GENERATOR selector on MAIN. Voltmeter voltages ......... .
Page 154 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook MAIN GEN LOW VOLTAGE With GENERATOR selector on ST-BY (after MAIN generator failure), functioning on ST-BY generator. GENERATOR selector ........MAIN MAIN GENERATOR RESET push-button .
Page 155 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved MAIN GEN LOW VOLTAGE ► Continuing GENERATOR selector ......If altitude >...
Page 156 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook MAIN GEN LOW VOLTAGE ► Continuing PITOT R & STALL HTR ....OFF/LDG/TAXI light .
Page 157 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved ELEC FEATH FAULT Indicates a propeller feathering system malfunction. ► Fly the airplane ◄ FEATHER breaker ..........Pull ►...
Page 158 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Bus bar Figure 3.9.1 (1/3) - Electrical distribution of bus bars Page 3.9.10 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 159 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Bus bar Figure 3.9.1 (2/3) - Electrical distribution of bus bars Edition 0 - October 31, 2013 Page 3.9.11 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 160 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Bus bar Figure 3.9.1 (3/3) - Electrical distribution of bus bars Page 3.9.12 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 161 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Total loss of electrical power CAUTION ▲ ▲ If no ESI-2000 key is pressed, the ESI-2000 will shut down automatically within 5 minutes. ▲ Maintain airplane control. ESI-2000 ......Press any key within 5 minutes To enable the use of ESI-2000 internal battery Use the ESI-2000 for...
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Page 163: Bleed Temp
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 3.10 - Pressurization and air conditioning BLEED TEMP Indicates overheat of bleed air system. Normally this leads to BLEED cut-off and to BLEED OFF appearance. ► Fly the airplane ◄ Should automatic cut-off occur or not : If possible : .
Page 164 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook BLEED OFF Possibly due to : system malfunction BLEED switch on OFF / RST position If in flight : Oxygen masks ......... BLEED switch .
Page 165 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved CPCS BACKUP MODE Indicates a GASC system malfunction. The GASC cannot compute optimal cabin altitude and is automatically set to 9800 ft default value as cabin altitude reference. ► Fly the airplane ◄ Continue the flight.
Page 166: Cabin Altitude (Pre-Mod70-0407-00D)
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook >> Without v15.11 GARMIN software (Pre-MOD70-0407-00D) CABIN ALTITUDE Indicates a cabin altitude over 10000 ft ± 500 ft. Pressurization indicator ........Check If cabin altitude >...
Page 167: Cabin Altitude And Use Oxygen Mask
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved >> With v15.11 GARMIN software (Post-MOD70-0407-00D) CABIN ALTITUDE USE OXYGEN MASK ● NOTE ● CABIN ALTITUDE is followed by USE OXYGEN MASK and 3 voice alerts “Use oxygen mask / Use oxygen mask”. ●...
Page 168 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook >> With v15.11 GARMIN software (Post-MOD70-0407-00D) and without EDM evolution patch (Pre-MOD70-0657-34) CABIN ALTITUDE USE OXYGEN MASK ● NOTE ● CABIN ALTITUDE is followed by USE OXYGEN MASK and 3 voice alerts “Use oxygen mask / Use oxygen mask”.
Page 169 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved >> With EDM evolution patch (Post-MOD70-0657-34) ● NOTE ● may come on 45 s after CABIN ALTITUDE USE OXYGEN MASK EDM makes a 90° left heading change and descent to 15000 ft. EDM override is possible by pressing twice the AP / TRIM DISC push-button, and other AP modes are usable.
Page 170 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook >> With v15.11 GARMIN software (Post-MOD70-0407-00D) EDM OVERRIDE Indicates that Emergency Descent Mode has been overridden by the crew, and is not available again until EDM OVERRIDE is OFF. ► Fly the airplane ◄ End of procedure.
Page 171: Cabin Diff Press
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved CABIN DIFF PRESS Indicates a cabin pressure differential over 6.4 PSI ± 0.2 PSI. Pressurization indicator ........Check If ΔP >...
Page 172 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Cabin not depressurized after landing If ΔP cabin remains > 0 : DUMP switch ......... Actuate BLEED switch .
Page 173 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved OXYGEN Indicates that the oxygen cylinder isolation valve is closed. WARNING ▲ ▲ Flight is prohibited with oxygen cylinder closed. ▲ Oxygen cylinder ..........Open End of procedure.
Page 174 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook DOOR Indicates that one of the door latches of the door(s) is not correctly locked. On ground : Check the correct locking, as well as the latches position of the door(s). DOOR is still ON : Do not take off.
Page 175 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved VACUUM LOW Low vacuum may lead to malfunctioning of leading edge deicing and pressurization. Monitor the normal functioning of leading edge deicing and pressurization. If necessary : Altitude ........Below 10000 ft Return to VMC conditions as soon as possible.
Page 176 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Defog malfunction If moisture starts to quickly cover the inside of the windscreen with the HOT AIR FLOW distributor already turned to the left : HOT AIR FLOW distributor ......Set to around a 10 o’clock position If moisture continues :...
Page 177: Deicing System
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 3.11 - Deicing system Leading edges deicing failure Symptoms : failure on one of the two pneumatic deicing pulses : ice on wing outboard sections, or, ice on wing inboard sections and stabilizers, one of the two cycling green lights is not lit.
Page 178: Prop Deice Fail
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook PROP DEICE FAIL Symptoms : propeller deicing green light is not lit, propeller vibrations............Reduce ►...
Page 179: Inert Sep Fail
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved INERT SEP FAIL Symptoms : INERT SEP ON does not appear within 50 seconds following INERT SEP switch setting ON, inertial separator is not retracted after 50 seconds following INERT SEP switch setting OFF, INERT DE ICE breaker triggered.
Page 180: Windshield Deicing Failure
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Windshield deicing failure Symptoms : windshield being covered uniformly by ice, no perception of heat when touching deiced section, windshield deicing green light is not lit. If symptoms result from overheat : WINDSHIELD switch .
Page 181: Windshield Misting Or Internal Icing
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Windshield misting or internal icing Symptoms : mist or ice on windshield internal face. TEMP/°C selector ......Set to 12 o’clock position HOT AIR FLOW distributor .
Page 182: Pitot No Ht L-R
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook PITOT NO HT L-R Indicates that : - corresponding pitot tube heating has failed or - PITOT L HTR switch or PITOT R & STALL HTR switch is not ON while the engine is running.
Page 183: Stall No Heat
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved STALL NO HEAT Indicates that : - stall warning vane heating has failed or - PITOT R & STALL HTR switch is not ON while the engine is running. Correct operation of the aural stall warning may be altered by severe or prolonged icing.
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Page 185: Miscellaneous
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 3.12 - Miscellaneous Trim Runaway ► Fly the airplane ◄ AP / TRIM DISC push-button ......Press and hold The three trim tabs are disconnected and runaway stops.
Page 186: Crack In Cockpit Window Or Window Panel
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Crack in cockpit window or window panel ► Fly the airplane ◄ Descend slowly. Cabin ∆P ..........Reduce By setting Landing Field Elevation to 10000 ft End of procedure.
Page 187: Emergency Exit Use
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Emergency exit use Check that the anti-theft safety pin has been removed. >> Pre-MOD70-0793-25 Remove the upholstery panel of the emergency exit. Pull it firmly through the access area to the opening handle. Refer to paragraph Emergency exit in chapter 7.3 >>...
Page 188 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Emergency exit use Check that the anti-theft safety pin has been removed. Lift up the opening handle. Pull emergency exit assembly towards oneself to release it from its recess. Put the emergency exit door inside fuselage or throw it away from the fuselage through the opening.
Page 189: Emergency Beacon (Elt) Use
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Emergency beacon (ELT) use Before a forced landing : If possible : Transmit a MAY DAY signal on COM VHF 121.5 MHz or on a known ATC frequency. After landing : ELT remote control switch .
Page 190: Inadvertent Spins
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Inadvertent spins WARNING ▲ ▲ Voluntary spins are prohibited. ▲ Control wheel ..........Neutral Pitch and roll axis Rudder...
Page 191: Stall Warning Sound
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Stall warning sound AP / TRIM DISC push-button ......Press twice Fly the airplane, wings levelled and nose down until stall warning stops.
Page 192 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved >> With v15.11 GARMIN software and voice alerts (Post-MOD70-0407-00D) : AURAL WRN FAIL Indicates that no aural warning alerts are available. CAUTION ▲ ▲ No aural stall warning. No aural overspeed warning. No landing gear warning.
Page 193 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook >> With v15.11 GARMIN software and voice alerts (Post-MOD70-0407-00D) : AURAL WRN 1 CHNL Indicates that one aural warning alerts channel is not available. Both sides GMA's SPKR button ....... . . Press SPKR led ON on available GMA(s) Volume...
Page 194: Oxygen Use (Pre-Mod70-0407-00D)
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved >> Without v15.11 GARMIN software (Pre-MOD70-0407-00D) : Oxygen use WARNING ▲ ▲ Smoking is strictly prohibited any time oxygen system is used. Before using oxygen, remove any trace of oil, grease, soap and other fatty substances (including lipstick, make-up, etc...).
Page 195: Oxygen Use (Post-Mod70-0407-00D)
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook >> Without v15.11 GARMIN software (Pre-MOD70-0407-00D) : Oxygen use ► Continuing For rear passengers : Take a mask. Uncoil tube totally. Pull on the lanyard cord to take out the lanyard pin. Put the mask onto the face.
Page 196 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved >> With v15.11 GARMIN software (Post-MOD70-0407-00D) : Oxygen use With or without USE OXYGEN MASK WARNING ▲ ▲ Smoking is strictly prohibited any time oxygen system is used. Before using oxygen, remove any trace of oil, grease, soap and other fatty substances (including lipstick, make-up, etc...).
Page 197 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook >> With v15.11 GARMIN software (Post-MOD70-0407-00D) : Oxygen use ► Continuing For rear passengers : Take a mask. Uncoil tube totally. Pull on the lanyard cord to take out the lanyard pin. Put the mask onto the face.
Page 198: Airspeed Indicating System Failure
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Airspeed indicating system failure Symptoms : erroneous indication in flight. PITOT L HTR switch ........Check ON PITOT R &...
Page 199: Flight Into Severe Icing Conditions
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Flight into severe icing conditions Severe icing conditions, particularly freezing rain and freezing drizzle, can be identified by : unusually extensive ice accumulation on the airframe and windshield in areas not normally observed to collect ice, accumulation of ice on the upper surface of the wing aft of the protected area.
Page 200: Front Cargo Door
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved FRONT CARGO DOOR Indicates that front cargo door is open. On ground : Check and close the door. In flight : ► Fly the airplane ◄ Airspeed ..........Reduce To minimum available ►...
Page 201: Gpu Door
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook GPU DOOR Indicates that GPU door is open. On ground : Check and close the door. In flight : ► Fly the airplane ◄ Airspeed ..........Reduce To minimum available ►...
Page 202: Ignition
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved IGNITION Indicates that ignition exciter is running. IGNITION switch ........Check position If weather permits : IGNITION switch...
Page 203: Ap On Yd Off
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook AP ON YD OFF Indicates that the autopilot is ON while Yaw Damper is OFF, so no automatic rudder trim is available. Yaw Damper status ......... . Check If necessary : Yaw Damper status...
Page 204: Autopilot Or Electric Pitch Trim Malfunction
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Autopilot or electric pitch trim malfunction ▲ CAUTION ▲ When disconnecting the autopilot after a pitch trim malfunction, hold the control wheel firmly. Up to 30 pounds of force on the control wheel may be necessary to hold the airplane level.
Page 205 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Dual GPS/SBAS failure annunciation on HSI) LOSS OF GPS/SBAS NAVIGATION DATA When both GPS/SBAS receivers are inoperative or GPS navigation information is not available or invalid, the GARMIN system will enter one of two modes : Dead Reckoning mode (DR) or Loss Of Integrity mode (LOI).
Page 206: Dual Gps/Sbas Failure Dr Or Loi Annunciation On Hsi)
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Dual GPS/SBAS failure annunciation on HSI) ► Continuing If no Alternate Navigation Sources are available : Dead Reckoning (DR) Mode - Active when the airplane is greater than 30 NM from the destination airport : Navigation .
Page 207: Gps Approach Alarm Limits Exceeded
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook GPS approach alarm limits exceeded During a GPS LPV, LNAV/VNAV, or LNAV+V approach, if the Horizontal or Vertical alarm limits are exceeded, the GARMIN System will downgrade the approach. This will be annunciated in the ALERTS window and by an annunciation change on the HSI from LPV, L/VNAV, or LNAV+V to LNAV.
Page 208: Left Pfd Failure
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Left PFD failure ► Fly the airplane ◄ At takeoff : Fly the airplane manually ... . . Using stand-by instruments AP / TRIM DISC push-button .
Page 209: Ahrs Failure
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook AHRS failure Symptoms : Autopilot is disconnected On PFD(s) : Comparator window HDG NO COMP and/or PIT NO COMP and/or ROL NO COMP annunciation(s) On PFD(s) : Reversionary sensor window BOTH ON AHRS1 BOTH ON AHRS2 annunciation Lost systems :...
Page 210 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved AHRS failure ► Continuing annunciations HDG NO COMP PIT NO COMP ROL NO COMP go off , refer to following condition. BOTH ON AHRS1 BOTH ON AHRS2 annunciation not associated to and/or and/or HDG NO COMP...
Page 211: Adc Failure
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook ADC failure Symptoms : On PFD(s) : Comparator window IAS NO COMP and/or ALT NO COMP annunciation(s) On PFD(s) : Reversionary sensor window BOTH ON ADC1 BOTH ON ADC2 annunciation Lost systems : ADC1 or ADC2 Actions : Autopilot is still operative.
Page 212: Mfd Failure
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved MFD failure Lost system : Actions : L.H. DISPLAY BACKUP button ....... . . Press MFD breaker .
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Page 214 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Section 4 Normal procedures Table of contents General ..........4.1.1 Airspeeds for normal operation .
Page 215 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before taxiing ......... . . 4.4.37 Taxiing .
Page 216: General
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved - General This section provides procedures for the conduct of normal operation of TBM airplane. The first part of this section lists the normal procedures required as a check list. The amplified procedures are developed in the second part of the section. The normal procedures for optional systems are given in section 9, Supplements of the POH.
Page 217 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 4.1.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 218: Airspeeds For Normal Operation
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved - Airspeeds for normal operation Conditions : Takeoff weight : 7394 lbs (3354 kg) Landing weight : 7024 lbs (3186 kg) Rotation airspeed (V Flaps TO ..........90 KIAS Best rate of climb speed (V Landing gear and flaps UP...
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Page 220: Check-List Procedures
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved - Check-list procedures Initial inside inspection and outside inspection performed. OXYGEN cylinder open. Inside inspection Cabin door and pilot door, if installed ....Closed / Locked Baggage .
Page 221 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Inside inspection ► Continuing 21 - LANDING GEAR ..........22 - MAN OVRD .
Page 222: Before Starting Engine
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before starting engine Crash lever ........... . ATIS .
Page 223: Motoring (If Residual Itt > 150°C)
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Motoring (if residual ITT > 150°C) IGNITION ........... . . AUX BP .
Page 224: Engine Start
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Engine start ▲ CAUTION ▲ After aborted engine starts, wait : 1 min / 5 min / 30 min before 2 new engine start. ▲ IGNITION ........... AUTO AUX BP .
Page 225: After Engine Start With Gpu
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook After engine start with GPU SOURCE ........... . BATT .
Page 226: Before Taxiing
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before taxiing Stand-by instruments ......... Check DE ICE SYSTEM .
Page 227: Before Line Up
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before line up LDG lights ............
Page 228: Normal Takeoff
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Normal takeoff ADI, HSI, headings ......... . . Check PROP RPM .
Page 229: Short Takeoff
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Short takeoff ADI, HSI, headings ......... . . Check PROP RPM .
Page 230: After Takeoff
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved After takeoff LANDING GEAR ......... Check UP FLAPS .
Page 231: Climb
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Climb ALT SEL ........... Check Altimeters setting .
Page 232: Cruise
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Cruise Altimeters setting ..........Check Autopilot .
Page 233: Before Descent
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before descent Briefing before approach ........Completed Altimeters setting .
Page 234: Approach
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Approach Altimeters setting (QNH) ........Set / Check Minimums .
Page 235: Final Approach (In Gs) Or Downwind Leg (Vmc)
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Final approach (in GS) or downwind leg (VMC) LDG lights ........... . . LANDING GEAR .
Page 236: Short Final (≈ 500 Ft)
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Short final (≈ 500 ft) LANDING GEAR ..........Check DN and 3 green FLAPS...
Page 237: Runway Clear
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Runway clear TAXI light ............
Page 238: Shutdown
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Shutdown 1 - PARK BRAKE ..........Set / ON 2 - EXT LIGHTS .
Page 239 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 4.3.20 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 240: Amplified Procedures
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved - Amplified procedures Preflight inspection 1/16 The preflight inspection procedure is based on a scanning method. It is divided in 6 subparts to cover all items of the preflight - see figure 4.4.1 Initial inside inspection Cabin L.H.
Page 241 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 2/16 ► Continuing WARNING ▲ ▲ Remove tie-downs. Refer to section 8 for quantities, products and specifications of products and materials currently used. ▲ Figure 4.4.1 - Preflight inspection Continue ►...
Page 242 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 3/16 ► Continuing Initial inside inspection Cockpit CAUTION ▲ ▲ When engine is shut down, do not set the PROP DE ICE switch to ON for more than 10 seconds, damage to the propeller blades could result. ▲...
Page 243 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 4/16 ► Continuing Open door of emergency landing compartment to check LANDING GEAR emergency control. 11 - Lever ..........Pushed down 12 - By-pass selector...
Page 244 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 5/16 ► Continuing 25 - STARTER switch ........●...
Page 245 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 6/16 ► Continuing If BATT source : 40 - Voltage ........Check >...
Page 246 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 7/16 ► Continuing Reentering the airplane 48 - EXT LIGHTS panel ......... All OFF 49 - HORN TEST push-button...
Page 247 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 8/16 ► Continuing 60 - PITOT L HTR switch ........61 - PITOT R &...
Page 248 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 9/16 ► Continuing Cabin 63 - Cabin fire extinguisher ......Pressure / Attachment 64 - Seats / belts...
Page 249 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 10/16 ► Continuing When the airplane is stored for extended periods of time, a thorough preflight inspection is recommended. Particular attention should be paid to possible blockages in airspeed sensing lines, foreign objects in engine intake and exhaust stubs and water contamination of the fuel system.
Page 250 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 11/16 ► Continuing 80 - Left pitot ..........Condition 81 - Wing lower surface...
Page 251 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 12/16 ► Continuing ● NOTE ● If airplane has been used from muddy airfields or in snow, check wheel wells to make sure they are clean and not obstructed. Check frequently all landing gear retraction mechanism components, shock-absorbers, tires and brakes.
Page 252 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 13/16 ► Continuing ● NOTE ● Inspect if possible pressure port located inside exhaust stub. A missing port or a cracked port may hinder correct operation of continuous heating of air inlet lip. ●...
Page 253 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 14/16 ► Continuing 103 - Propeller and spinner ..No nicks, cracks or oil leaks / Attachment ● NOTE ● In case of operation from contaminated runways, it is necessary to carefully examine propeller blades, where traces of abrasion may be found.
Page 254 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 15/16 ► Continuing R.H. main LANDING GEAR 110 - Shock absorber ........Check 111 - Doors .
Page 255 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 16/16 ► Continuing 129 - ELT door ......... . . Closed / Locked ●...
Page 256: Inside Inspection
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Inside inspection After completion of preflight inspection. Initial inside inspection and outside inspection performed. Cabin door and pilot door, if installed ....Closed / Locked Baggage .
Page 257 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Inside inspection ► Continuing 10 - PASSENGER OXYGEN switch ........11 - OXYGEN switch .
Page 258 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Inside inspection ► Continuing 22 - IGNITION switch ..........AUTO ●...
Page 259 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Inside inspection ► Continuing CAUTION ▲ ▲ Make sure that MAN OVRD control is backward to avoid overtemperature risks at start. ▲ 37 - MAN OVRD control ......Full backward (notched) CAUTION ▲...
Page 260: Before Starting Engine
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before starting engine Check that the weight and balance are within the correct limits. Brief passengers about use of seat belts and the emergency oxygen system, as well as opening the access door and the emergency exit.
Page 261 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before starting engine ► Continuing 15 - OXYGEN ..........Check OFF OXYGEN is ON :...
Page 262 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before starting engine ► Continuing ● NOTE ● PARK BRAKE appearance does not indicate that parking brake is set. For that, press on brake pedals before turning brake selector to the right. ●...
Page 263: Engine Start
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Engine start STROBE switch ..........G1000 .
Page 264 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Engine start ► Continuing ▲ CAUTION ▲ When THROTTLE is positioned on LO-IDLE before having obtained 13 % of Ng, there is a risk of overtemperature further to an excessive accumulation of fuel inside the combustion chamber before ignition. ▲...
Page 265 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Engine start ► Continuing When Ng > 50 % and, 1 minute max : CAUTION ▲ ▲ If the starter does not go off automatically, disengage it using the ABORT position of the STARTER switch. ▲...
Page 266: Motoring
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Motoring To drain fuel accumulated inside the combustion chamber, a motoring procedure is required following an aborted start. A 15-second dry motoring run is sufficient to clear any fuel pooled in the engine. The fuel is removed in liquid or vapor form, through an airflow intended to dry combustion chamber, turbines and exhaust nozzles.
Page 267 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Motoring ► Continuing FUEL PRESS ........Check OFF Fuel pressure is necessary for lubrication of HP pump.
Page 268 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Motoring ► Continuing 23 - STARTER switch ........ABORT Then OFF 24 -...
Page 269: Motoring Followed By An Engine Start
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Motoring followed by an engine start Amplified procedures stated in starting engine sequences using airplane power or with GPU are also to be applied to hereunder procedure. Within starter operating limits (continuous max. 1 minute), it is possible to initiate a starting procedure from a motoring procedure.
Page 270 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Motoring followed by an engine start ► Continuing 13 - Motor ..........For 30 sec.
Page 271 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Motoring followed by an engine start ► Continuing Fuel panel 24 - AUX BP switch ........AUTO 25 - AUX BOOST PMP ON...
Page 272: After Engine Start With Gpu
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved After engine start with GPU SOURCE selector ..........BATT Electrical network .
Page 273: After Engine Start
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook After engine start ▲ CAUTION ▲ Generator load < 200 amps ▲ THROTTLE ........LO-IDLE Flight IDLE .
Page 274 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved After engine start ► Continuing 17 - Oxygen ........... . Check Verify quantity available for the planned flight.
Page 275: In-Flight Available Oxygen Quantity
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook In-flight available oxygen quantity Oxygen pressure ..........Read Outside air temperature (OAT) .
Page 276: Before Taxiing
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before taxiing Stand-by instruments ......... Check Check de-ice system ●...
Page 277 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before taxiing ► Continuing ......... . . Increase >...
Page 278 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before taxiing ► Continuing 15 - Pitch trim ..........UP / DN 16 - Pitch trim...
Page 279 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before taxiing ► Continuing ▲ CAUTION ▲ During feathering test, keep the spent time with the propeller RPM in the caution (yellow) range at a minimum. ▲ 31 - THROTTLE ......... FEATHER twice Flight IDLE to LO-IDLE then Flight IDLE, twice 32 -...
Page 280: Taxiing
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Taxiing ▲ CAUTION ▲ Generator load < 200 amps. ▲ ▲ CAUTION ▲ Avoid using reverse during taxiing. ▲ ● NOTE ● Operation in the Beta (β) range / reverse is not restricted during ground operations.
Page 281: Before Line Up
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before line up CAUTION ▲ ▲ Generator load < 200 amps. ▲ PARK BRAKE ..........PARK BRAKE .
Page 282 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before line up ► Continuing Adjust trims for takeoff 17 - Pitch ........... . Adjust inside green index sector, depending on the current balance condition 18 -...
Page 283 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before line up ► Continuing ▲ CAUTION ▲ Do not take off if battery charge > 50 amps ± 4 amps. ▲ ● NOTE ● After starting engine with airplane power, a battery charge above 50 amps is normal.
Page 284 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before line up ► Continuing 41 - Rotation airspeed (V ........Check 42 - Pilot's / Passengers' belts...
Page 285: Normal Takeoff
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Normal takeoff When lined up, on brakes : ▲ CAUTION ▲ If heavy precipitation, turn IGNITION and INERT SEP switches to ON. If icing conditions are foreseen, refer to chapter 4.5, paragraph Flight into known icing conditions.
Page 286 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Normal takeoff ► Continuing 11 - Rotation airspeed 12 - Attitude ........... . 10°...
Page 287: Short Takeoff
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Short takeoff When lined up, on brakes : ▲ CAUTION ▲ If heavy precipitation, turn IGNITION and INERT SEP switches to ON. If icing conditions are foreseen, refer to chapter 4.5, paragraph Flight into known icing conditions.
Page 288 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Short takeoff ► Continuing 10 - Brakes ........... . Release ●...
Page 289 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Short takeoff ► Continuing In case of initial climb at Vx : WARNING ▲ ▲ It is recommended not to retract FLAPS to UP before 500 ft AGL. ▲ 17 - Airspeed .
Page 290: After Takeoff
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved After takeoff LANDING GEAR lever ........Check UP FLAPS lever .
Page 291: Climb
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Climb ALT SEL ........... Check Altimeters setting .
Page 292 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Climb ► Continuing ECS panel TEMP/°C selector ..........Adjust 10 - FUEL gages...
Page 293: Cruise
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Cruise Altimeters setting ..........Check Autopilot .
Page 294 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Cruise ► Continuing When the cruise parameters are stabilized, after 4 min minimum : 12 - AMPS / VOLTS ........Check CAUTION ▲...
Page 295: Before Descent
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before descent Briefing before approach ........Completed Altimeters settings .
Page 296: Approach
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Approach Altimeters settings (QNH) ....... . . Set / Check Minimums .
Page 297: Final Approach (In Gs) Or Downwind Leg (Vmc)
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Final approach (in GS) or downwind leg (VMC) Long final : Altimeters ........... Check FUEL gages .
Page 298: Short Final (≈ 500 Ft)
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Short final (≈ 500 ft) Stabilized approach LANDING GEAR lever ........Check DN and 3 green When airspeed is below 122 KIAS :...
Page 299: Landing
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Landing WARNING ▲ ▲ Reduce power smoothly. Quickly reducing the power to idle during the flare may induce a pronounced deceleration which may lead to a drop down of the airplane. ▲...
Page 300: Go-Around
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Go-around GO AROUND push-button ........Press It provides the moving up of the flight director to + 10°...
Page 301 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Go-around ► Continuing When airspeed is at or above 115 KIAS : FLAPS lever ........10 - Climb airspeed .
Page 302: Touch And Go
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Touch and go Before wheels touch : WARNING ▲ ▲ Reduce power smoothly. Quickly reducing the power to idle during the flare may induce a pronounced deceleration which may lead to a drop down of the airplane.
Page 303 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Touch and go ► Continuing WARNING ▲ ▲ Check that flaps have well reached the TO position before increasing power. Do not increase power with full flaps, as airplane may lift off prematurely at low speed. ▲...
Page 304: Runway Clear
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Runway clear Runway clear - airplane stopped ▲ CAUTION ▲ Generator load < 200 amps ▲ TAXI lights ........... . . NAV switch .
Page 305: Shutdown
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Shutdown PARK BRAKE ..........Set ON PARK BRAKE .
Page 306 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Shutdown ► Continuing 16 - AUX BP switch ..........17 - GENERATOR selector .
Page 307: Outside Check After Shutdown
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Outside check after shutdown Oxygen cylinder (R.H. Karman) ....... . . Close ●...
Page 308: Particular Procedures
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved - Particular procedures ● NOTE ● The procedures and procedure elements given in this chapter Particular procedures supplement the normal procedures or complete certain elements of the normal procedures described in chapter(s) 4.3 and/or 4.4. ●...
Page 309 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Flight into known icing conditions ► Continuing Windshield electrical deice system. Inertial separator. Description of deice systems is presented in chapter 7.13. Ice accumulation thickness is monitored by the pilot on the L.H. wing leading edge. At night, a leading edge icing inspection light located on the fuselage L.H.
Page 310 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Flight into known icing conditions ► Continuing INERT SEP ON ........Check ON AIRFRAME DE ICE switch .
Page 311 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Flight into known icing conditions ► Continuing 12 - WINDSHIELD switch ........●...
Page 312 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Flight into known icing conditions ► Continuing Ice accumulation effects When ice has accumulated on the unprotected surfaces of the airplane, aerodynamic characteristics may be changed. Particularly stall airspeeds may increase by up to : FLAPS UP 20 KIAS FLAPS TO...
Page 313: Flight Into Severe Icing Conditions
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Flight into severe icing conditions The following weather conditions may be conducive to severe in-flight icing : Visible rain at temperatures below 0°C ambient air temperature, Droplets that splash or splatter on impact at temperatures below 0°C ambient air temperature.
Page 314: Flight Under Heavy Precipitations
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Flight under heavy precipitations IGNITION switch ..........●...
Page 315: Utilization On Runways Covered With Melting Or Not Tamped Snow
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization on runways covered with melting or not tamped snow If required : Refer to paragraph Utilization by cold weather and very cold weather. CAUTION ▲ ▲ When engine is shut down, do not set the PROP DE ICE switch to ON for more than 10 seconds, damage to the propeller blades could result.
Page 316 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization on runways covered with melting or not tamped snow ► Continuing Rotation airspeed ..... Increased by 5 KIAS ●...
Page 317 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization on runways covered with melting or not tamped snow ► Continuing Touch and Go : WARNING ▲ ▲ Touch and Go is prohibited ▲ On the ramp, after landing or taxiing : 18 - Do not use the parking brake to prevent brake lock.
Page 318: Utilization On Icy Or Covered With Tamped Snow Runways 1/2
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization on icy or covered with tamped snow runways 1/2 If required : Refer to paragraph Utilization by cold weather and very cold weather. CAUTION ▲ ▲ When engine is shut down, do not set the PROP DE ICE switch to ON for more than 10 seconds, damage to the propeller blades could result.
Page 319 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization on icy or covered with tamped snow runways 2/2 ► Continuing Takeoff : 11 - After takeoff, normally retract the landing gear, then perform a complete cycle (extension / retraction) at IAS < 150 KIAS. Before landing : 12 - IGNITION switch...
Page 320 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) ● NOTE ● The procedure hereafter supplements the normal procedures for the airplane use when operating under temperatures between 0°...
Page 321 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 1 ● NOTE ● The procedure hereafter supplements the normal procedures for the airplane use when operating in the Envelope 1 defined in figure 4.5.1.
Page 322 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 1 ► Continuing 12 - PITOT L HTR switch ....... . 13 - PITOT R &...
Page 323 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 1 ► Continuing 22 - PARK BRAKE ........Check OFF ●...
Page 324 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 2 ● NOTE ● The procedures hereafter supplement or replace the normal procedures for the airplane use when operating in the Envelope 2 defined in figure 4.5.1.
Page 325 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 2 ► Continuing 11 - IGNITION switch ......ON during 30 seconds 12 - IGNITION...
Page 326: Utilization By Cold Weather (- 0°C To - 25°C) And Very Cold Weather (- 25°C To - 40°C)
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 2 ► Continuing CAUTION ▲ ▲ When the engine is shut down, the THROTTLE must not be moved into the reverse area.
Page 327: Utilization By Cold Weather (- 0°C To - 25°C) And Very Cold Weather (- 25°C To - 40°C) - Envelope 2
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 2 ► Continuing When Ng > 50% : CAUTION ▲ ▲ If the starter does not go off automatically, disengage it using the ABORT position of the STARTER switch.
Page 328: Utilization By Cold Weather (- 0°C To - 25°C) And Very Cold Weather (- 25°C To - 40°C) - Envelope 3
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 2 ► Continuing After engine start : As soon as the current flow is lower than 100 A : ECS panel 46 - BLEED switch...
Page 329 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 3 ● NOTE ● The procedures defined for the Envelope 2 are also applicable for the Envelope 3.
Page 330 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 3 ► Continuing ● NOTE ● If landing is foreseen by cold or very cold weather, or in case of prolonged operation of the airplane in such conditions, it is recommended to prepare the airplane as specified in chapter 8.10.
Page 331: Landing Procedure With Strong Headwind Or Crosswind 1/2
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Landing procedure with strong headwind or crosswind 1/2 If landing must be performed with strong headwind or crosswind : Increase approach airspeed by the greatest of these 2 following values : ( wind down 10 ) −...
Page 332 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Landing procedure with strong headwind or crosswind 2/2 ► Continuing Before touch-down : Generate a slideslip with the rudder in order to align fuselage with the runway (ie left crosswind, left wing low). Immediately after landing : CAUTION ▲...
Page 333: Utilization On Grass Runway
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization on grass runway CAUTION ▲ ▲ The small wheels of the airplane and its weight may lead it to sink in soaked or soft ground. ▲ Before planning the landing, ensure that the field is hard, smooth and dry enough. Landing and moreover takeoff shall not begin if any doubt exists about the condition of such a runway.
Page 334 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization on grass runway ► Continuing ● NOTE ● Under 40 KIAS, using the reverse makes a cloud of solid particles (dusts, sand, gravels, cut grass, ...) appear around the front face of the airplane. This will damage the propeller and, after ingestion, the engine internal components (compressor and turbine blades).
Page 335: Gps Navigation
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook GPS navigation Set up conditions Verify if the data base is current. Verify that altitude data is valid for the GPS prior to flight. Check the systems availability requirements in the table 2.6.1 in section 2 / GNSS (GPS/SBAS) navigation equipment approvals, depending on the planned navigation performance.
Page 336 Section 5 Performance Pilot's Operating Handbook Section 5 Performance Table of contents General ..........5.1.1 Noise level .
Page 337 Section 5 Performance Pilot's Operating Handbook 5.10 Climb performance ........5.10.1 MXCL - Speeds (IAS = 124 KIAS) .
Page 338 Section 5 Performance Pilot's Operating Handbook EASA Approved - General This section provides all of the required and additional performance data for airplane operations. The section 9, Supplements of the POH, provides specific airplane performance associated with optional equipment and systems. Edition 0 - October 31, 2013 Page 5.1.1 Rev.
Page 339 Section 5 Performance EASA Approved Pilot's Operating Handbook Intentionally left blank Page 5.1.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 340: Noise Level
Section 5 Performance Pilot's Operating Handbook EASA Approved - Noise level Maximum noise level Demonstrated noise permitted level FAR PART 36, 88 dB(A) 76.4 dB(A) Appendix G - Amdt 28 ICAO, Annex 16, Vol. 1, 6th edition, Amdt 8 85 dB(A) 76.4 dB(A) Chapter 10, Appendix 6 Approved noise levels for TBM airplane are stated in EASA.A.010 Type Certificate...
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Page 342: Airspeed Calibration
Section 5 Performance Pilot's Operating Handbook EASA Approved - Airspeed calibration ● NOTE ● Indicated airspeeds (IAS) : instrument error supposed to be null (power configuration for cruise condition flight). ● Flaps UP Flaps TO Flaps LDG LDG GR UP LDG GR DN LDG GR DN KIAS...
Page 343 Section 5 Performance EASA Approved Pilot's Operating Handbook Flaps UP Flaps TO Flaps LDG LDG GR UP LDG GR DN LDG GR DN KIAS KCAS KIAS KCAS KIAS KCAS MPH IAS MPH CAS MPH IAS MPH CAS MPH IAS MPH CAS Figure 5.3.2 - Alternate static source (Bleed auto) Page 5.3.2 Edition 0 - October 31, 2013...
Page 344: Cabin Pressurization Envelope
Section 5 Performance Pilot's Operating Handbook - Cabin pressurization envelope ● NOTE ● The cabin pressurization envelope below characterizes the cabin altitude that could be sustained by the fuselage at different flight levels. The curve shows the minimum cabin altitude as a function of flight level, corresponding to the maximum differential pressure.
Page 345 Section 5 Performance Pilot's Operating Handbook Intentionally left blank Page 5.4.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 346: Sat - Oat Conversions
Section 5 Performance Pilot's Operating Handbook - SAT - OAT conversions ● NOTE ● These indicated temperatures are available for stabilized cruise at normal operating power. ● ISA - 20°C ISA - 10°C ISA + 10°C ISA + 20°C Pressure altitude (feet) - 05...
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Page 348: Stall Speeds
Section 5 Performance Pilot's Operating Handbook EASA Approved - Stall speeds Config. Bank Flight Airplane 0° 30° 45° 60° idle weight Flaps KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS 4850 lbs (2200 kg) 5512 lbs (2500 kg) 6579 lbs (2984 kg) 7394 lbs (3354 kg)
Page 349 Section 5 Performance Pilot's Operating Handbook Intentionally left blank Page 5.6.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 350: Wind Components
Section 5 Performance Pilot's Operating Handbook - Wind components Example : Angle between wind direction and flight path 50 ° Headwind 8 kts Crosswind 10 kts Wind speed 13 kts Figure 5.7.1 - Wind components Edition 0 - October 31, 2013 Page 5.7.1 Rev.
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Page 352: Engine Operation
Section 5 Performance Pilot's Operating Handbook - Engine operation The following tables or/and the optimum torque indicator must be used during normal operation of the airplane. ▲ CAUTION ▲ It is the responsibility of the operator to make sure that the required version of GARMIN system software is installed prior to using the hereafter engine operation tables.
Page 353 Section 5 Performance Pilot's Operating Handbook Example, for conditions : FL = 260 OAT = - 22°C the following tables give the maximum torque to be set. Maximum climb power TRQ setting = 82 % for IAS = 124 KIAS (Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed), cf.
Page 354: Maximum Climb Power (Fl < 200) - 124 Kias
Section 5 Performance Pilot's Operating Handbook Maximum climb power (FL < 200) - 124 KIAS Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 355 Section 5 Performance Pilot's Operating Handbook Maximum climb power (FL > 200) - 124 KIAS Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 356: Maximum Climb Power (Fl < 200) - 170 Kias / M 0.40
Section 5 Performance Pilot's Operating Handbook Maximum climb power (FL < 200) - 170 KIAS / M 0.40 Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 357: Maximum Climb Power (Fl > 200) - 170 Kias / M 0.40
Section 5 Performance Pilot's Operating Handbook Maximum climb power (FL > 200) - 170 KIAS / M 0.40 Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 358: Maximum Cruise Power (Fl < 200)
Section 5 Performance Pilot's Operating Handbook Maximum cruise power (FL < 200) Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Use preferably recommended cruise power. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 359 Section 5 Performance Pilot's Operating Handbook Maximum cruise power (FL > 200) Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Use preferably recommended cruise power. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 360: Normal (Recommended) Cruise Power (Fl < 200)
Section 5 Performance Pilot's Operating Handbook Normal (recommended) cruise power (FL < 200) Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Table not valid if INERT SEP ON and/or BLEED HI msg ON. T°...
Page 361: Normal (Recommended) Cruise Power (Fl > 200)
Section 5 Performance Pilot's Operating Handbook Normal (recommended) cruise power (FL > 200) Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Table not valid if INERT SEP ON and/or BLEED HI msg ON. T°...
Page 362: Takeoff Distances
Section 5 Performance Pilot's Operating Handbook EASA Approved - Takeoff distances The following tables give the takeoff distances for several weight configurations. All common information applicable to tables (pages 5.9.2 to 5.9.4) are listed below. Associated conditions Landing gear DN and flaps TO TRQ = 100 % BLEED switch on AUTO Hard, dry and level runway...
Page 363 Section 5 Performance EASA Approved Pilot's Operating Handbook Weight : 5512 lbs (2500 kg) Associated condition : 15° of attitude after rotation Rotation speed choice (V Weight : 5512 lbs (2500 kg) At 50 ft = 91 KIAS - 105 MPH IAS ISA - 35°C ISA - 20°C ISA - 10°C...
Page 364 Section 5 Performance Pilot's Operating Handbook EASA Approved Weight : 6579 lbs (2984 kg) Associated condition 15° of attitude after rotation Rotation speed choice (V Weight : 6579 lbs (2984 kg) At 50 ft = 94 KIAS - 108 MPH IAS ISA - 35°C ISA - 20°C ISA - 10°C...
Page 365 Section 5 Performance EASA Approved Pilot's Operating Handbook Weight : 7394 lbs (3354 kg) Associated condition 12°5 of attitude after rotation Rotation speed choice (V Weight : 7394 lbs (3354 kg) At 50 ft = 99 KIAS - 114 MPH IAS ISA - 35°C ISA - 20°C ISA - 10°C...
Page 366: Climb Performance
Section 5 Performance Pilot's Operating Handbook 5.10 - Climb performance MXCL - Speeds (IAS = 124 KIAS) Conditions : Maximum climb power TRQ = 100 % Landing gear and flaps UP IAS = 124 KIAS - BLEED switch on AUTO and BLEED HI msg OFF Rate of climb (ft/min) Pressure Airplane...
Page 367: Mxcl - Speeds (Ias = 170 Kias / M 0.40)
Section 5 Performance Pilot's Operating Handbook MXCL - Speeds (IAS = 170 KIAS / M 0.40) Conditions : Maximum climb power TRQ = 100 % Landing gear and flaps UP IAS = 170 KIAS / M 0.40 BLEED switch on AUTO and BLEED HI msg OFF Rate of climb (ft/min) Pressure Airplane...
Page 368 Section 5 Performance Pilot's Operating Handbook MXCL - Time, consumption and climb distance (IAS = 124 KIAS) Conditions : ISA - 20°C Maximum climb power Landing gear and flaps UP IAS = 124 KIAS - BLEED switch on AUTO ● NOTE ● : Time, consumption and distance from the 50 ft If BLEED HI msg ON, reduce TRQ by 5 %.
Page 369 Section 5 Performance Pilot's Operating Handbook MXCL - Time, consumption and climb distance (IAS = 124 KIAS) Conditions : Maximum climb power Landing gear and flaps UP IAS = 124 KIAS - BLEED switch on AUTO ● NOTE ● : Time, consumption and distance from the 50 ft If BLEED HI msg ON, reduce TRQ by 5 %.
Page 370 Section 5 Performance Pilot's Operating Handbook MXCL - Time, consumption and climb distance (IAS = 124 KIAS) Conditions : ISA + 20°C Maximum climb power Landing gear and flaps UP IAS = 124 KIAS - BLEED switch on AUTO ● NOTE ● : Time, consumption and distance from the 50 ft If BLEED HI msg ON, reduce TRQ by 5 %.
Page 371: Mxcl - Time, Consumption And Climb Distance (Ias = 124 Kias)
Section 5 Performance Pilot's Operating Handbook MXCL - Time, consumption and climb distance (IAS = 170 KIAS / M 0.40) Conditions : ISA - 20°C Maximum climb power Landing gear and flaps UP IAS = 170 KIAS / M 0.40 - BLEED switch on AUTO ●...
Page 372 Section 5 Performance Pilot's Operating Handbook MXCL - Time, consumption and climb distance (IAS = 170 KIAS / M 0.40) Conditions : Maximum climb power Landing gear and flaps UP IAS = 170 KIAS / M 0.40 - BLEED switch on AUTO ●...
Page 373 Section 5 Performance Pilot's Operating Handbook MXCL - Time, consumption and climb distance (IAS = 170 KIAS / M 0.40) Conditions : ISA + 20°C Maximum climb power Landing gear and flaps UP IAS = 170 KIAS / M 0.40 - BLEED switch on AUTO ●...
Page 374: Climb Performance After Go-Around
Section 5 Performance Pilot's Operating Handbook Climb performance after go-around Conditions : Landing gear DN and flaps LDG IAS = 90 KIAS Rate of climb (ft/min) Pressure Airplane altitude weight (feet) - 35°C - 20°C - 10°C + 10°C + 20°C + 30°C 1635 1610...
Page 375: Climb Performance - Flaps To
Section 5 Performance Pilot's Operating Handbook Climb performance - Flaps TO Conditions : Landing gear UP and flaps TO IAS = 110 KIAS Rate of climb (ft/min) Pressure Airplane altitude weight (feet) - 35°C - 20°C - 10°C + 10°C + 20°C + 30°C 2295...
Page 376: Cruise Performance
Section 5 Performance Pilot's Operating Handbook 5.11 - Cruise performance Maximum cruise 7100 lbs 6300 lbs Figure 5.11.1 - Cruise performance (Maximum cruise) Edition 0 - October 31, 2013 Page 5.11.1 Rev. 6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 377 Section 5 Performance Pilot's Operating Handbook Maximum cruise Conditions : ISA - 20°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power. If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 5 KIAS.
Page 378 Section 5 Performance Pilot's Operating Handbook Maximum cruise Conditions : ISA - 10°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power. If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 6 KIAS.
Page 379 Section 5 Performance Pilot's Operating Handbook Maximum cruise Conditions : ISA - 5°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power. If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 6 KIAS.
Page 380 Section 5 Performance Pilot's Operating Handbook Maximum cruise Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power. If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 6 KIAS.
Page 381 Section 5 Performance Pilot's Operating Handbook Maximum cruise Conditions : ISA + 5°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power. If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 5 KIAS.
Page 382 Section 5 Performance Pilot's Operating Handbook Maximum cruise Conditions : ISA + 10°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power. If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 5 KIAS.
Page 383 Section 5 Performance Pilot's Operating Handbook Maximum cruise Conditions : ISA + 20°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power. If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 6 KIAS.
Page 384: Normal Cruise (Recommended)
Section 5 Performance Pilot's Operating Handbook Normal cruise (Recommended) 7100 lbs 6300 lbs Figure 5.11.9 - Cruise performance (Recommended cruise) Edition 0 - October 31, 2013 Page 5.11.9 Rev. 6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 385 Section 5 Performance Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA - 20°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 6 KIAS.
Page 386 Section 5 Performance Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA - 10°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 5 KIAS.
Page 387 Section 5 Performance Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA - 5°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 5 KIAS.
Page 388 Section 5 Performance Pilot's Operating Handbook Normal cruise (Recommended) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 5 KIAS.
Page 389 Section 5 Performance Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA + 5°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 5 KIAS.
Page 390 Section 5 Performance Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA + 10°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 6 KIAS.
Page 391 Section 5 Performance Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA + 20°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON, reduce TRQ by 5 %. This TRQ reduction will result in an airspeed reduction of up to 6 KIAS.
Page 392: Long Range Cruise (5500 Lbs - 2495 Kg)
Section 5 Performance Pilot's Operating Handbook Long range cruise (5500 lbs - 2495 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure altitude...
Page 393 Section 5 Performance Pilot's Operating Handbook Long range cruise (5500 lbs - 2495 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure altitude...
Page 394: Long Range Cruise (6300 Lbs - 2858 Kg)
Section 5 Performance Pilot's Operating Handbook Long range cruise (6300 lbs - 2858 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure altitude...
Page 395 Section 5 Performance Pilot's Operating Handbook Long range cruise (6300 lbs - 2858 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure altitude...
Page 396: Long Range Cruise (7100 Lbs - 3220 Kg)
Section 5 Performance Pilot's Operating Handbook Long range cruise (7100 lbs - 3220 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure altitude...
Page 397 Section 5 Performance Pilot's Operating Handbook Long range cruise (7100 lbs - 3220 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure altitude...
Page 398: Time, Consumption And Descent Distance
Section 5 Performance Pilot's Operating Handbook 5.12 - Time, consumption and descent distance Conditions : Power as required to maintain constant Vz Landing gear and flaps UP CAS = 230 KCAS - BLEED switch on AUTO Vz = 1500 ft/min Vz = 2000 ft/min Vz = 2500 ft/min Pressure...
Page 399 Section 5 Performance Pilot's Operating Handbook Intentionally left blank Page 5.12.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 400: Holding Time
Section 5 Performance Pilot's Operating Handbook 5.13 - Holding time Conditions : Landing gear and flaps UP IAS = 120 KIAS - BLEED switch on AUTO TRQ ≈ 26 % Fuel used during holding time Pressure Weight 5500 lbs (2495 kg) Weight 6300 lbs (2858 kg) altitude 10 min...
Page 401 Section 5 Performance Pilot's Operating Handbook Intentionally left blank Page 5.13.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 402: Landing Distances
Section 5 Performance Pilot's Operating Handbook EASA Approved 5.14 - Landing distances The following tables give the landing distances for several weight configurations. All common information applicable to tables (pages 5.14.2 to 5.14.4) are listed below. Associated conditions Landing gear DN and flaps LDG Maximum breaking without reverse Hard, dry and level runway In table headings :...
Page 403: Weight : 7024 Lbs (3186 Kg)
Section 5 Performance EASA Approved Pilot's Operating Handbook Weight : 7024 lbs (3186 kg) Associated conditions Approach speed IAS = 85 KIAS Touch-down speed IAS = 78 KIAS ISA - 35°C ISA - 20°C ISA - 10°C Pressure altitude ft 1575 2135 1675...
Page 404: Weight : 6250 Lbs (2835 Kg)
Section 5 Performance Pilot's Operating Handbook EASA Approved Weight : 6250 lbs (2835 kg) Associated conditions Approach speed IAS = 80 KIAS Touch-down speed IAS = 65 KIAS ISA - 35°C ISA - 20°C ISA - 10°C Pressure altitude ft 1050 1900 1115...
Page 405: Weight : 5071 Lbs (2300 Kg)
Section 5 Performance EASA Approved Pilot's Operating Handbook Weight : 5071 lbs (2300 kg) Associated conditions Approach speed IAS = 80 KIAS Touch-down speed IAS = 60 KIAS ISA - 35°C ISA - 20°C ISA - 10°C Pressure altitude ft 1900 2000 1000...
Page 406 Section 6 Weight and balance Pilot's Operating Handbook Section 6 Weight and balance Table of contents General ..........6.1.1 Airplane weighing procedures .
Page 407 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.0.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 408: General
Section 6 Weight and balance Pilot's Operating Handbook - General This section is intended to provide the pilot with the procedure to determine the weight and balance of the airplane. WARNING ▲ ▲ It is the pilot's responsibility to ensure that the airplane is properly loaded and the weight and balance limits are adhered to.
Page 409 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.1.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 410: Airplane Weighing Procedures
Section 6 Weight and balance Pilot's Operating Handbook - Airplane weighing procedures Refer to maintenance manual for the procedures to use. ● NOTE ● Weighing carried out at the factory takes into account all equipment installed on the airplane. The list of this equipment and the total weight is noted in the individual inspection record.
Page 411 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.2.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 412: Baggage Loading
Section 6 Weight and balance Pilot's Operating Handbook - Baggage loading There are two baggage compartments : one in fuselage non pressurized forward section, between firewall and cockpit with maximum baggage capacity of 110 lbs (50 kg), one located in the rear of the pressurized cabin with following characteristics : >>...
Page 413 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.3.1 - Baggage limits Authorized anchoring points are identified with green self-adhesive labels affixed to the inside of the rail. A placard indicates loading limits for each securing net. Evenly distribute the load within the cargo zone and ensure that overall weight is centered.
Page 414 Section 6 Weight and balance Pilot's Operating Handbook >> All WARNING ▲ ▲ It is the pilot's responsibility to check that all parcels and baggages are properly secured in the cabin. Transport of dangerous product is normally prohibited, however if transport of such product is necessary, it must be performed in compliance with regulations concerning transport of dangerous product and any other applicable regulation.
Page 415 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.3.4 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 416: Determining Weight And Balance
Section 6 Weight and balance Pilot's Operating Handbook - Determining weight and balance General This section is intended to provide the pilot with the procedure to determine the weight and balance of the airplane. WARNING ▲ ▲ It is the pilot's responsibility to ensure that the airplane is properly loaded and that the weight and balance limits are adhered to.
Page 417 Section 6 Weight and balance Pilot's Operating Handbook Compute ramp weight (7a) and moment (7b) as sum of zero fuel weight (3a) loaded fuel (6a) and moments (3b) (6b). Check value (7a) to be below maximum ramp weight. Compute ramp weight arm and CG (MAC %) (9c) using given formulas.
Page 418: Airplane Loading Form (M, Kg)
Section 6 Weight and balance Pilot's Operating Handbook Airplane loading form (m, kg) ( Arm (m) − 4.392 ) CG (MAC %) = × 100 Moment = Weight x Arm 1.51 Weight Moment Item (kg) (m.kg) (MAC %) (1a) (1b) (1c) Empty weight (kg)
Page 419 Section 6 Weight and balance Pilot's Operating Handbook Weight Item (kg) (1a) Empty weight Baggage (2a) (< 50 kg) (2a) Front seats -17 kg per seat (2a) removed Inter. seats (2a) -24 kg per seat (2a) removed Rear (2a) bench/net (2a) Cargo (<...
Page 420: Example Of Airplane Weight And Balance Report
Section 6 Weight and balance Pilot's Operating Handbook Example of airplane weight and balance report ● NOTE ● Airplane original report shall be kept with airplane POH. ● Figure 6.4.1 - Example of weight and balance report and basic airplane characteristics, in kg and m Edition 0 - October 31, 2013 Page 6.4.5...
Page 421 Section 6 Weight and balance Pilot's Operating Handbook ● NOTE ● Airplane original report shall be kept with airplane POH. ● Figure 6.4.2 - Example of weight and balance report and basic airplane characteristics, in lb and in Page 6.4.6 Edition 0 - October 31, 2013 Rev.
Page 422: Weight And Balance Form And Diagram (M, Kg)
Section 6 Weight and balance Pilot's Operating Handbook Weight and balance form and diagram (m, kg) ( Arm (m) − 4.392 ) CG (MAC %) = × 100 Moment = Weight x Arm 1.51 Weight Moment Item (kg) (m.kg) (MAC %) Empty weight (kg) Baggage...
Page 423 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.3 - Weight and balance diagram Page 6.4.8 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 424: Weight And Balance Form And Diagram (In, Lbs)
Section 6 Weight and balance Pilot's Operating Handbook Weight and balance form and diagram (in, lbs) ( Arm (in) − 172.93 ) CG (MAC %) = × 100 Moment = Weight x Arm 59.45 Weight Moment Item (lbs) (in) (in.lbs) (MAC %) Empty weight (lbs)
Page 425 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.4 - Weight and balance diagram Page 6.4.10 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 426: Weight And Balance Samples (M, Kg)
Section 6 Weight and balance Pilot's Operating Handbook Weight and balance samples (m, kg) ▲ CAUTION ▲ Loading samples - see figure 6.4.5 or 6.4.6 - are only given as an example ; for calculation concerning your airplane, refer to the diagram corresponding to its validity.
Page 427 Section 6 Weight and balance Pilot's Operating Handbook ( Arm (m) − 4.392 ) CG (MAC %) = × 100 Moment = Weight x Arm 1.51 Weight Moment Item (kg) (m.kg) (MAC %) Empty weight (kg) 2 126 4.738 10 073 22.9 Baggage (<...
Page 428 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.5 - Loading sample (in kg and m) Edition 0 - October 31, 2013 Page 6.4.13 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 429: Weight And Balance Samples (In, Lbs)
Section 6 Weight and balance Pilot's Operating Handbook Weight and balance samples (in, lbs) ▲ CAUTION ▲ Loading samples - see figure 6.4.5 or 6.4.6 - are only given as an example ; for calculation concerning your airplane, refer to the diagram corresponding to its validity.
Page 430 Section 6 Weight and balance Pilot's Operating Handbook ( Arm (in) − 172.93 ) CG (MAC %) = × 100 Moment = Weight x Arm 59.45 Weight Moment Item (lbs) (in) (in.lbs) (MAC %) Empty weight (lbs) 4 638 186.3 864 173 22.6 Baggage...
Page 431 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.6 - Loading samples (in lbs and in) Page 6.4.16 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 432: Determining Empty Airplane Characteristics
Section 6 Weight and balance Pilot's Operating Handbook Determining empty airplane characteristics Empty airplane characteristics (weight and balance) may vary with regard to those indicated on weighing form according to installed optional equipment and installed seats. List of equipment (refer to chapter 6.5) contains the standard and optional equipment, as well as their characteristics (weight, arm), except those listed in this Chapter.
Page 433 Section 6 Weight and balance Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 10 - Parking, mooring, storage and return to service Board kit 0406-10 - Blanking caps bag 8.27 128.00 (3.75)
Page 434 Section 6 Weight and balance Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 0207-00 Carpet 35.27 211.42 (16.000) (5.370) - Cabin furnishings 302.45 211.42 (137.19) (5.370) Leather seats - L.H.
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Page 436: List Of Equipment
Section 6 Weight and balance Pilot's Operating Handbook - List of equipment list equipment available manufacturer Report reference NAV No.34/90--RJ--App 2, located at the end of this POH. A separate list of equipment of items installed at the factory in your specific airplane is provided in your airplane file.
Page 437 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.5.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 438 Section 7 Description Pilot's Operating Handbook Section 7 Description Table of contents General ..........7.1.1 Airframe .
Page 439 Section 7 Description Pilot's Operating Handbook Powerplant ..........7.6.1 Turboprop engine operation .
Page 440 Section 7 Description Pilot's Operating Handbook 7.10 Emergency oxygen system ....... 7.10.1 Flight above 15000 ft with possible emergency descent .
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Page 442: General
Section 7 Description Pilot's Operating Handbook - General This section provides description and operation of the airplane and its systems. Some of the equipment described herein is optional and may not be installed in the airplane. Complete description and operation of the GARMIN integrated flight deck are detailed in the GARMIN Pilot's Guide.
Page 443 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.1.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 444: Airframe
Section 7 Description Pilot's Operating Handbook - Airframe - see figures 7.2.1, 7.2.1A and 7.2.1B This airplane is a six-place, low wing airplane. The airplane can be changed into 2, 3, 4 or 5-seat accommodation. The structure is a semi-monocoque all-metal construction and is equipped with a retractable tricycle landing gear.
Page 445 Section 7 Description Pilot's Operating Handbook Figure 7.2.1 - Cabin arrangement 6-seat accommodation Page 7.2.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 446 Section 7 Description Pilot's Operating Handbook Figure 7.2.1A - Cabin arrangement 4-seat accommodation with large securing net Edition 0 - October 31, 2013 Page 7.2.3 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 447 Section 7 Description Pilot's Operating Handbook Figure 7.2.1B - Cabin arrangement 4-seat accommodation with small securing net Page 7.2.4 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 448: Wings
Section 7 Description Pilot's Operating Handbook Wings The wings are monocoque, bi-spar structures. Main spars of each wing are linked to the fuselage by two integral attach fittings. Each wing contains a main landing gear well and sealed casings forming the fuel tank. The wing leading edge is equipped with a deicing system.
Page 449 Section 7 Description Pilot's Operating Handbook Geared motor Internal actuator Intermediate bearings Wing flap External actuator Rods Control selector Figure 7.2.2 (1/2) - Wing flaps Page 7.2.6 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 450 Section 7 Description Pilot's Operating Handbook Figure 7.2.2 (2/2) - Wing flaps Edition 0 - October 31, 2013 Page 7.2.7 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
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Page 452: Accomodations
Section 7 Description Pilot's Operating Handbook - Accomodations Instrument panel The instrument panel contains instruments and controls necessary for flight monitoring. The typical instrument panel consists of all standard equipment, as well as additional optional equipment. Upper panel - see figure 7.3.2 The upper panel located at the top part of the windshield, contains electrical generation control panels, engine starting, ancillary electrical systems, AP/TRIMS switch, ELT remote control switch and the FUEL control panel.
Page 453 Section 7 Description Pilot's Operating Handbook Reception-micro jacks are located inside the recess under the arm-rest on both lateral sides of the cockpit, on R.H. side of intermediate R.H. passenger's seat and on the arm-rest of rear R.H. passenger's seat. Pedestal console - see figure 7.3.6 The pedestal console, under the MFD control unit, comprises flaps controls, pitch trim tab control wheel, aileron trim switch, engine controls and fuel tank selector.
Page 454 Section 7 Description Pilot's Operating Handbook >> Without v15.11 GARMIN software and voice alerts (Pre-MOD70-0407-00D). General alarms warning lights and CAS messages WARNING CAUTION messages appear on the MFD CAS window to alert crew about monitored systems discrepancies. As a message appears, a chime is heard.
Page 455 Section 7 Description Pilot's Operating Handbook gear up, idle and stall alternate high-pitched and low-pitched sounds gear up, extended flaps and stall alternate high-pitched and low-pitched sounds The aural warning box is fixed under cabin floor, on L.H. side, between frames C5 and It is electrically supplied by ESS BUS 2 bar and protected by AURAL WARN circuit breaker.
Page 456 Section 7 Description Pilot's Operating Handbook >> With v15.11 GARMIN software and voice alerts (Post-MOD70-0407-00D) General alarms warning lights and CAS messages WARNING CAUTION messages appear on the MFD CAS window to alert crew about monitored systems discrepancies. As a message appears, a chime is heard.
Page 457 Section 7 Description Pilot's Operating Handbook Refer to the GARMIN Pilot's Guide for description of the other aural warning alerts. Cockpit overhead panel - see figure 7.3.2 This panel includes following elements : the loud-speaker of GMA 1, the loud-speaker of GMA 2, the HORN TEST push-button, the emergency lighting rheostat.
Page 458 Section 7 Description Pilot's Operating Handbook >> All Figure 7.3.1 - Instrument panel assembly (Typical arrangement) Edition 0 - October 31, 2013 Page 7.3.7 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 459 Section 7 Description Pilot's Operating Handbook L.H. instrument panel emergency lighting Buzzer (V alarm) Loud-speaker of GMA 2 R.H. instrument panel emergency lighting Instrument panel emergency lighting switches (rheostats) R.H. cockpit floodlight ELT remote control switch AP/TRIMS switch FUEL control panel - see figure 7.7.3 ENGINE START switches - see figure 7.6.4 ELECTRIC POWER switches - see figure 7.8.5 INT LIGHTS internal lighting switches - see figure 7.8.7...
Page 460 Section 7 Description Pilot's Operating Handbook Figure 7.3.2 (2/2) - Upper panel and cockpit overhead panel Edition 0 - October 31, 2013 Page 7.3.9 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 461 Section 7 Description Pilot's Operating Handbook GMA 1 audio panel General alarm red and amber indicators PFD 1 ESI-2000 Landing gear configuration and control panel - see figure 7.5.1 Parking brake control - see figure 7.5.6 Left station control wheel tube Deicing control and check panel - see figure 7.13.1 L.H.
Page 462 Section 7 Description Pilot's Operating Handbook Figure 7.3.3 (2/2) - Left instrument panel (Typical arrangement) Edition 0 - October 31, 2013 Page 7.3.11 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 463 Section 7 Description Pilot's Operating Handbook Stand-by compass AFCS mode controller Registration ECS air conditioning control panel - see figure 7.9.2 MFD control unit Figure 7.3.4 (1/2) - Central instrument panel Page 7.3.12 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 464 Section 7 Description Pilot's Operating Handbook Figure 7.3.4 (2/2) - Central instrument panel (Typical arrangement) Edition 0 - October 31, 2013 Page 7.3.13 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 465 Section 7 Description Pilot's Operating Handbook PFD 2 GMA 2 audio panel Right station control wheel tube Crew music Adjustable air outlet Right station reception-micro jacks Hour meter R. H. station rudder pedals adjusting handle Circuit breakers panel postlight Cigar lighter and two USB servicing plugs Cabin emergency air control (EMERGENCY RAM AIR control knob) Static source selector COM 2 (Stand-by / active)
Page 466 Section 7 Description Pilot's Operating Handbook Figure 7.3.5 (2/2) - Right instrument panel (Typical arrangement) Edition 0 - October 31, 2013 Page 7.3.15 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 467 Section 7 Description Pilot's Operating Handbook THROTTLE FLAPS lever THROTTLE friction adjustment Manual FUEL TANK SELECTOR - see figure 7.7.2 Roll trim tab control MAN OVRD emergency fuel regulation lever Pitch trim tab control Lock for access door to landing gear emergency pump - see figure 7.5.2 Figure 7.3.6 (1/2) - Pedestal console Page 7.3.16 Edition 0 - October 31, 2013...
Page 468 Section 7 Description Pilot's Operating Handbook Figure 7.3.6 (2/2) - Pedestal console (Typical arrangement) Edition 0 - October 31, 2013 Page 7.3.17 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 469 Section 7 Description Pilot's Operating Handbook Figure 7.3.7 - Circuit breakers panel Page 7.3.18 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 470 Section 7 Description Pilot's Operating Handbook Figure 7.3.8 - General alarms warning lights Edition 0 - October 31, 2013 Page 7.3.19 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 471: Doors, Windows And Emergency Exit
Section 7 Description Pilot's Operating Handbook Doors, windows and emergency exit Cabin access door - see figure 7.3.9 The cabin one-piece access door, located on the left side of fuselage aft of the wings, opens outside. The retractable stairs and hand rail make boarding easier. To open the door from outside the airplane (make sure the door is not locked), press on front end of the handle embedded in door (this pressure disengages the handle from its recess), then turn the handle upwards.
Page 472 Section 7 Description Pilot's Operating Handbook CAUTION ▲ ▲ Retract stairs before closing access door and make sure door deflection area is clear. ▲ To retract stairs from outside the airplane, raise stairs by pushing them upwards from the lower part and fold them inside cabin. While stairs are retracted, the hand rail folds To close the door from outside the airplane, press on knob on outside fuselage at the right side of the door.
Page 473 Section 7 Description Pilot's Operating Handbook Figure 7.3.9 - Cabin access door Page 7.3.22 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 474 Section 7 Description Pilot's Operating Handbook Cockpit access door - see figure 7.3.9A The cockpit access door, so-called pilot door, if installed located on the left side of fuselage forward of the wings, opens outside. Retractable footstep makes boarding easier. WARNING ▲...
Page 475 Section 7 Description Pilot's Operating Handbook FWD compartment door The FWD compartment door is located on the airplane left side between the firewall and the front pressure bulkhead. It is hinged at the top. It is maintained in the up position by a compensation rod.
Page 476 Section 7 Description Pilot's Operating Handbook Figure 7.3.9A - Cockpit access door (pilot door) Edition 0 - October 31, 2013 Page 7.3.25 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 477 Section 7 Description Pilot's Operating Handbook Emergency exit - see figure 7.3.10 The emergency exit is installed on the right side of the fuselage and opens towards the inside. It is equipped with two handles, one inside and the other outside, each located on the upper frame.
Page 478 Section 7 Description Pilot's Operating Handbook Emergency exit - see figure 7.3.10 The emergency exit is installed on the right side of the fuselage and opens towards the inside. It is equipped with two handles, one inside and the other outside, each located on the upper frame.
Page 479 Section 7 Description Pilot's Operating Handbook Figure 7.3.10 - Emergency exit Edition 0 - October 31, 2013 Page 7.3.27 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 480 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 481 Section 7 Description Pilot's Operating Handbook Intentionally left blank Edition 0 - October 31, 2013 Page 7.3.27B TR29 - July 2022 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 482: Seats, Belts And Harnesses
Section 7 Description Pilot's Operating Handbook >> All Seats, belts and harnesses Cockpit seats - see figure 7.3.11 L.H. and R.H. front seats are mounted on rails attached to the structure. Longitudinal position, height and back-rest tilting of each seat can be adjusted and the arm-rest is hinged.
Page 483 Section 7 Description Pilot's Operating Handbook Seats, belts and harnesses Cockpit seats - see figure 7.3.11 L.H. and R.H. front seats are mounted on rails attached to the structure. Longitudinal position, height and back-rest tilting of each seat can be adjusted and the arm-rest is hinged.
Page 484 Section 7 Description Pilot's Operating Handbook ONLY zone B and zone C can be modified for seat configurations Location For all configurations, verify that your number luggages are stowed and attached in the appropriate areas Fwd baggage zone Pilot zone: No modification allowed MID Seat Zone = Possibility of seat configuration REAR Seat Zone = Possibility of seat...
Page 485 Section 7 Description Pilot's Operating Handbook Here are all the configurations possibilities Configuration Location number name Zone C Zone B (1) This configuration accepts small net or large net Each cross indicates that you have a seat at the correspondent location number. Page 7.3.30 Edition 0 - October 31, 2013 Rev.
Page 486: Baggage Compartments
Section 7 Description Pilot's Operating Handbook Belts and harnesses - see figure 7.3.12 WARNING ▲ ▲ Incorrect closure of the safety belt may introduce a risk. Make sure it is tightened when buckled. To be most efficient, the belt must not be twisted. Check that there is no constraint when operated.
Page 487 Section 7 Description Pilot's Operating Handbook WARNING ▲ ▲ Any parcel or baggage must be stowed by straps. It is the pilot's responsibility to check that all the parcels and baggage are properly secured in the cabin. In case of transport of dangerous materials, respect the law concerning transport of dangerous materials and any other applicable regulation.
Page 488 Section 7 Description Pilot's Operating Handbook Authorized anchoring points are identified with green self-adhesive labels affixed to the inside of the seat rail. A placard indicates loading limits for each cargo net : for the small cargo net, it is affixed on frame C13bis, for the large cargo net, it is affixed on R.H.
Page 489: Use Of Cargo Nets
Section 7 Description Pilot's Operating Handbook Use of cargo nets Net inspection Before each use, visually inspect net for : webbing condition, seam condition of tensioning strap, metallic part condition. Installation instructions Tensioning straps must be installed so that they make a V with a minimum angle of 40° between both strands attached on the net.
Page 490 Section 7 Description Pilot's Operating Handbook Intentionally left blank Edition 0 - October 31, 2013 Page 7.3.35 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 491 Section 7 Description Pilot's Operating Handbook >> With 6-seat accommodation Front passenger seat L. H. pilot seat R. H. intermediate passenger seat, back to flight direction L. H. intermediate passenger seat, back to flight direction R. H. rear passenger seat Rear bench L.
Page 492 Section 7 Description Pilot's Operating Handbook Figure 7.3.11 (2/2) - Seats Edition 0 - October 31, 2013 Page 7.3.37 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 493 Section 7 Description Pilot's Operating Handbook >> With 4-seat accommodation Front passenger seat L. H. pilot seat R. H. intermediate passenger seat, facing flight direction L. H. intermediate passenger seat, facing flight direction Front seat(s) longitudinal shift control Front seat(s) height control Front seat(s) back-rest tilt control Intermediate seat(s) back-rest tilt control Figure 7.3.11A (1/2) - Seats...
Page 494 Section 7 Description Pilot's Operating Handbook Figure 7.3.11A (2/2) - Seats Edition 0 - October 31, 2013 Page 7.3.39 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 495 Section 7 Description Pilot's Operating Handbook >> All Figure 7.3.12 - Front and rear seat belts,with movable straps, and harnesses Page 7.3.40 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 496: Flight Controls
Section 7 Description Pilot's Operating Handbook - Flight controls Flight controls consist of roll, pitch and rudder controls, as well as roll trim tab, pitch trim tab and rudder trim tab controls. ● NOTE ● During airplane parking, it is recommended to lock flight controls - see figure 8.6.2 ●...
Page 497 Section 7 Description Pilot's Operating Handbook Pedestal assembly Control wheels Fuselage roll lever Spoiler Aileron Aileron control in wing Spoiler control Figure 7.4.1 (1/2) - Roll Page 7.4.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 498 Section 7 Description Pilot's Operating Handbook Figure 7.4.1 (2/2) - Roll Edition 0 - October 31, 2013 Page 7.4.3 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 499 Section 7 Description Pilot's Operating Handbook Roll trim tab Aileron Adjustable rods Actuator Trim tab control wiring Trim switch on pedestal console Figure 7.4.2 (1/2) - Lateral trim Page 7.4.4 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 500 Section 7 Description Pilot's Operating Handbook Figure 7.4.2 (2/2) - Lateral trim Edition 0 - October 31, 2013 Page 7.4.5 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 501: Elevator
Section 7 Description Pilot's Operating Handbook Elevator - see figure 7.4.3 Both elevators are activated simultaneously by the same control. Each control surface is hinged at three points to the rear part of horizontal stabilizer. The control wheel controls the two elevators through rods, bearings and bellcranks. A spring actuator creates a nose-down artificial force which allows a better static stability.
Page 502 Section 7 Description Pilot's Operating Handbook Control wheel assembly Elevators Lever assembly, fuselage rear part Elevator bellcrank Rod with presseal connection Lever assembly under floor Pedestal assembly Actuator Figure 7.4.3 (1/2) - Elevator Edition 0 - October 31, 2013 Page 7.4.7 Rev.
Page 503 Section 7 Description Pilot's Operating Handbook Figure 7.4.3 (2/2) - Elevator Page 7.4.8 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 504 Section 7 Description Pilot's Operating Handbook Cables Pulleys Pitch trim tabs Actuating rods Actuator Pitch trim manual control wheel Electric pitch trim control Figure 7.4.4 (1/2) - Pitch trim Edition 0 - October 31, 2013 Page 7.4.9 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 505 Section 7 Description Pilot's Operating Handbook Figure 7.4.4 (2/2) - Pitch trim Page 7.4.10 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 506: Rudder
Section 7 Description Pilot's Operating Handbook Rudder - see figure 7.4.5 The rudder is hinged on three fittings attached to the vertical stabilizer rear spar. The rudder pedals / rudder linkage is ensured through cables and a rod. Pilot and R.H. station rudder pedal positions are adjustable at each station. The rudder pedal adjustment mechanism (for piloting comfort purposes) includes a manual control located against the external bulkhead beneath the instrument panel and a locking device on the rudder pedals.
Page 507 Section 7 Description Pilot's Operating Handbook Roll / rudder combination bellcrank installation Rudder pedals assembly Control cables Pulleys Rudder lever assembly Rudder Nose gear steering rod Figure 7.4.5 (1/2) - Rudder Page 7.4.12 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 508 Section 7 Description Pilot's Operating Handbook Figure 7.4.5 (2/2) - Rudder Edition 0 - October 31, 2013 Page 7.4.13 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 509 Section 7 Description Pilot's Operating Handbook Trim switch on control wheel Actuator Rudder trim tab Rods Rudder trim control wiring Figure 7.4.6 (1/2) - Rudder trim Page 7.4.14 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 510 Section 7 Description Pilot's Operating Handbook Figure 7.4.6 (2/2) - Rudder trim Edition 0 - October 31, 2013 Page 7.4.15 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 511 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.4.16 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 512: Landing Gear
Section 7 Description Pilot's Operating Handbook - Landing gear The airplane is equipped with electro-hydraulically actuated, fully retractable tricycle landing gear. Each landing gear is equipped with one wheel and an oil-air shock absorber integrated in the strut. Main landing gears swivel on two ball joints installed on wing spars. Each landing gear retracts toward airplane centerline.
Page 513: Landing Gear Position Indicator
Section 7 Description Pilot's Operating Handbook Landing gear position indicator - see figure 7.5.1 Landing gear position indication is accomplished by 5 lights : On LANDING GEAR control panel 3 green indicator lights (one per landing gear), 1 red warning light GEAR UNSAFE 1 amber light in the LANDING GEAR lever.
Page 514 Section 7 Description Pilot's Operating Handbook Green indicator light Red warning light LANDING GEAR lever CHECK DOWN push-button LIGHT TEST push-button Amber light Figure 7.5.1 - Control panel and landing gear indicating Edition 0 - October 31, 2013 Page 7.5.3 Rev.
Page 515: Safety
Section 7 Description Pilot's Operating Handbook Safety Safety switch - landing gear retraction A safety switch installed on each main landing gear prevents, by detecting shock strut compression, landing gear accidental retraction when airplane is on ground. >> Without voice alerts (Pre-MOD70-0407-00D) Landing gear horn Landing gear horn is controlled by throttle and / or flaps.
Page 516 Section 7 Description Pilot's Operating Handbook Figure 7.5.2 - Emergency landing gear extension control Edition 0 - October 31, 2013 Page 7.5.5 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 517: Ground Maneuvers
Section 7 Description Pilot's Operating Handbook Ground maneuvers Nose gear steering control - see figures 7.5.3 and 7.5.4 Nose gear steering control is combined with rudder pedals and is fitted with a shimmy damper. When one of rudder pedals is fully pushed, nose wheel swivels about 20°. Steering may be increased up to 28°...
Page 518 Section 7 Description Pilot's Operating Handbook Figure 7.5.3 - Minimum turn diameter (Full rudder pedals travel without using differential braking) Edition 0 - October 31, 2013 Page 7.5.7 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 519 Section 7 Description Pilot's Operating Handbook Figure 7.5.4 - Minimum turn diameter (Full rudder pedals travel by using differential braking) Page 7.5.8 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 520: Brake System
Section 7 Description Pilot's Operating Handbook Brake system - see figure 7.5.5 Airplane is equipped with a hydraulically actuated disc braking system installed on the main landing gear wheels. Each toe brake at L.H. and R.H. stations is equipped with a master cylinder which sends hydraulic pressure to the corresponding disc brake : L.H.
Page 521 Section 7 Description Pilot's Operating Handbook Reservoir Vent R.H. station master cylinders PARK BRAKE control knob PARK BRAKE valve Drain Pilot's station master cylinders L.H. brake assembly R.H. brake assembly Figure 7.5.5 (1/2) - Brake system Page 7.5.10 Edition 0 - October 31, 2013 Rev.
Page 522 Section 7 Description Pilot's Operating Handbook Figure 7.5.5 (2/2) - Brake system Edition 0 - October 31, 2013 Page 7.5.11 Rev. 6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 523 Section 7 Description Pilot's Operating Handbook Figure 7.5.6 - Brake system Page 7.5.12 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 524: Powerplant
Section 7 Description Pilot's Operating Handbook - Powerplant Turboprop engine operation - see figure 7.6.1 The PRATT & WHITNEY CANADA turboprop engine (PT6A-66D model) is a free turbine engine rated at 850 SHP and developing a thermodynamic power of 1825 ESHP. Intake air enters engine through an annular casing and is then ducted toward compressor.
Page 525 Section 7 Description Pilot's Operating Handbook Propeller governor Exhaust stub Axial compressors Accessory gearbox FCU Fuel Control Unit Oil to fuel heater Input coupling shaft Air intake Centrifugal impeller Combustion chamber Compressor turbine Power turbine 1st stage Power turbine 2nd stage Power turbine shaft Figure 7.6.1 (1/2) - Powerplant Page 7.6.2...
Page 526 Section 7 Description Pilot's Operating Handbook Figure 7.6.1 (2/2) - Powerplant Edition 0 - October 31, 2013 Page 7.6.3 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 527: Engine Control Levers
Section 7 Description Pilot's Operating Handbook Engine control levers - see figure 7.6.2 Engine operation requires use of two levers located on pedestal console in cabin : THROTTLE (Item 1), and its detent for reverse (Item 4) MAN OVRD control for emergency fuel regulation (Item 3). ●...
Page 528 Section 7 Description Pilot's Operating Handbook THROTTLE - see figure 7.6.3 The THROTTLE has two operating modes : thrust mode and condition mode. Thrust mode The THROTTLE is in vertical position. It modulates engine power from full reverse to max power. Engine running, the throttle rearward displacement, past the lock using the detent, allows to control : the engine power in the Beta range from idle to maximum reverse,...
Page 529 Section 7 Description Pilot's Operating Handbook Condition mode The THROTTLE is moved to the condition side by lifting the knob. As long as the THROTTLE is in condition mode, the propeller is in feather position.The THROTTLE can be positioned to CUT OFF, idle LO-IDLE or idle HI-IDLE.
Page 530: Engine Instruments
Section 7 Description Pilot's Operating Handbook Engine instruments Engine indicating consists of : engine torque expressed in percent (%), TRQ propeller speed in RPM, PROP RPM generator rotation speed expressed in percent (%), Ng ITT expressed in °C, oil pressure expressed in PSI. oil temperature expressed in °C.
Page 531: Engine Starting
Section 7 Description Pilot's Operating Handbook Engine starting - see figure 7.6.4 Ignition function Ignition system consists of an ignition unit and two spark igniter plugs in powerplant, a three-position IGNITION switch OFF - AUTO - ON located on ENGINE START panel at upper panel.
Page 532 Section 7 Description Pilot's Operating Handbook Figure 7.6.4 - Engine starting Edition 0 - October 31, 2013 Page 7.6.9 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 533: Engine Air Inlet
Section 7 Description Pilot's Operating Handbook Engine air inlet Engine air inlet is located at front lower section of engine cowling. Air inlet port is protected against icing by a hot air flux provided by engine. Air is driven throughout a duct in engine casing before entering engine through a protective screen.
Page 534 Section 7 Description Pilot's Operating Handbook Compressor turbine tacho-generator (Ng) Compressor turbine tacho-generator (Ng) is attached on accessory gearbox. It supplies a voltage which is transmitted to the GARMIN system for display on the MFD, under normal display conditions. Power turbine tacho-generator (Np) Power turbine tacho-generator is attached on the right side of the reduction gearbox.
Page 535: Propeller
Section 7 Description Pilot's Operating Handbook Propeller Airplane is equipped with a composite five-bladed, constant-speed and full-feathering propeller. Regulation Propeller governor located on engine maintains rotation speed to the nominal value of 2000 RPM. Regulation is obtained through propeller blade pitch variation : counterweights drive propeller blades toward high pitch (low RPM) whereas oil pressure delivered by governor drives back blades toward low pitch (high RPM).
Page 536: Fuel System
Section 7 Description Pilot's Operating Handbook - Fuel system - see figure 7.7.1 The fuel system comprises fuel tanks, fuel unit, selectors, manual and automatic, electric and mechanical boost pumps, engine fuel system, gaging installation, monitoring installation and drains. Fuel tanks Fuel tanks are formed by sealed casings in each wing.
Page 537 Section 7 Description Pilot's Operating Handbook Flow divider Fuel unit Flowmeter Filter drain Collector tank Fuel return pipe Fuel regulator Filling port High pressure pump (HP) NACA scoop Oil to fuel heater Tank vent valve Low pressure switch Fuel level gages Fuel jet Tank drain valve Main mechanical boost pump...
Page 538 Section 7 Description Pilot's Operating Handbook Figure 7.7.1 (2/2) - Fuel system Edition 0 - October 31, 2013 Page 7.7.3 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 539: Automatic Tank Selector
Section 7 Description Pilot's Operating Handbook Automatic tank selector - see figures 7.7.2 and 7.7.3 Automatic tank selection allows, without pilot's intervention, feeding the engine from one tank or the other in predetermined sequences. These sequences depend on airplane configuration (ground, in-flight, fuel low level CAS messages appearance). Automatic tank selection system comprises an electronic sequencer, an actuator attached on the fuel unit, FUEL SEL two-position selector (AUTO, MAN) and SHIFT push-knob located on FUEL panel.
Page 540: Electric Boost Pump (Aux Bp)
Section 7 Description Pilot's Operating Handbook >> All ● NOTE ● The manual selector is driven by the fuel unit and is positioned on R or L mark corresponding to the tank selected by the sequencer. Therefore, the pilot continuously knows the tank which is operating. ●...
Page 541 Section 7 Description Pilot's Operating Handbook Figure 7.7.2 - Manual selector of fuel tanks Page 7.7.6 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 542 Section 7 Description Pilot's Operating Handbook AUX BP switch FUEL SEL switch SHIFT push-button Figure 7.7.3 - Fuel control panel Edition 0 - October 31, 2013 Page 7.7.7 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 543: Main Mechanical Boost Pump
Section 7 Description Pilot's Operating Handbook Main mechanical boost pump The mechanical boost pump is attached to accessory gearbox and supplies fuel necessary for engine operation. Engine fuel system The engine fuel system consists of a fuel regulator, pumps, filters, a fuel divider and fuel nozzles.
Page 544: Fuel System Draining And Clogging Indicator
Section 7 Description Pilot's Operating Handbook Fuel system draining and clogging indicator - see figure 7.7.4 The fuel system comprises five drain points, a drain on the filter bowl, two drain valves on each tank, located on wing lower surface, one at wing root and the other past main landing gear well.
Page 545 Section 7 Description Pilot's Operating Handbook Lighting switch Mirror door Clogging indicator Central access door Filter drain Tank drain Drain bowl Figure 7.7.4 - Fuel system draining points and clogging indicator Page 7.7.10 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 546: Electrical System
Section 7 Description Pilot's Operating Handbook - Electrical system - see figures 7.8.1, 7.8.2 and 7.8.5 The airplane is fitted with a 28-volt direct-current electrical system. Electrical supply is obtained from various power supplies : a starter generator a stand-by generator a battery a ground power unit, via a plug, located on L.H.
Page 547: Stand-By Generator
Section 7 Description Pilot's Operating Handbook Stand-by generator Stand-by generator supplies a 28-volt stand-by direct current which may be used in case of main generator failure. Generator connection with main bus bar is controlled through GENERATOR selector set to ST-BY, it will be effective when connection conditions are met. ●...
Page 548: Distribution
Section 7 Description Pilot's Operating Handbook Ground power receptacle door opening is indicated by GPU DOOR appearance. ● NOTE ● Before connecting a GPU to the airplane, ensure that the voltage of the GPU is regulated between 27.5 volts and 28.5 volts. The amperage output needs to be consistent with the airplane placard in front of compartment door : GPU shall provide a current limiting function, and current limit shall be set per placard.
Page 549: Emergency Use
Section 7 Description Pilot's Operating Handbook BATT BUS bar is directly connected to the battery ; it is protected by a fuse, located in EPS box, and a breaker, located in the front cargo compartment on C2 frame left side. ●...
Page 550 Section 7 Description Pilot's Operating Handbook Figure 7.8.1 - Electrical diagram Edition 0 - October 31, 2013 Page 7.8.5 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 551 Section 7 Description Pilot's Operating Handbook Switches Buses are powered by Crash BATT BUS 1 Source Generator lever BUS 1 BUS 2 TO 5 BATT NORM Battery Battery Battery Battery Battery Battery Battery Battery BATT MAIN NORM & MAIN & MAIN &...
Page 552 Section 7 Description Pilot's Operating Handbook Figure 7.8.3 (1/3) - Electrical distribution of bus bars Edition 0 - October 31, 2013 Page 7.8.7 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 553 Section 7 Description Pilot's Operating Handbook Figure 7.8.3 (2/3) - Electrical distribution of bus bars Page 7.8.8 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 554 Section 7 Description Pilot's Operating Handbook Figure 7.8.3 (3/3) - Electrical distribution of bus bars Edition 0 - October 31, 2013 Page 7.8.9 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 555 Section 7 Description Pilot's Operating Handbook ESS BUS TIE Essential bus NORM & EMER switch BUS 1 AP SERVOS Autopilot servo protection FLAPS Flaps protection AIL TRIM Aileron trim protection RUD TRIM Pitch trim protection BUS 2 LDG GEAR Landing gear general supply protection ESS BUS 1 ESS BUS 1 Essential bus 1 circuit protection...
Page 556 Section 7 Description Pilot's Operating Handbook BUS 1 AP CTRL Flight controller protection PFD 2 Primary Flight Display 2 protection COM 2 VHF 2 & radio protection GPS/NAV 2 GPS NAV 2 protection ADC 2 Air Data Computer 2 protection AIRFRAME DE ICE Empennage and wing leading edges deicing INERT DE ICE...
Page 557 Section 7 Description Pilot's Operating Handbook BUS 3 OXYGEN PRESS Oxygen/Pressure indication protection L WS DE ICE L.H. windshield deicing protection PITOT R & STALL Pitot R and stall warning heating protection FUEL SEL Tank selector timer protection AUX BP Electrical fuel pump protection XPDR 2 Transponder 2, if installed, protection...
Page 558 Section 7 Description Pilot's Operating Handbook Figure 7.8.4 (4/4) - Breaker panel (Typical arrangement) Edition 0 - October 31, 2013 Page 7.8.13 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 559: Indicating
Section 7 Description Pilot's Operating Handbook Indicating Electrical system indicating consists of voltage and ampere indicating - refer to GARMIN Pilot's Guide for further details. Following CAS messages may appear on the MFD CAS window : BAT OFF : Battery is not connected to main bus bar MAIN GEN : Starter generator is not connected to main bus bar LOW VOLTAGE...
Page 560 Section 7 Description Pilot's Operating Handbook MAIN reset knob ST-BY reset knob Crash lever SOURCE selector GENERATOR selector Figure 7.8.5 - Electrical control Edition 0 - October 31, 2013 Page 7.8.15 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 561: Exterior Lighting
Section 7 Description Pilot's Operating Handbook Exterior lighting - see figure 7.8.6 The airplane is equipped with three strobe and navigation lights, two landing lights, two taxi lights, two recognition lights and a wing leading edge icing inspection light. Landing lights Landing lights are embedded in the winglets and located in leading edges.
Page 562 Section 7 Description Pilot's Operating Handbook FWD compartment light The dome light illumination of the FWD compartment is controlled by the switch located in the upper section of the door frame. Fuel unit compartment light The lighting of the fuel unit compartment allows improving the visibility of the clogging indicator by pressing the push-button located besides the inspection door.
Page 563 Section 7 Description Pilot's Operating Handbook Taxi and landing light switch Pulselite system switch Navigation lights switch Strobe lights switch Figure 7.8.6 - External lighting controls Page 7.8.18 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 564: Interior Lighting
Section 7 Description Pilot's Operating Handbook Interior lighting - see Figure 7.8.7 Interior lighting consists of access, cabin, instrument panel, instruments, baggage compartment and emergency lighting. Access lighting Access lighting consists of two floodlights located on the ceiling upholstering (one at the level of the access door, the other at the level of the storage cabinet) and the L.H.
Page 565 Section 7 Description Pilot's Operating Handbook Instrument panel lighting switch (rheostat) DIMMER switch Cabin lighting switch (rear seats reading light) Access door, baggage compartment and FWD dome light (delayed breaker) push-button Emergency lighting switch Breaker panel lighting switch Figure 7.8.7 (1/2) - Internal lighting controls Page 7.8.20 Edition 0 - October 31, 2013 Rev.
Page 566 Section 7 Description Pilot's Operating Handbook Figure 7.8.7 (2/2) - Internal lighting controls Edition 0 - October 31, 2013 Page 7.8.21 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 567 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.8.22 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 568: Air Conditioning And Pressurization
Section 7 Description Pilot's Operating Handbook - Air conditioning and pressurization ● NOTE ● A list of abbreviations used in this chapter is given in figure 7.9.2. ● The airplane is equipped with a Global Air System (GAS), which ensures air conditioning and pressurization control - see figure 7.9.2.
Page 569: Engine Bleed Air System
Section 7 Description Pilot's Operating Handbook Engine bleed air system The engine bleed air system is designed to ensure the following functions : to regulate the bleed air from the engine, to ensure a controlled airflow in the cabin, to adjust the bleed air temperature for cabin heating. To regulate the bleed air from the engine The engine bleed air system operates from either P2.5 or P3 engine bleed ports.
Page 570: Cabin Pressurization Control System
Section 7 Description Pilot's Operating Handbook System operation See figure 7.9.3. The BLEED switch allows selection of the engine bleed air system provided that the engine is running. The Ground Fan (GF) operates until takeoff, when BLEED switch is set to AUTO, and MAIN GEN is OFF.
Page 571 Section 7 Description Pilot's Operating Handbook Cabin altitude management In order to maximize comfort during all phases of flight, the cabin altitude is automatically computed by the GASC using flight parameters (such as aircraft altitude, altitude rate of change) sent by the avionics. During descent, the GASC uses the Landing Field Elevation (LFE) to manage the optimal cabin altitude rate of change in order to land with a cabin altitude equal to LFE minus 200 ft.
Page 572 Section 7 Description Pilot's Operating Handbook CAS messages are displayed in the MFD CAS window : BLEED TEMP indicates that an overtemperature was detected by either the Bleed Temperature Switch (BTSW) or the Overheat Thermal Switch (OTSW). BLEED OFF indicates that either the BLEED switch is in OFF position or that a system malfunction was detected by the GASC.
Page 573: Dual Zones Environmental Control System
Section 7 Description Pilot's Operating Handbook Dual zones Environmental Control System (ECS) The ECS ensures both Cockpit and Cabin heating and cooling functions. The ECS consists of two independent air circuits : Heating circuit, controlled by Temperature Conditioning System (TCS) Cooling circuit, controlled by Vapor Cycle Cooling System (VCCS) Heating circuit The TCS regulates hot air coming from the bleed air system (also used for...
Page 574 Section 7 Description Pilot's Operating Handbook cabin circuit, by passing through : the overhead duct equipped with swivelling and adjustable air outlets, ports located on the floor between the cabinets and the intermediate passenger's seats. System operation See figure 7.9.3 and paragraph Air temperature management. ECS control panel selection : If the A/C switch is set to OFF : >>...
Page 575 Section 7 Description Pilot's Operating Handbook TEMP/°C selectors : Allow adjustment of the temperature for the cockpit and cabin zones. >> After GASC software evolution (Post-MOD70-0689-21) If the pilot or passengers set the TEMP/°C selector to the maximum heat position, the bleed air system automatically switches from the P2.5 to the P3 bleed port to increase the temperature and flow rate of the incoming bleed air.
Page 576 Section 7 Description Pilot's Operating Handbook System protection Power for the ECS is supplied by the BUS 2 bar and is protected by the AIR COND breaker. Four fans are supplied by BUS 4 bar and protected respectively by following breakers : COND FAN, CABIN FAN, COCKPIT FAN and GND FAN.
Page 577 Section 7 Description Pilot's Operating Handbook Air temperature management Cockpit and cabin heating / cooling Cockpit and cabin air temperature management is operated by selecting : For optimal air temperature management, select A/C switch to MANUAL and CONTROL selector to CABIN : Air temperature Cockpit panel selection Cabin panel selection...
Page 578 Section 7 Description Pilot's Operating Handbook Air temperature Cockpit panel selection Cabin panel selection expectations Cockpit Warm area Cabin Warm area Results Mixed Bleed Air Circuit : Warm air is distributed to both cockpit and cabin equally due to equal temperature demand. Cold Air Circuit : Not active, as no TEMP/°C selector is set below 22°C.
Page 579 Section 7 Description Pilot's Operating Handbook Air temperature Cockpit panel selection Cabin panel selection expectations Cockpit Cool area Cabin Cool area Results Mixed Bleed Air Circuit : With the cockpit and cabin TEMP/°C selectors set below 22°C, the Hot Air Distributor discharges the mixed bleed air below the floor towards the cold air circuit fans and evaporators to reduce the air to the desired temperature.
Page 580 Section 7 Description Pilot's Operating Handbook Cabin override Select A/C switch to MANUAL and CONTROL selector to COCKPIT. Setting the CONTROL selector to COCKPIT position disables TEMP/°C and FAN SPEED selectors in the cabin area. The COCKPIT position also distributes warm air equally to the cockpit and cabin. Only the cockpit TEMP/°C and FAN SPEED selectors inputs are used by the GASC for air temperature management.
Page 581 Section 7 Description Pilot's Operating Handbook Air temperature Cockpit panel selection Cabin panel selection expectations Cockpit Cool area Cabin area Results Mixed Bleed Air Circuit : With the cockpit TEMP/°C selector set below 22°C, the Hot Air Distributor discharges the mixed bleed air below the floor towards the cold air circuit fans and evaporators to reduce the air to the desired temperature.
Page 582 Section 7 Description Pilot's Operating Handbook Windshield DEFOG Windshield defog is operated by selecting : Air temperature Cockpit panel selection Cabin panel selection expectations Cockpit area Cabin area Results Mixed Bleed Air Circuit : Air is distributed to the windshields and cockpit side windows at a fixed temperature regardless of TEMP/°C selector settings.
Page 583 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.9.16 Edition 0 - October 31, 2013 Rev. 6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 584 Section 7 Description Pilot's Operating Handbook Demisting outlets Front vents Cockpit ventilated temperature sensor (CKVTS) Cabin ventilated temperature sensor (CBVTS) Air ports Cabin control panel Global air system controller (GASC) Out-flow valve (OFV) Safety valve (SFV) Condenser fan Condenser High pressure switch Drier filter Cabin fan Cabin evaporator...
Page 585 Section 7 Description Pilot's Operating Handbook Demisting microswitch Hot air distributor (HAD) Cabin inlet temperature sensor (ITS) Cabin bleed temperature switch (BTSW) Mixing ejector (MIXEJ) Check valve MFD unit Ground safety microswitch Differential pressure switch By-pass valve (BPV) Cabin altitude alarm switch Emergency air supply system (EMERGENCY RAM AIR) Main heat exchanger (MHX)
Page 586 Section 7 Description Pilot's Operating Handbook Figure 7.9.2 (3/3) - Edition 0 - October 31, 2013 Page 7.9.19 Rev. 6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 587 Section 7 Description Pilot's Operating Handbook A/C switch BLEED switch PRES MODE switch DUMP switch HOT AIR FLOW distributor TEMP/° C selector (cockpit/cabin) CONTROL selector FAN SPEED selector (cockpit) FAN SPEED selector (cabin) CABIN TEMP/° C selector (cabin) Figure 7.9.3 (1/2) - GAS controls Page 7.9.20 Edition 0 - October 31, 2013 Rev.
Page 588 Section 7 Description Pilot's Operating Handbook Figure 7.9.3 (2/2) - GAS controls Edition 0 - October 31, 2013 Page 7.9.21 Rev. 6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
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Page 590: Emergency Oxygen System
Section 7 Description Pilot's Operating Handbook 7.10 - Emergency oxygen system - see figure 7.10.1 The gaseous oxygen system will be used by the crew and the passengers, when the cabin altitude is greater than 10000 ft following a loss of pressurization or in case of cabin air contamination.
Page 591 Section 7 Description Pilot's Operating Handbook MICRO / MASK switch OXYGEN switch PASSENGER OXYGEN switch Figure 7.10.1 - Emergency oxygen system Page 7.10.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 592 Section 7 Description Pilot's Operating Handbook A control panel located in the cockpit overhead panel at the disposal of the pilot includes : a two-position valve ON/OFF (OXYGEN switch) to permit the supply of the front seats occupiers masks, a two-position valve ON/OFF (PASSENGERS OXYGEN switch) with guard to permit the supply of the passengers four masks, when the first valve is open.
Page 593: Flight Above 15000 Ft With Possible Emergency Descent
Section 7 Description Pilot's Operating Handbook Flight above 15000 ft with possible emergency descent Minimum oxygen pressure (PSIG) for following conditions : 4 minutes from 31000 to 15000 ft. All equipment used from 31000 ft. Plus 30 minutes usage by each pilot and passenger at 15000 ft. Plus 86 minutes usage by each pilot at 10000 ft.
Page 594: When Required To Remain Above 15000 Ft Due To Minimum Enroute Altitude
Section 7 Description Pilot's Operating Handbook When required to remain above 15000 ft due to minimum enroute altitude Minimum oxygen pressure (PSIG) for following conditions : Flight above 15000 ft. All equipment used. 1 hour usage by each pilot and passenger. Plus 1 hour usage by each pilot under 15000 ft.
Page 595: Flight Between 15000 Ft And 10000 Ft
Section 7 Description Pilot's Operating Handbook Flight between 15000 ft and 10000 ft Minimum oxygen pressure (PSIG) for following conditions : Flight under 15000 ft. 90 minutes usage by each pilot and one passenger. Plus 30 minutes usage by each pilot at 10000 ft. Number of Outside temperature occupants...
Page 596: O 2 Smart Mike Mask, If Installed
Section 7 Description Pilot's Operating Handbook smart mike mask, if installed The two cockpit masks, O smart mike masks, are equipped with a system that detects when a communication is made operating one of the push-to-talk buttons. It activates a noise reduction system that attenuates the oxygen flow noise in the headsets.
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Page 598: Air Data System And Instruments
Section 7 Description Pilot's Operating Handbook 7.11 - Air data system and instruments - see figure 7.11.1 Airplane air data system consists of : two separate static pressure systems supplying an electronic standby indicator and air data computers (ADC). A part of system 1 is backed up by an alternate system which operation is controlled by a switching valve (normal / alternate) attached to instrument panel under R.H.
Page 599: Dynamic Pressure System
Section 7 Description Pilot's Operating Handbook Dynamic pressure system One heated pitot probe is installed under the L.H. wing. The second one is installed under the R.H. wing. The first one supplies the electronic standby indicator and one ADC. The second one supplies the other ADC. Both lines incorporate a drain plug located in the root of L.H.
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Page 601 Section 7 Description Pilot's Operating Handbook Pitot L Dynamic system drain Electronic Standby Instrument FWD pressure bulkhead Static system drain Static system drain Static system drain Emergency static system drain Emergency static valve (Normal / alternate) Instrument panel Dynamic system drain Pitot R Rear pressure bulkhead Static port...
Page 602 Section 7 Description Pilot's Operating Handbook Figure 7.11.1 (2/2) - Air data system Edition 0 - October 31, 2013 Page 7.11.5 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
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Page 604: Vacuum System And Instruments
Section 7 Description Pilot's Operating Handbook 7.12 - Vacuum system and instruments - see figure 7.12.1 The airplane is fitted with a vacuum system providing the suction necessary to operate the cabin pressurization and the leading edge deicing. Vacuum system includes : A pressure regulator An ejector A regulating and relief valve...
Page 605 Section 7 Description Pilot's Operating Handbook Pressure regulator Ejector Valve Regulating and relief valve Pressure switch Failure CAS message Figure 7.12.1 (1/2) - Vacuum system Page 7.12.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 606 Section 7 Description Pilot's Operating Handbook Figure 7.12.1 (2/2) - Vacuum system Edition 0 - October 31, 2013 Page 7.12.3 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 607 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.12.4 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 608: Ice Protection Equipment
Section 7 Description Pilot's Operating Handbook 7.13 - Ice protection equipment - see figure 7.13.1 Ice protection equipment is as follows : Pneumatic deice system for inboard, central and outboard wing and for stabilizers : AIRFRAME DE ICE Propeller electrical deice system : PROP DE ICE Windshield electrical deice system : WINDSHIELD Electrical heating system for both pitots and for the stall warning sensor : PITOT L HTR and PITOT R &...
Page 609: Propeller Deicing
Section 7 Description Pilot's Operating Handbook Propeller deicing Propeller deicing is accomplished through electrical heating of blade roots. This system operates cyclically and alternately on the inboard and outboard zones of all blades. Each cycle is 180 seconds long. The system operation is correct when green warning light located above PROP DE ICE switch illuminates.
Page 610: Heating Of Pitots And Stall Warning Sensor (Pitot L Htr And Pitot R & Stall Htr)
Section 7 Description Pilot's Operating Handbook Heating of pitots and stall warning sensor (PITOT L HTR and PITOT R & STALL HTR) The two pitots, which supply ADCs, the airspeed indicator and the stall warning sensor are electrically heated. This deice equipment must be used even during flight into non-icing conditions.
Page 611 Section 7 Description Pilot's Operating Handbook Page 7.13.4 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 612: Miscellaneous Equipment
Section 7 Description Pilot's Operating Handbook 7.14 - Miscellaneous equipment Stall warning system The airplane is equipped with an electrically deiced stall sensor in the leading edge of the right wing. This sensor fitted with a vane is electrically connected to an audible warning.
Page 613: Cabin Fire Extinguisher
Section 7 Description Pilot's Operating Handbook Cabin fire extinguisher The fire extinguisher is located on R.H. front station side panel. A pressure gage allows checking the fire extinguisher condition. Follow the recommendations indicated on the extinguisher. Autopilot Autopilot control panel is located above the MFD. Refer to section 2 Limitations of this POH and to GARMIN Pilot's Guide for further details.
Page 614 Section 7 Description Pilot's Operating Handbook CAUTION ▲ ▲ Reset the ELT after an inadvertent activation. ▲ Reset procedure : Set remote control switch or ELT switch to ON. a) The ELT keeps on transmitting emergency signal. b) On remote control box, red indicator light flashes. On ELT, red indicator light flashes.
Page 615: Flight Deck Information System (Fs 210), If Installed
Section 7 Description Pilot's Operating Handbook A red indicator light located on R.H. side of locator transmitter switch and a buzzer located in the fuselage rear section indicate the emergency locator transmitter is transmitting. CAUTION ▲ ▲ Reset the ELT after an inadvertent activation. ▲...
Page 616: Garmin Integrated Flight Deck (Gifd) Approaches
Section 7 Description Pilot's Operating Handbook GARMIN Integrated Flight Deck (GIFD) approaches The purpose of this section is to provide an overview of the GIFD capabilities and operation related to GIFD Approaches. Detailed descriptions as well as operating instructions of these approaches are provided in the applicable Pilot’s Guide and Cockpit Reference Guide.
Page 617 Section 7 Description Pilot's Operating Handbook During execution of a GPS approach with LNAV/VNAV service levels, while the aircraft is between the FAF and MAP, excessive deviation indicators appear as white vertical lines to indicate an area where the vertical deviation exceeds ±75 feet. If the glide-path indicator is within an area of excessive deviation, the glide-path indicator becomes yellow and the vertical lines also become yellow.
Page 618: Optional Equipment
Section 7 Description Pilot's Operating Handbook Optional equipment For optional equipment such as weather radar, stormscope, SVS or TAWS, refer to section 9 Supplements. Other optional equipment such as radio altimeter or chartview system or TAS are described in the GARMIN Pilot's Guide. ●...
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Page 620 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Section 8 Handling, servicing and maintenance Table of contents General ..........8.1.1 Identification plate .
Page 621 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook 8.10 Utilization by cold weather (- 0°C to - 25°C) or very cold weather (- 25°C to - 40°C) ..... 8.10.1 Page 8.0.2 Edition 0 - October 31, 2013...
Page 622: General
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook - General This section contains the procedures recommended by the manufacturer for the proper ground handling and routine care and servicing of airplane. Also included in this section are the inspection and maintenance requirements which must be followed if your airplane is to retain its performance and dependability.
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Page 624: Identification Plate
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook - Identification plate Any correspondence regarding your airplane should include its serial number. This number together with the model number, type certificate number and production certificate number are stamped on the identification plate attached to the left side of the fuselage beneath the horizontal stabilizer.
Page 625 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.2.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 626: Publications
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook - Publications When the airplane is delivered from the factory, it is supplied with a POH, the GARMIN Integrated Flight Deck Pilot's Guide and supplemental data covering optional equipment installed in the airplane (refer to section 9 Supplements and pilot guides). In addition, the owner may get access to the following publications online : Maintenance Manual Illustrated Parts Catalog...
Page 627 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.3.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 628: Inspection Periods
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook - Inspection periods Refer to regulations in force in the certification country for information concerning preventive maintenance to be carried out. A maintenance manual must be obtained prior to performing any preventive maintenance to make sure that proper procedures are followed.
Page 629 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.4.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 630: Alterations Or Repairs
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook - Alterations or repairs It is essential that the airworthiness authorities be contacted prior to any alterations or repairs on the airplane to make sure that airworthiness of the airplane is not violated. Alterations or repairs must be accomplished by licensed personnel.
Page 631 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.5.2 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 632: Ground Handling
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook - Ground handling ▲ CAUTION ▲ Only move or tow the airplane with someone in the cockpit. ▲ Towing CAUTION ▲ ▲ Using the propeller for ground handling could result in serious damage, especially if pressure or pull is exerted on blade tips.
Page 633: Tie-Down
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook For long term parking, blanking covers (static ports, pitot, engine air inlet, NACAs, exhaust stubs), cockpit cover, tie-downs, wheel chocks, propeller lock and control lock are recommended. In severe weather and high wind conditions, tie the airplane down as outlined in the following paragraph.
Page 634 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Figure 8.6.1 - Turning angle limits Edition 0 - October 31, 2013 Page 8.6.3 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 635: Jacking
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Jacking When it is necessary to jack the airplane off the ground, refer to maintenance manual for specific procedures and equipment required. Leveling Level the airplane as described in maintenance manual. Flyable storage (below 28 days) Airplanes placed in storage for a maximum of 28 days are considered in flyable storage.
Page 636 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Figure 8.6.2 - Control lock device Edition 0 - October 31, 2013 Page 8.6.5 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
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Page 638: Servicing
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook - Servicing Maintenance In addition to the preflight inspection, refer to section 4, Normal procedures, servicing, inspection and test requirements for the airplane are detailed in the maintenance manual. Maintenance manual outlines all items which require servicing, inspection, testing or overhaul.
Page 639: Fuel
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Oil level check To avoid overfilling of oil tank, and high oil consumption, an oil level check is recommended within 30 minutes after engine shutdown. Ideal interval is 15 to 20 minutes. If more than 30 minutes have passed and the dipstick indicates that oil is needed, start the engine and run at LO-IDLE for five minutes, and recheck oil level.
Page 640 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook WARNING ▲ ▲ During all fueling operations, fire fighting equipment must be available ; attach grounding wire to an unpainted metallic part of the airplane. Do not operate any avionics or electrical equipment on the airplane during fueling.
Page 641 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Fuel additives Fuel used must contain an anti-ice additive conforming to MIL-I-27686 or MIL-I-85470 specification. Strict adherence to recommended preflight draining instructions as called for in Section 4 will eliminate any free water accumulations from the tank sumps. While small amounts of water may still remain emulsified in the gasoline, it will normally be consumed and go unnoticed in the operation of the engine.
Page 642 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Prolonged storage of the airplane will result in a water buildup in the fuel which leeches out the additive. An indication of this is when an excessive amount of water accumulates in the fuel tank sumps. The concentration can be checked using a differential refractometer.
Page 643 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Figure 8.7.3 - Additive mixing ratio (EGME or DIEGME) Page 8.7.6 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 644: Landing Gear
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Landing gear Nose gear tire 5.00-5 10 PR - Inflation pressure : 98 psi (6.7 bars) * Main gear tires 18 5.5 10 PR - Inflating pressure : 135 psi (9.32 bars) * Nose gear shock absorber Fill with hydraulic fluid AIR 3520 B (MIL.H5606E) ;...
Page 645: Oxygen
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Oxygen The replenishment device of the oxygen cylinder is installed directly on the cylinder head. It consists of a charging valve and of a pressure gage graduated from 0 to 2000 PSIG. A chart - see figure 8.7.4, located on the inside of the cylinder service door, gives the cylinder charge maximum pressure according to the environment temperature.
Page 646 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Replenishment procedure WARNING ▲ ▲ Make sure that the airplane is fitted with a grounding cable and is properly grounded. The oxygen cart must be electrically bonded to the airplane. Do not operate the airplane electrical switches or connect/disconnect ground power during oxygen system replenishment.
Page 647 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook If the pressure on the oxygen cylinder gage is low : Fill the oxygen cylinder Make sure the area around the oxygen cylinder charging valve is clean. Remove the cap from the charging valve. Make sure the oxygen supply hose is clean and connect it to the charging valve.
Page 648 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Passenger masks repacking instructions CAUTION ▲ ▲ Do not use oil or other petroleum based lubricants on passenger oxygen mask or deployment container. Oil based lubricants are a fire hazard in oxygen-rich environments. Repacking procedures shall be performed by personnel familiar with the instructions and warnings in this document.
Page 649 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Gently fold reservoir bag lengthwise into thirds (outside edges folded inward over center of bag). Do not crease bag. Fold reservoir bag away from breathing valves and into facepiece. Make sure bag does not cover breathing valves.
Page 650 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Coil oxygen tubing inside facepiece over reservoir bag. Connect oxygen tubing to manifold oxygen fitting. WARNING ▲ ▲ Make sure lanyard pin is inserted into correct check valve for mask being installed. Cross connected pins will result in passengers pulling lanyard cords only to initiate oxygen flow to another mask.
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Page 652: Airplane Cleaning And Care
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook - Airplane cleaning and care Windshield and windows The windshield and windows should be cleaned with an airplane windshield cleaner. ● NOTE ● Refer to the maintenance manual for products and procedures to apply. ●...
Page 653: Propeller Care
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Propeller care Preflight inspection of propeller blades for nicks and cleaning them occasionally with a cloth soaked with soapy water to clean off grass and bug stains will assure long blade life.
Page 654: Preparation Of The Airplane (Equipment And Furnishings)
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook - Preparation of the airplane (equipment and furnishings) WARNING ▲ ▲ In any accommodation, make sure access to emergency exit is free. ▲ CAUTION ▲ ▲ Removed equipment items must be stowed in a place which ensures their integrity.
Page 655 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook ● NOTE ● For the R.H. rear seat, backrest tilting handle is located behind backrest. ● Clear the carpet from under the seat to facilitate moving in rails. Unlock seat using seat tilting handle (1) and tilt it forward. Hold the seat in tilted position and unscrew quick links (7) of strap (9) located under L.H.
Page 656 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook If necessary, remove the cabin central carpet. ● NOTE ● If one of two cargo nets must be installed, it is necessary to use the carpet with appropriate cuttings. ● E - Removal of a cabinet ●...
Page 657 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Position the seat and put lock (22) near the color mark (37) made on rail bottom on aisle side. ● NOTE ● The color mark (37) in the rail is aligned with red marks (36). ●...
Page 658 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook B - Preparation Make sure the SOURCE selector is set to OFF and the crash lever is down. If installed, remove the cargo net. Remove intermediate seats – refer to paragraph 1.D. Remove the deflectors (34) maintained with Velcro-type strap.
Page 659 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Pull up and hold L.H. and R.H. rings (2) and turn knobs (8) by 90° in order to insert locks (3) into rail (5) apertures. Make sure the seat is correctly locked on rails (5). Tilt seat forward, hold it and slip strap (9) around the locking control hinge pin.
Page 660 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Description Equipment Action operation Removal Paragraph 1.C. Rear seat Installation Paragraph 2. F. Removal Paragraph 1.D. Intermediate seat Installation Paragraph 1.G. Cargo net Installation Section 7 Table 1 Edition 0 - October 31, 2013 Page 8.9.7 Rev.
Page 661 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Seat tilting handle Ring Lock Rail Backrest tilting handle Quick link Knob Strap Figure 8.9.1 (1/2) - Removal / installation of rear seat Page 8.9.8 Edition 0 - October 31, 2013 Rev.
Page 662 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Figure 8.9.1 (2/2) - Removal / installation of rear seat Edition 0 - October 31, 2013 Page 8.9.9 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 663 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Locking handle Lock Rail Backrest bottom upholstery Figure 8.9.2 - Removal / installation of intermediate seat Page 8.9.10 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 664 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Blanking plug Blanking plug Blanking device assy Deflector Figure 8.9.3 - Cabin comfort - Installation of blanking plugs and deflector Edition 0 - October 31, 2013 Page 8.9.11 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 665 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Deflector Deflector hole Red mark Color mark Figure 8.9.4 - Cabin comfort - Installation of deflector Page 8.9.12 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 666 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook 8.10 - Utilization by cold weather (- 0°C to - 25°C) or very cold weather (- 25°C to - 40°C) ● NOTE ● Check pressure values in a hangar heated at about 15°C with control equipment at room temperature.
Page 667 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Check pressure values and inflate, if necessary, according to following table 1 during operation in cold weather only : OAT (°C) - 40° - 30° - 20° - 10° + 15° Main landing gear shock absorber (13)
Page 668 List of equipment Report NAV No. 34/90-RJ-App 2 From S/N 1000 to S/N 1049, plus S/N 687 The content of this document is the property of DAHER AEROSPACE. It is supplied in confidence and commercial security of its contents must be maintained.
Page 669 List of equipment Pilot's Operating Handbook List of effective pages and validities Original issue of October 31, 2013 From S/N 1000 to S/N 1049, plus S/N 687 Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date Title APR 19 APR 19 APR 19 APR 19 APR 19...
Page 670 List of equipment Pilot's Operating Handbook Intentionally left blank Page 0B Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 671 List of equipment Pilot's Operating Handbook List of amendments Revision 1 dated February 2014 Pages Description All pages Page heading change to introduce the TBM700 trade name associated to the airplane serial numbers concerning the content of this POH : ”TBM850” becomes ”TBM900” Edition 0 - October 31, 2013 Page 0C Rev.
Page 672 List of equipment Pilot's Operating Handbook List of amendments Revision 2 dated October 2014 Pages Description Addition of modification No. MOD70-0319 Integration of TR14 Change of equipment supplier Addition of smoke goggles Addition of paper clips Modification of pilot and front R.H. Seats part numbers Three frequency ELT C406-1: Version F deleted, Version G added Additon of different versions for Portable fire extinguisher unit...
Page 673 List of equipment Pilot's Operating Handbook List of amendments Revision 3 dated June 2016 Pages Description Title Copyright and logo update List of effective pages 0E, 0F List of amendments Addition of ”Pre-MOD70-0407-00D” validity for Aural warning system Edition 0 - October 31, 2013 Page 0E Rev.
Page 674 List of equipment Pilot's Operating Handbook List of amendments Revision 4 dated December 2017 Pages Description Title Copyright List of effective pages List of amendments - Revision 4 All pages Presentation and/or text moving Integration of TR25 Page 0F Edition 0 - October 31, 2013 Rev.
Page 675 List of equipment Pilot's Operating Handbook List of amendments Revision 5 dated April 8, 2019 Pages Description Title Copyright and company identity name change List of effective pages 0G and 0H List of amendments - Revision 5 4 thru 40 Removal of manufacturer data Terminology, text moving and/or presentation Edition 0 - October 31, 2013...
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Page 677 List of equipment Pilot's Operating Handbook Table of contents Page ATA 01 - Specific optional equipment ........ATA 21 - Environmental system .
Page 678 List of equipment Pilot's Operating Handbook The following list contains standard equipment installed on each airplane and available optional equipment. A separate list of equipment of items installed at the factory in your specific airplane is provided in your airplane file. Columns showing weight (in pounds) and arm (in inches) provide the weight and center of gravity location for the equipment.
Page 679 List of equipment Pilot's Operating Handbook List of critical RVSM equipment Equipment listed hereafter, or later approved versions, is required for RVSM operation. Equipment Barometric altimeter : - GDC74B (Air data computer) P/N 011-01110-00 - GDU1XXX (Display) P/N 011-00916-00 or P/N 011-01108-00 Autopilot Altitude Hold function : - GMC710 (AFCS mode controller)
Page 680: Specific Optional Equipment
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 01 - Specific optional equipment 01026A Flight ceiling at 31000 ft Page 4 Edition 0 - October 31, 2013 Rev.
Page 681: Environmental System
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 21 - Environmental system General Air System Controller (GASC) 1.98 311.02 82024A040601 (0.900) (7.900) 21-20 - Distribution Mixing unit 9723A010001 0.53 151.57...
Page 682 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) Shut-off valve 4589A010001 2.37 114.17 (1.075) (2.900) Intermediate pressure sensor 93557A010001 0.33 110.24 (0.150) (2.800) Overheat thermal switch A042010300-5 0.18 110.24 (0.080)
Page 683 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) Cockpit ventilated sensor 92279A010002 0.18 182.09 (0.080) (4.625) Cabin ventilated sensor 92279A010002 0.18 250.00 (0.080) (6.350) Edition 0 - October 31, 2013 Page 7 Rev.
Page 684: Auto Flight
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 22 - Auto flight 0305-22 Upgrading of AFCS GFC 700 composed of : - Pitch servo GSA 81 + Servo mount GSM 86 4.08 247.40 (1.85)
Page 685: Communications
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 23 - Communications 0176-00A Dual audio system with integrated Marker Beacon 2.59 153.35 Receiver # 1 GMA 1347C (1.17) (3.895) 0176-00A...
Page 686 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 0331-23 Weather Data Link and Satellite Phone GSR 56 3.80 58.00 (1.736) (1.474) Post-MOD70-0319 - Version C : with antenna CI 490-1 (GSR unit support pre-installed) - Version D : with antenna CI 490-1 (Whole capability pre-installed)
Page 687: Electrical Power
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 24 - Electrical power 24-30 - DC generation 0234-24 Electric power system (EPS) 1408-1-1 14.330 128.15 (6.500) (3.255) Stand-by alternator ES10024B-5...
Page 688: Equipment And Furnishings
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 25 - Equipment and furnishings 25004D Leather upholstering - version D ”Autolux” 6.614 212.60 (3.000) (5.400) 0386-25 Leather upholstering ”Vulcain”...
Page 689 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) - 12 VDC servicing plugs unit (Qty : 2 - one in the 3.31 195.28 cockpit, one in the cabin), of which : (1.500) (4.960) 28-5VDC Converter USB-04-13...
Page 690 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 25-61 - Emergency locator transmitter 25030G Three-frequency emergency locator transmitter 7.77 349.92 C406-1 (with base) (with G1000 system GPS (3.523) (8.888) source) (airplanes equipped with reinforcement), of...
Page 691: Fire Protection
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 26 - Fire protection 26002E Engine fire detection system - capability installation 26002F Engine fire detection system 1.455 96.06 (0.660)
Page 692: Flight Controls
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 27 - Flight controls 27-10 - Roll control Roll trim actuator 145700.02 1.543 212.60 (0.700) (5.400) 27-20 - Yaw control Rudder trim actuator 145700.02 1.543...
Page 693: Fuel System
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 28 - Fuel system 28-20 - Fuel supply Electric boost pump 1B9-5 4.409 129.92 (2.000) (3.300) Engine driven fuel pump 1127-02 1.543 110.24...
Page 694: Ice And Rain Protection
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 30 - Ice and rain protection Deicer T700A3013003000, 4.189 398.42 L.H. horizontal stabilizer (1.900) (10.120) Deicer T700A3013003001, 4.189 398.42 R.H.
Page 695: Indicating / Recording Systems
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 31 - Indicating / recording systems 31-20 - Independent instruments 31002A Hourmeter 56457-3 (engine running time) 0.551 156.30 (0.250)
Page 696: Landing Gears
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 32 - Landing gears 32-10 - Main landing gear 0190-32 L.H. main landing gear D23767001 53.79 200.39 (24.400) (5.090)
Page 697 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 0409-32 Main tire 18x5.5-10PR 14.396 204.33 (6.530) (5.190) Master cylinder 010-07802 0.882 145.67 (0.400) (3.700) Nose tire 5.00-5-10PR TL MICHELIN 5.600 89.57...
Page 698: Lights
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 33 - Lights 33-10 - Instrument panel lighting Instruments emergency lighting 2240-3 0.110 181.10 (0.050) (4.600) 0372-33 Back lighted panels 2.132...
Page 699 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) - R.H. navigation/strobe/recognition lights 0.499 184.29 01-0771170-01 (0.227) (4.681) - Rear tail navigation/strobe lights 0.499 444.21 01-0790667-00 (0.227) (11.283)
Page 700: Navigation
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 34 - Navigation 34-11 - Air data systems Lift transducer 799-13 0.882 173.23 (0.400) (4.400) Pitot L heated probe AN 5812-1) 0.750 200.79 (0.340)
Page 701 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 0176-00A Magnetometer # 1 GMU 44 0.48 180.98 (0.22) (4.597) 0176-00A Magnetometer # 2 GMU 44 0.48 180.98 (0.22)
Page 702 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) - Integrated Avionics Unit # 2 GIA 63W 7.21 149.37 (3.27) (3.794) - MFD remote controller GCU 475 0.82 157.83 (0.37)
Page 703 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) - Transmitting antenna S67-2002 0.300 182.09 (0.136) (4.625) - Receiving antenna S67-2002 0.300 205.83 (0.136) (5.228) 34-44 - Traffic advisory system 0176-00F G1000 TAWS system...
Page 704 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 34-53 - Transponder 0176-00D Transponder # 1 GTX 33D - Mode S diversity 4.12 149.65 (1.87) (3.801) + Antenna KA 61 (under fuselage) 0.40...
Page 705 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 34-54 - Automatic Direction Finder (ADF) 0176-00H ADF RA 3500 system, of which : 7.61 214.65 (3.45) (5.452) - Receiver RA3502 P/N 0505.757-912...
Page 706: Oxygen
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 35 - Oxygen 0207-00 Gaseous oxygen system 22.73 226.77 (10.310) (5.760) Page 30 Edition 0 - October 31, 2013 Rev.
Page 707: Vacuum
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 37 - Vacuum Air ejector valve 19E17-5A 0.661 116.14 (0.300) (2.950) Regulator and relief valve 38E-96-2D 1.323 116.14 (0.600)
Page 708: Information Systems
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 46 - Information systems 0459-46B Flight stream transceiver FS 210 0.264 151.18 (0.120) (3.840) Page 32 Edition 0 - October 31, 2013 Rev.
Page 709: Doors
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 52 - Doors 52002A ”Pilot” door 44.092 171.26 (20.000) (4.350) 0320-52A New ”Pilot” door 44.864 173.23 Up to S/N 1006 (20.350) (4.400)
Page 710: Windows
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 56 - Windows 56001A Deiced R.H. Windshield 158.27 Δ1.764 (Δ 0.800) (4.020) Page 34 Edition 0 - October 31, 2013 Rev.
Page 711: Wings
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 57 - Wings 57001A Utilization on runways covered Δ- 7.716 200.00 with melting snow (Δ- 3.500) (5.080) Edition 0 - October 31, 2013 Page 35...
Page 712: Propeller
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 61 - Propeller 61-10 - Propeller assembly Propeller (4-blade) HC-E4N.3 / E 9083 S (K) 154.76 43.11 + spinner 104553P (70.20)
Page 713: Power Plant
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 71 - Power plant Turboprop engine PT6 A-66D 497.30 79.72 (226.00) (2.025) Top silentblocks 95007-16 (Qty 2) 2.647 79.72 (1.201)
Page 714: Engine Indicating
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 77 - Engine indicating Compressor turbine tacho-generator (Ng) 0.981 108.27 MIL-G-26611C GEU-7/A (0.445) (2.750) Propeller tacho-generator (Np) 0.981 55.12 MIL-G-26611 GEU-7/A...
Page 715: Lubrication
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 79 - Lubrication 79-20 - Distribution Oil cooler L8538233 10.472 90.55 (4.750) (2.300) 79-30 - Indicating 79001A Oil pressure transmitter 8107-400-00-10 0.441...
Page 716 List of equipment Pilot's Operating Handbook Intentionally left blank Page 40 Edition 0 - October 31, 2013 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 717 Supplement A Section 9 Pilot's Operating Handbook List of supplements and validities Airplane type * Sup. Edit. Description List of supplements From S/N 1000, plus S/N 687 WX-500 stormscope OPT70-34-056 From S/N 1000, plus S/N 687 Engine fire detection system OPT70-26-002G OPT70-26-002H MOD70-0496-26A...
Page 718 Supplement A Section 9 Pilot's Operating Handbook Airplane type * Sup. Sup. Edit. Edit. Description Description GARMIN GSR56 weather datalink and satellite phone MOD70-0331-23 From S/N 1000, plus S/N 687 Public transportation French-registered airplanes MOD70-0352-11 From S/N 1000, plus S/N 687 with MOD70-0176-00 Five-bladed propeller MOD70-0345-61...
Page 719 Supplement A Section 9 Pilot's Operating Handbook Airplane type * Sup. Sup. Edit. Edit. Description Description Lavatory compartment MOD70-0505-25 From S/N 1000, plus S/N 687 Stick Shaker MOD70-0510-27 Version C From S/N 1000 to S/N 1049, plus S/N 687 GARMIN G1000 NXi retrofit MOD70-0539-00 From S/N 1000 to S/N 1169 Data collection and transmission...
Page 720 Supplement A Section 9 Pilot's Operating Handbook Airplane type * Sup. Sup. Edit. Edit. Description Description Extended large storage cabinet MOD70-0684-25 From S/N 1270 GDR66 COM3 VHF communication MOD70-0722-23 From S/N 1272 900 E0 From S/N 1000 to S/N 1049, plus S/N 687 900 E1 From S/N 1050 910 E0...
Page 721 Supplement 6 WX-500 stormscope Pilot's Operating Handbook SUPPLEMENT WX-500 stormscope Table of contents Page General ..........9.6.2 Limitations .
Page 722 Supplement 6 WX-500 stormscope Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the TBM airplane is equipped with the option WX-500 stormscope. Whenever this supplement refers to the WX-500 Pilot's Guide, it states the one described in section 2.
Page 723 Supplement 6 WX-500 stormscope Pilot's Operating Handbook SECTION 3 Emergency procedures Installation and operation of WX-500 stormscope do not change the basic emergency procedures of the airplane described in section 3 Emergency procedures of the basic POH. SECTION 4 Normal procedures Normal operating procedures of the WX-500 stormscope are outlined in the WX-500 Pilot's Guide.
Page 724 Supplement 6 WX-500 stormscope Pilot's Operating Handbook SECTION 6 Weight and balance The weight and balance hereafter supplement or replace those of the standard airplane described in section 6 Weight and balance of the basic POH when the airplane is equipped with the option WX-500 stormscope. Item Weight OPT70...
Page 725 Supplement 18 Engine fire detection system Pilot's Operating Handbook SUPPLEMENT Engine fire detection system Table of contents Page General ..........9.18.2 Limitations .
Page 726: General
Supplement 18 Engine fire detection system Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the airplane is equipped with the option Engine fire detection system. The general hereafter supplement or replace those of the standard airplane described in section 1 General of the basic POH when the airplane is equipped with the option Engine fire detection system.
Page 727: Emergency Procedures
Supplement 18 Engine fire detection system Pilot's Operating Handbook SECTION 3 Emergency procedures The emergency procedures hereafter supplement or replace those of the standard airplane described in section 3 Emergency procedures of the basic Pilot's Operating Handbook when the airplane is equipped with the option Engine fire detection system. Engine fire on ground Symptoms : ITT increasing, FIRE...
Page 728 Supplement 18 Engine fire detection system Pilot's Operating Handbook Engine fire in flight Symptoms : FIRE Try to confirm the fire warning by looking for other indications such as ITT increase, , smoke from engine cowls or air conditioning system. CAUTION ▲...
Page 729: Normal Procedures
Supplement 18 Engine fire detection system Pilot's Operating Handbook SECTION 4 Normal procedures The normal procedures hereafter supplement or replace those of the standard airplane described in section 4 Normal procedures of the basic Pilot's Operating Handbook when the airplane is equipped with the option Engine fire detection system. Before starting the engine >>...
Page 730 Supplement 18 Engine fire detection system Pilot's Operating Handbook SECTION 6 Weight and balance The weight and balance hereafter supplement or replace those of the standard airplane described in section 6 Weight and balance of the basic Pilot's Operating Handbook when the airplane is equipped with the option Engine fire detection system. Item Weight OPT70...
Page 731 Supplement 18 Engine fire detection system Pilot's Operating Handbook SECTION 7 Description Information hereafter supplement or replace those of the standard airplane described in section 7 Description of the basic Pilot’s Operating Handbook when the airplane is equipped with the option Engine fire detection system. The engine fire detection system enables the monitoring and indication of a fire in the engine area.
Page 732 Supplement 18 Engine fire detection system Pilot's Operating Handbook Intentionally left blank Page 9.18.8 Edition 3 - December 31, 2015 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 733: Weight And Balance
Supplement 45 Mexico specifics Pilot's Operating Handbook SUPPLEMENT Mexico specifics Table of contents Page General ..........9.45.2 Limitations .
Page 734 Supplement 45 Mexico specifics Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the airplane specifics, among others those required by the relevant Certification Authorities (limitations, description and operations necessary to the operation of the TBM airplane). SECTION 2 Limitations The limitations hereafter supplement or replace those of the standard airplane...
Page 735 Supplement 45 Mexico specifics Pilot's Operating Handbook For the small cargo net, on frame C13bis For the large cargo net, on R.H. Side upholstery panel, in the rear baggage compartment Non pressurized FWD baggage compartment On baggage compartment door frame MÁXIMO 50 kg - (110 lbs) PARA INSTRUCCIONES DE CARGA REFIERASE A LOS ”DATOS DE PESO Y BALANCE”...
Page 736 Supplement 45 Mexico specifics Pilot's Operating Handbook On R.H. side at front seat level and on the first rear passengers masks container (R.H. side on the ceiling) On rear passengers masks containers (on R.H. side on the ceiling and left side) On rear passenger's table casing LA MESA DEBE ESTAR GUARDADA DURANTE EL DESPEGUE Y ATERRIZAJE.
Page 737 Supplement 45 Mexico specifics Pilot's Operating Handbook Door internal side On access door On pilot door, if installed On emergency exit handle Edition 2 - April 29, 2016 Page 9.45.5 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 738 Supplement 45 Mexico specifics Pilot's Operating Handbook On landing gear emergency control access door At the upper corner of the window on each side of the cockpit 10 - On cabinet drawer (optional) >> Airplane equipped with coat hanger (Post-MOD70-0557-25) 11 - On the upper edge of the L.H.
Page 739 Supplement 45 Mexico specifics Pilot's Operating Handbook >> Airplane equipped with lavatory compartment (Post-MOD70-0505-25) 12 - On fixed panel, cabin side 13 - On fixed panel, toilet side Edition 2 - April 29, 2016 Page 9.45.7 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 740 Supplement 45 Mexico specifics Pilot's Operating Handbook 14 - On access door, cabin side and toilet side 15 - Behind access door, cabin side and toilet side Page 9.45.8 Edition 2 - April 29, 2016 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 741 Supplement 45 Mexico specifics Pilot's Operating Handbook 16 - Front face of lavatory compartment, near opening / closing switches 17 - On the magazine rack Edition 2 - April 29, 2016 Page 9.45.9 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 742 Supplement 45 Mexico specifics Pilot's Operating Handbook >> All External placards 18 - Under engine cowling and under each wing 19 - Near fuel tank caps Page 9.45.10 Edition 2 - April 29, 2016 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 743 Supplement 45 Mexico specifics Pilot's Operating Handbook 20 - Above brakes hydraulic fluid reservoir against firewall 21 - On langing gear hydraulic fluid reservoir 22 - On fuse box in engine cowling Edition 2 - April 29, 2016 Page 9.45.11 Rev.
Page 744 Supplement 45 Mexico specifics Pilot's Operating Handbook 23 - On internal face of L.H. engine cowling 24 - On front lower portion of firewall L.H. side Page 9.45.12 Edition 2 - April 29, 2016 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 745 Supplement 45 Mexico specifics Pilot's Operating Handbook 25 - On engine cowling, in front of compartment door 26 - On nose gear door 27 - On nose gear leg Edition 2 - April 29, 2016 Page 9.45.13 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 746 Supplement 45 Mexico specifics Pilot's Operating Handbook 28 - On main gear leg 29 - On internal face of the oxygen cylinder service door 30 - On the oxygen service door Page 9.45.14 Edition 2 - April 29, 2016 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 747 Supplement 45 Mexico specifics Pilot's Operating Handbook 31 - Near air data system port 32 - On external side of emergency locator transmitter inspection door 33 - On emergency exit external side Edition 2 - April 29, 2016 Page 9.45.15 Rev.
Page 748 Supplement 45 Mexico specifics Pilot's Operating Handbook 34 - Door external side On pilot door On access door On outer fuselage skin aft of access door and in the cabin forward of access door Page 9.45.16 Edition 2 - April 29, 2016 Rev.
Page 749 Supplement 45 Mexico specifics Pilot's Operating Handbook 35 - On last step of stairs CARGA MÁXIMA SOBRE LA ESCALERA : UNA PERSONA 36 - On R.H. access door jamb Edition 2 - April 29, 2016 Page 9.45.17 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 750 Supplement 45 Mexico specifics Pilot's Operating Handbook SECTION 3 Emergency procedures No specifics SECTION 4 Normal procedures No specifics SECTION 5 Performance No specifics SECTION 6 Weight and balance The weight and balance hereafter supplement or replace those of the standard airplane described in section 6 Weight and balance of the basic POH.
Page 751 Supplement 45 Mexico specifics Pilot's Operating Handbook SECTION 7 Description No specifics SECTION 8 Handling, servicing and maintenance No specifics Edition 2 - April 29, 2016 Page 9.45.19 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 752 Supplement 45 Mexico specifics Pilot's Operating Handbook Intentionally left blank Page 9.45.20 Edition 2 - April 29, 2016 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 753 Supplement 47 GARMIN GWX 70 color weather radar Pilot's Operating Handbook SUPPLEMENT GARMIN GWX 70 color weather radar Table of contents Page General ..........9.47.2 Limitations .
Page 754 Supplement 47 GARMIN GWX 70 color weather radar Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the airplane is equipped with the option GARMIN GWX 70 color weather radar. SECTION 2 Limitations The limitations hereafter supplement or replace those of the standard airplane...
Page 755 Supplement 47 GARMIN GWX 70 color weather radar Pilot's Operating Handbook SECTION 3 Emergency procedures The emergency procedures hereafter supplement or replace those of the standard airplane described in Section 3 Emergency procedures of the basic POH when the airplane is equipped with the option GARMIN GWX 70 color weather radar. ▲...
Page 756 Supplement 47 GARMIN GWX 70 color weather radar Pilot's Operating Handbook SECTION 4 Normal procedures The normal procedures hereafter supplement or replace those of the standard airplane described in Section 4 Normal procedures of the basic POH when the airplane is equipped with the option GARMIN GWX 70 color weather radar. Normal operating procedures for GARMIN GWX 70 color weather radar are outlined in the Pilot's Guide, the references of which are given in section 2 Limitations of this Supplement.
Page 757 Supplement 47 GARMIN GWX 70 color weather radar Pilot's Operating Handbook Shutdown Radar Mode Softkey ......... . . SECTION 5 Performance Installation of GARMIN GWX 70 color weather radar system results in a 5 KIAS...
Page 758 Supplement 47 GARMIN GWX 70 color weather radar Pilot's Operating Handbook SECTION 7 Description Information hereafter supplement or replace those of the standard airplane described in section 7 Description of the basic POH when the airplane is equipped with the option GARMIN GWX 70 color weather radar.
Page 759 Supplement 47 GARMIN GWX 70 color weather radar Pilot's Operating Handbook Figure 9.47.1 (2/2) - GWX 70 weather radar display and controls Edition 1 - October 31, 2013 Page 9.47.7 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 760 Supplement 47 GARMIN GWX 70 color weather radar Pilot's Operating Handbook SECTION 8 Handling, servicing and maintenance Installation and operation of GARMIN GWX 70 color weather radar do not change the basic handling, servicing and maintenance procedures of the airplane described in section 8 Handling, servicing and maintenance of the basic POH.
Page 761 Supplement 49 GARMIN TAWS system Pilot's Operating Handbook SUPPLEMENT GARMIN TAWS system Table of contents Page General ..........9.49.2 Limitations .
Page 762: General
Supplement 49 GARMIN TAWS system Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the airplane is equipped with the option GARMIN TAWS system. The TAWS function enables to detect if the airplane path is in compliance with the overflown terrain relief.
Page 763: Emergency Procedures
Supplement 49 GARMIN TAWS system Pilot's Operating Handbook SECTION 3 Emergency procedures The emergency procedures hereafter supplement or replace those of the standard airplane described in section 3 Emergency procedures of the basic POH when the airplane is equipped with the option GARMIN TAWS system. TAWS FAIL annunciation The TAWS function is not operational.
Page 764: Normal Procedures
Supplement 49 GARMIN TAWS system Pilot's Operating Handbook SECTION 4 Normal procedures The normal procedures hereafter supplement or replace those of the standard airplane described in section 4 Normal Procedures of the basic POH when the TBM airplane is equipped with the option GARMIN TAWS system. Before takeoff ”TAWS System Test OK”...
Page 765 Supplement 49 GARMIN TAWS system Pilot's Operating Handbook 4.2 - Cautions of the TAWS function ”Caution terrain”, ”Caution obstacle”, ”Too low terrain” voice alerts TERRAIN PFD/MFD alert annunciation and CAUTION TERRAIN/OBSTACLE or TOO LOW TERRAIN MFD pop-up alerts light ON. Adjust airplane path in order to make the warning disappear.
Page 766: Performance
Supplement 49 GARMIN TAWS system Pilot's Operating Handbook SECTION 5 Performance Installation and operation of GARMIN TAWS system do not change the basic performance of the airplane described in section 5 Performance of the basic POH. SECTION 6 Weight and balance The weight and balance hereafter supplement or replace those of the standard airplane described in section 6 Weight and balance of the basic POH when the airplane is equipped with the option GARMIN TAWS system.
Page 767: Description
Supplement 49 GARMIN TAWS system Pilot's Operating Handbook SECTION 7 Description Information hereafter supplement or replace those of the standard airplane described in section 7 Description of the basic POH when the TBM airplane is equipped with the option GARMIN TAWS system. >>...
Page 768 Supplement 49 GARMIN TAWS system Pilot's Operating Handbook Imminent Terrain Impact and Imminent Obstacle Impact Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI) alerts are issued when the airplane is below the elevation of a terrain or obstacle cell in the airplane's projected path.
Page 769 Supplement 49 GARMIN TAWS system Pilot's Operating Handbook The aural/displayed messages associated with the FLTA function are described in the table 9.49.2. PFD/MFD MFD Map Page Alert Type TAWS Page Aural Message Pop-Up Alert Annunciation Reduced Required Terrain Clearance ”Terrain, Terrain ; PULL UP TERRAIN - PULL UP Warning (RTC)
Page 770 Supplement 49 GARMIN TAWS system Pilot's Operating Handbook 2. Premature descent alerting A Premature Descent Alert (PDA) is issued when the system detects that the airplane is significantly below the normal approach path to a runway (Figure 9.49.1). PDA alerting begins when the airplane is within 15 Nm of the destination airport. PDA alerting ends when the airplane is either : 0.5 Nm from the runway threshold at an altitude of 125 feet AGL while within 1.0 Nm of the threshold.
Page 771 Supplement 49 GARMIN TAWS system Pilot's Operating Handbook 3. Excessive descent rate alert The purpose of the Excessive Descent Rate (EDR) alert is to provide suitable notification when the airplane is determined to be closing (descending) upon terrain at an excessive speed. Figure 9.49.2 shows the parameters for the alert as defined by TSO-C151b.
Page 772 Supplement 49 GARMIN TAWS system Pilot's Operating Handbook The aural/displayed messages associated with the EDR function are described in the table 9.49.4. PFD/MFD MFD Map Page Alert Type TAWS Page Aural Message Pop-Up Alert Annunciation Excessive Descent Rate Warning ”Pull up” PULL UP PULL UP (EDR) (Red)
Page 773 Supplement 49 GARMIN TAWS system Pilot's Operating Handbook Figure 9.49.3 shows two figures which illustrate the NCR alerting parameters as defined by TSO-C151b. The NCR alert is issued when the altitude loss and height are within the range in the first figure, or when the sink rate (negative vertical speed) and height are within the range in the second figure.
Page 774: Handling, Servicing And Maintenance
Supplement 49 GARMIN TAWS system Pilot's Operating Handbook The aural/displayed messages associated with the NCR function are described in the table 9.49.5. PFD/MFD MFD Map Page Alert Type TAWS Page Aural Message Pop-Up Alert Annunciation Negative Climb Rate Caution ”Don't sink” TERRAIN DONT' SINK (NCR) (Amber)
Page 775 Supplement 50 GARMIN Synthetic Vision System Pilot's Operating Handbook SUPPLEMENT GARMIN Synthetic Vision System Table of contents Page General ..........9.50.2 Limitations .
Page 776 Supplement 50 GARMIN Synthetic Vision System Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the TBM airplane is equipped with the option GARMIN Synthetic Vision System (SVS). The SVS does not replace and is not intended to be used independently of the TAS and/or TAWS system(s).
Page 777 Supplement 50 GARMIN Synthetic Vision System Pilot's Operating Handbook The use of the Synthetic Vision System alone for vertical and/or horizontal navigation, or obstacle or terrain avoidance is prohibited. Pathway boxes must be selected OFF when flying an instrument approach. Turn Pathways OFF when ACTIVATE VECTORS-TO-FINAL, ACTIVATE APPROACH is selected, or the airplane is established on any segment of the approach.
Page 778 Supplement 50 GARMIN Synthetic Vision System Pilot's Operating Handbook >> Airplane with G3000 Flight deck (MOD70-0476-00) From PFD display unit PFD Settings softkey ......... Press Attitude Overlays softkey .
Page 779 Supplement 50 GARMIN Synthetic Vision System Pilot's Operating Handbook SECTION 5 Performance Installation and operation of GARMIN Synthetic Vision System do not change the basic performance of the airplane described in Section 5 Performance of the basic POH. SECTION 6 Weight and balance The weight and balance hereafter supplement or replace those of the standard airplane described in Section 6 Weight and balance of the basic POH when the...
Page 780 Supplement 50 GARMIN Synthetic Vision System Pilot's Operating Handbook SECTION 8 Handling, servicing and maintenance Installation and operation of GARMIN Synthetic Vision System do not change the basic handling, servicing and maintenance procedures of the airplane described in section 8 Handling, servicing and maintenance of the basic POH. Page 9.50.6 Edition 2 - December 31, 2015 Rev.
Page 781 Supplement 56 GARMIN GSR 56 weather datalink Pilot's Operating Handbook and satellite phone SUPPLEMENT GARMIN GSR 56 weather datalink and satellite phone Table of contents Page General ..........9.56.2 Limitations .
Page 782: General
Supplement 56 GARMIN GSR 56 weather datalink and satellite phone Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the TBM airplane is equipped with the option GARMIN GSR 56 weather datalink and satellite phone. Unless otherwise mentioned, whenever a G1000 system is called in this supplement it concerns either a G1000 system or a G1000 NXi system.
Page 783 Supplement 56 GARMIN GSR 56 weather datalink Pilot's Operating Handbook and satellite phone Only the TEL button, on Copilot and Pass Tabs (located in NAV COM/Audio & Radios page) on GTC Touchscreen Controllers can be activated at all time of flight for the front passenger and passengers to have the GSR 56 telephone audio functions.
Page 784: Emergency Procedures
Supplement 56 GARMIN GSR 56 weather datalink and satellite phone Pilot's Operating Handbook SECTION 3 Emergency procedures Installation and operation of GARMIN GSR 56 weather datalink and satellite phone do not change the basic emergency procedures of the airplane described in section 3 Emergency procedures of the basic POH.
Page 785 Supplement 56 GARMIN GSR 56 weather datalink Pilot's Operating Handbook and satellite phone >> Airplane with G1000 Flight deck Before starting engine On L.H. GMA audio panel TEL button ........... . End of procedure.
Page 786 Supplement 56 GARMIN GSR 56 weather datalink and satellite phone Pilot's Operating Handbook >> Airplane with G3000 Flight deck Before starting engine In one of the GTC's NAV COM / Audio & Radios / pilot Tab TEL button ........... . End of procedure.
Page 787: Performance
Supplement 56 GARMIN GSR 56 weather datalink Pilot's Operating Handbook and satellite phone SECTION 5 Performance Installation and operation of GARMIN GSR 56 weather datalink and satellite phone. do not change the basic performance of the airplane described in section 5 Performance of the basic POH.
Page 788: Description
Supplement 56 GARMIN GSR 56 weather datalink and satellite phone Pilot's Operating Handbook SECTION 7 Description Information hereafter supplement or replace those of the standard airplane described in section 7 Description of the basic POH when the airplane is equipped with the option GARMIN GSR 56 weather datalink and satellite phone.
Page 789 Supplement 56 GARMIN GSR 56 weather datalink Pilot's Operating Handbook and satellite phone SECTION 8 Handling, servicing and maintenance Installation and operation of GARMIN GSR 56 weather datalink and satellite phone. do not change the basic handling, servicing and maintenance procedures of the airplane described in section 8 Handling, Servicing and Maintenance of the basic POH.
Page 790 Supplement 56 GARMIN GSR 56 weather datalink and satellite phone Pilot's Operating Handbook Intentionally left blank Page 9.56.10 Edition 3 - December 31, 2015 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 791 Supplement 57 Public transportation for Pilot's Operating Handbook French-registered airplanes SUPPLEMENT Public transportation for French-registered airplanes Table of contents Page General ..........9.57.2 Limitations .
Page 792: General
Supplement 57 Public transportation for French-registered airplanes Pilot's Operating Handbook SECTION 1 General This supplement supplies information necessary for the operation of the TBM airplane when used for Public transportation for French-registered airplanes SECTION 2 Limitations The limitations hereafter supplement or replace those of the standard airplane described in section 2 Limitations of the basic POH when the TBM airplane is used for Public transportation for French-registered airplanes - Placards...
Page 793 Supplement 57 Public transportation for Pilot's Operating Handbook French-registered airplanes On access door - External side On pilot door - External side, if installed On outer fuselage skin aft of access door and in the cabin, forward of access door Edition 1 - October 31, 2013 Page 9.57.3 Rev.
Page 794 Supplement 57 Public transportation for French-registered airplanes Pilot's Operating Handbook On emergency exit handle - Internal side Marking on cover Marking on handle On emergency exit handle - External side On R.H. access door jamb Page 9.57.4 Edition 1 - October 31, 2013 Rev.
Page 795 Supplement 57 Public transportation for Pilot's Operating Handbook French-registered airplanes On last step of stairs On rear passengers masks containers (10) On R.H. side at front seat level and on the first rear passengers masks container (R.H. side on the ceiling) (11) Under window, at L.H.
Page 796: Emergency Procedures
Supplement 57 Public transportation for French-registered airplanes Pilot's Operating Handbook (12) On rear passenger's table edge (13) On the chemical toilet cabinet curtain, if installed SECTION 3 Emergency procedures Use of TBM airplane for Public transportation for French-registered airplanes does not change the basic emergency procedures of the airplane described in section 3 Emergency procedures of the basic POH.
Page 797: Description
Supplement 57 Public transportation for Pilot's Operating Handbook French-registered airplanes SECTION 6 Weight and balance Use of TBM airplane for Public transportation for French-registered airplanes does not change the weight and balance of the airplane described in section 6 Weight and balance of the basic POH.
Page 798 Supplement 57 Public transportation for French-registered airplanes Pilot's Operating Handbook Intentionally left blank Page 9.57.8 Edition 1 - October 31, 2013 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 799: Handling, Servicing And Maintenance
Supplement 58 Five-bladed propeller Pilot's Operating Handbook SUPPLEMENT Five-bladed propeller Table of contents Page General ..........9.58.2 Limitations .
Page 800 Supplement 58 Five-bladed propeller Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the TBM airplane is equipped with the option five-bladed propeller. The general hereafter supplement or replace those of the standard airplane described in section 1 General of the basic POH when the airplane is equipped with the option five-bladed propeller.
Page 801 Supplement 58 Five-bladed propeller Pilot's Operating Handbook SECTION 2 Limitations The limitations hereafter supplement or replace those of the standard airplane described in section 2 Limitations of the basic POH when the TBM airplane is equipped with the option five-bladed propeller. - Powerplant limitations Propeller Number of propellers : 1...
Page 802 Supplement 58 Five-bladed propeller Pilot's Operating Handbook SECTION 4 Normal procedures The normal procedures hereafter supplement those of the standard airplane described in section 4 Normal procedures of the basic POH when the airplane is equipped with the option five-bladed propeller. - Amplified procedures Preflight inspection CAUTION...
Page 803 Supplement 58 Five-bladed propeller Pilot's Operating Handbook - Particular procedures CAUTION ▲ ▲ When engine is shutdown, do not set the “prop de ice” switch to on, damage to the propeller blades could result. ▲ SECTION 5 Performance The performance hereafter supplement or replace those of standard airplane described in section 5 Performance of the basic POH when the airplane is equipped with the option five-bladed propeller.
Page 804 Supplement 58 Five-bladed propeller Pilot's Operating Handbook - Engine operation The following tables or/and the optimum torque indicator must be used during normal operation of the airplane. CAUTION ▲ ▲ It is the responsibility of the operator to make sure that the required version of GARMIN system software is installed prior to using the hereafter engine operation tables.
Page 805 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Example, for conditions : FL = 260 OAT = - 22°C the following tables give the maximum torque to be set. Maximum climb power TRQ setting = 82 % for IAS = 124 KIAS (Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed), cf.
Page 806 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Maximum climb power (FL < 200) - 124 KIAS Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 807 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Maximum climb power (FL > 200) - 124 KIAS Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 808 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Maximum climb power (FL < 200) - 170 KIAS / M 0.40 Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 809 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Maximum climb power (FL > 200) - 170 KIAS / M 0.40 Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 810 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Maximum cruise power (FL < 200) Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Use preferably recommended cruise power. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 811 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Maximum cruise power (FL > 200) Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Use preferably recommended cruise power. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 812 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Normal (recommended) cruise power (FL < 200) Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Table not valid if INERT SEP ON and/or BLEED HI msg ON. T°...
Page 813 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Normal (recommended) cruise power (FL > 200) Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Table not valid if INERT SEP ON and/or BLEED HI msg ON. T°...
Page 814 Supplement 58 Five-bladed propeller Pilot's Operating Handbook - Takeoff distances The following tables give the takeoff distances for several weight configurations. All common information applicable to tables (5.9.1 to 5.9.4) are listed below. Associated conditions Landing gear DN and flaps TO TRQ = 100 % BLEED switch on AUTO Hard, dry and level runway...
Page 815 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Weight : 5512 lbs (2500 kg) Associated condition : 15° of attitude after rotation Rotation speed choice (V (KT) 5000 5500 6000 6500 WEIGHT (LBS) 2200 2500 2800 MASSE (KG) Weight : 5512 lbs (2500 kg) At 50 ft = 91 KIAS - 105 MPH IAS ISA - 35°C ISA - 20°C ISA - 10°C...
Page 816 Supplement 58 Five-bladed propeller EASA Approved Pilot's Operating Handbook Weight : 6579 lbs (2984 kg) Associated condition 15° of attitude after rotation Rotation speed choice (V (KT) 5000 5500 6000 6500 WEIGHT (LBS) 2200 2500 2800 MASSE (KG) Weight : 6579 lbs (2984 kg) At 50 ft = 94 KIAS - 108 MPH IAS ISA - 35°C ISA - 20°C ISA - 10°C...
Page 817 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Weight : 7394 lbs (3354 kg) Associated condition 12°5 of attitude after rotation Rotation speed choice (V (KT) 7394 7500 6500 7000 WEIGHT (LBS) 3000 3200 3354 3400 MASSE (KG) Weight : 7394 lbs (3354 kg) At 50 ft = 99 KIAS - 114 MPH IAS ISA - 35°C ISA - 20°C ISA - 10°C...
Page 818 Supplement 58 Five-bladed propeller Pilot's Operating Handbook 5.10 - Climb performance MXCL - Speeds (IAS = 124 KIAS) Conditions : Maximum climb power TRQ = 100 % Landing gear and flaps UP IAS = 124 KIAS - BLEED switch on AUTO or BLEED HI msg ON Rate of climb (ft/min) Pressure Airplane...
Page 819 Supplement 58 Five-bladed propeller Pilot's Operating Handbook MXCL - Speeds (IAS = 170 KIAS / M 0.40) Conditions : Maximum climb power TRQ = 100 % Landing gear and flaps UP IAS = 170 KIAS / M 0.40 BLEED switch on AUTO or BLEED HI msg ON Rate of climb (ft/min) Pressure Airplane...
Page 820 Supplement 58 Five-bladed propeller Pilot's Operating Handbook MXCL - Time, consumption and climb distance (IAS = 124 KIAS) Conditions : ISA - 20°C Maximum climb power Landing gear and flaps UP IAS = 124 KIAS - BLEED switch on AUTO ●...
Page 821 Supplement 58 Five-bladed propeller Pilot's Operating Handbook MXCL - Time, consumption and climb distance (IAS = 124 KIAS) Conditions : Maximum climb power Landing gear and flaps UP IAS = 124 KIAS - BLEED switch on AUTO ● NOTE ● : Time, consumption and distance from the 50 ft If BLEED HI msg ON : Fuel consumption increased by 2 % Time to climb increased up to 1 % above FL 260...
Page 822 Supplement 58 Five-bladed propeller Pilot's Operating Handbook MXCL - Time, consumption and climb distance (IAS = 124 KIAS) Conditions : ISA + 20°C Maximum climb power Landing gear and flaps UP IAS = 124 KIAS - BLEED switch on AUTO ●...
Page 823 Supplement 58 Five-bladed propeller Pilot's Operating Handbook MXCL - Time, consumption and climb distance (IAS = 170 KIAS / M 0.40) Conditions : ISA - 20°C Maximum climb power Landing gear and flaps UP IAS = 170 KIAS / M 0.40 - BLEED switch on AUTO ●...
Page 824 Supplement 58 Five-bladed propeller Pilot's Operating Handbook MXCL - Time, consumption and climb distance (IAS = 170 KIAS / M 0.40) Conditions : Maximum climb power Landing gear and flaps UP IAS = 170 KIAS / M 0.40 - BLEED switch on AUTO ●...
Page 825 Supplement 58 Five-bladed propeller Pilot's Operating Handbook MXCL - Time, consumption and climb distance (IAS = 170 KIAS / M 0.40) Conditions : ISA + 20°C Maximum climb power Landing gear and flaps UP IAS = 170 KIAS / M 0.40 - BLEED switch on AUTO ●...
Page 826 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Climb performance after go-around Conditions : Landing gear DN and flaps LDG IAS = 90 KIAS Rate of climb (ft/min) Pressure Airplane altitude weight (feet) - 35°C - 20°C - 10°C + 10°C + 20°C + 30°C 1635...
Page 827 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Climb performance - Flaps TO Conditions : Landing gear UP and flaps TO IAS = 110 KIAS Rate of climb (ft/min) Pressure Airplane altitude weight (feet) - 35°C - 20°C - 10°C + 10°C + 20°C + 30°C 2295...
Page 828 Supplement 58 Five-bladed propeller Pilot's Operating Handbook 5.11 - Cruise performance Maximum cruise 7100 lbs 6300 lbs Figure 5.11.1 - Cruise performance (Maximum cruise) Page 9.58.30 Edition 0 - October 31, 2013 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 829 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Maximum cruise Conditions : ISA - 20°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power If BLEED HI msg ON : Fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 830 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Maximum cruise Conditions : ISA - 10°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power If BLEED HI msg ON : Below FL 300 : fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 831 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Maximum cruise Conditions : ISA - 5°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power If BLEED HI msg ON : Below FL 290 : fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 832 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Maximum cruise Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power If BLEED HI msg ON : Below FL 280 : fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 833 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Maximum cruise Conditions : ISA + 5°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power If BLEED HI msg ON : Below FL 270 : fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 834 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Maximum cruise Conditions : ISA + 10°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power If BLEED HI msg ON : Below FL 260 : fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 835 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Maximum cruise Conditions : ISA + 20°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power If BLEED HI msg ON : Below FL 230 : fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 836 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Normal cruise (Recommended) 7100 lbs 6300 lbs Figure 5.11.9 - Cruise performance (Recommended cruise) Page 9.58.38 Edition 0 - October 31, 2013 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 837 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA - 20°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON : Below FL 310 : fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 838 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA - 10°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON : Below FL 290 : fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 839 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA - 5°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON : Below FL 280 : fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 840 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Normal cruise (Recommended) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON : Below FL 270 : fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 841 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA + 5°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON : Below FL 260 : fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 842 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA + 10°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON : Below FL 240 : fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 843 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA + 20°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON : Below FL 210 : fuel flow will increase by 1 %, reduce the torque only to respect the maximum power of 100 %.
Page 844 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Long range cruise (5500 lbs - 2495 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure...
Page 845 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Long range cruise (5500 lbs - 2495 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure...
Page 846 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Long range cruise (6300 lbs - 2858 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure...
Page 847 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Long range cruise (6300 lbs - 2858 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure...
Page 848 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Long range cruise (7100 lbs - 3220 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure...
Page 849 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Long range cruise (7100 lbs - 3220 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure...
Page 850 Supplement 58 Five-bladed propeller Pilot's Operating Handbook 5.12 - Time, consumption and descent distance Conditions : Power as required to maintain constant Vz Landing gear and flaps UP CAS = 230 KCAS - BLEED switch on AUTO Vz = 1500 ft/min Vz = 2000 ft/min Vz = 2500 ft/min Pressure...
Page 851 Supplement 58 Five-bladed propeller Pilot's Operating Handbook 5.13 - Holding time Conditions : Landing gear and flaps UP IAS = 120 KIAS - BLEED switch on AUTO TRQ ≈ 26 % Fuel used during holding time Pressure Weight 5500 lbs (2495 kg) Weight 6300 lbs (2858 kg) altitude 10 min...
Page 852 Supplement 58 Five-bladed propeller Pilot's Operating Handbook SECTION 6 Weight and balance The weight and balance hereafter supplement or replace those of the standard airplane described in section 6 Weight and balance of the basic POH when the TBM airplane is equipped with the option five-bladed propeller. Item Weight OPT70...
Page 853 Supplement 58 Five-bladed propeller Pilot's Operating Handbook SECTION 7 Description Information hereafter supplement or replace those of the standard airplane described in section 7 Description of the basic POH when the airplane is equipped with the option five-bladed propeller - Powerplant Propeller Airplane is equipped with a composite five-bladed, constant-speed and full-feathering propeller.
Page 854 Supplement 58 Five-bladed propeller Pilot's Operating Handbook Intentionally left blank Page 9.58.56 Edition 0 - October 31, 2013 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 855 Supplement 59 Brazil specifics Pilot's Operating Handbook SUPPLEMENT Brazil specifics Table of contents Page General ..........9.59.2 Limitations .
Page 856 Supplement 59 Brazil specifics Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the airplane specifics, among others those required by the relevant Certification Authorities (limitations, description and operations necessary to the operation of the TBM airplane). SECTION 2 Limitations The limitations hereafter supplement or replace those of the standard airplane...
Page 857 Supplement 59 Brazil specifics Pilot's Operating Handbook - Operation limits When operating the VHF-COMM system in Brazilian air space, the selection of 8.33 kHz in the channels spacing can cause the loss of communication with the Air Traffic Control (ATC). GNSS (GPS/SBAS) navigation system limitations In accordance with Brazilian IS 21-013A, use of GNSS/GPS is prohibited under IFR unless other means of navigation, suitable and approved for the intended route, are...
Page 858 Supplement 59 Brazil specifics Pilot's Operating Handbook For the small cargo net, on frame C13bis For the large cargo net, on R.H. side upholstery panel, in the rear baggage compartment On FWD baggage compartment door frame, non pressurized 50 kg MÁXIMO PARA INSTRUÇÓES DE CARREGAMENTO CONSULTAR A SEÇÃO DE PESO E BALANCEAMENTO DO MANUAL DE VÔO...
Page 859 Supplement 59 Brazil specifics Pilot's Operating Handbook Near fuel tank caps On internal face of L.H. engine cowling Capacidade de óleo 12 l 12,7 qt On rear passenger's table casing A MESA DEVERÁ ESTAR RECOLHIDA PARA DECOLAGEM E POUSO Edition 1 - December 31, 2015 Page 9.59.5 Rev.
Page 860 Supplement 59 Brazil specifics Pilot's Operating Handbook On nose gear door On engine cowling, in front of compartment door - - TOMADA EXTERNA - - 28 VOLTS D.C. NOMINAL - - 800 AMPS CAPACIDADE MÍNIMA PARA PARTIDA - - NÃO EXCEDA 1000 AMPS On pilot door - External side, if installed Page 9.59.6 Edition 1 - December 31, 2015...
Page 861 Supplement 59 Brazil specifics Pilot's Operating Handbook On access door - External side On outer fuselage skin aft of access door and in the cabin forward of access door On access door - Internal side Edition 1 - December 31, 2015 Page 9.59.7 Rev.
Page 862 Supplement 59 Brazil specifics Pilot's Operating Handbook On pilot door - Internal side, if installed On emergency exit handle Marking on cover Marking on handle On last step of stairs MAX. UMA PESSOA NA ESCADA Page 9.59.8 Edition 1 - December 31, 2015 Rev.
Page 863 Supplement 59 Brazil specifics Pilot's Operating Handbook On R.H. access door jamb On R.H. side at front seat level and on the first rear passengers masks container (R.H. side on the ceiling) On rear passengers masks containers Edition 1 - December 31, 2015 Page 9.59.9 Rev.
Page 864 Supplement 59 Brazil specifics Pilot's Operating Handbook On the oxygen service door >> Airplanes equipped with Lavatory compartment (Post-MOD70-0505-25) On fixed panel, cabin side On fixed panel, toilet side Page 9.59.10 Edition 1 - December 31, 2015 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 865 Supplement 59 Brazil specifics Pilot's Operating Handbook On access door, cabin side and toilet side Behind access door, cabin side and toilet side Edition 1 - December 31, 2015 Page 9.59.11 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 866 Supplement 59 Brazil specifics Pilot's Operating Handbook Front face of lavatory compartment, near opening / closing switches On the magazine rack and on side wall of storage volume >> Airplanes equipped with Coat hanger (Post-MOD70-0557-25) On the upper edge of the L.H. Passenger access door panel Page 9.59.12 Edition 1 - December 31, 2015 Rev.
Page 867 Supplement 59 Brazil specifics Pilot's Operating Handbook SECTION 3 Emergency procedures No specifics SECTION 4 Normal procedures No specifics SECTION 5 Performance No specifics SECTION 6 Weight and balance The weight and balance hereafter supplement or replace those of the standard airplane described in section 6 Weight and balance of the basic POH.
Page 868 Supplement 59 Brazil specifics Pilot's Operating Handbook SECTION 7 Description No specifics SECTION 8 Handling, servicing and maintenance No specifics Page 9.59.14 Edition 1 - December 31, 2015 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 869 Supplement 60 ADS-B OUT function Pilot's Operating Handbook SUPPLEMENT ADS-B OUT function Table of contents Page General ..........9.60.2 Limitations .
Page 870 Supplement 60 ADS-B OUT function Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the airplane is equipped with ADS-B OUT function. The ADS-B OUT function is integrated in the optional modifications : MOD70-0264-34 : Garmin GTX 33 Non-Diversity or diversity Mode S transponders with the extended squitter functionality, MOD70-0542-34 : Garmin GTX 3X5 transponders.
Page 871 Supplement 60 ADS-B OUT function Pilot's Operating Handbook SECTION 4 Normal procedures Operation of ADS-B OUT function does not change the normal procedures of the airplane described in section 4 Normal procedures of the basic POH. SECTION 5 Performance Operation of ADS-B OUT function does not change the basic performance of the airplane described in section 5 Performance of the basic POH.
Page 872 Supplement 60 ADS-B OUT function Pilot's Operating Handbook After being informed of ADS-B OUT failure either by XPDR1 ADS-B FAIL message or by Air Traffic Control, it is possible to disable ADS-B OUT function by selecting transponder 2 (if installed). >>...
Page 873 Supplement 62 Flight envelope protection Pilot's Operating Handbook SUPPLEMENT Flight envelope protection Table of contents Page General ..........9.62.2 Limitations .
Page 874 Supplement 62 Flight envelope protection Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the airplane is equipped with Flight envelope protection. The flight envelope protection may be : Option No.
Page 875 Supplement 62 Flight envelope protection Pilot's Operating Handbook SECTION 3 Emergency procedures Information hereafter supplement or replace those of the standard airplane described in section 3 Emergency Procedures of the basic POH. - Electrical system >> From S/N 1000 to S/N 1105, plus S/N 687 Figure 3.9.1 - Partial electrical distribution of bus bars >>...
Page 876 Supplement 62 Flight envelope protection Pilot's Operating Handbook 3.12 - Miscellaneous Inadvertent spins WARNING ▲ ▲ Voluntary spins are prohibited. ▲ AP / TRIM DISC push-button ... . . Press and hold until recovery Control wheel .
Page 877 Supplement 62 Flight envelope protection Pilot's Operating Handbook USP ACTIVE Do not disconnect AP Increase power up to 50 % minimum Manage the flight ● NOTE ● Stall warning may be triggered but AP will remain ON ● End of procedure. >>...
Page 878 Supplement 62 Flight envelope protection Pilot's Operating Handbook ESP DEGRADED - AOA Indicates AoA protection at low speed is inoperative. Maintain airspeed above 1.3 Vs FLAPS UP 105 < IAS < 266 KIAS FLAPS TO 100 < IAS < 178 KIAS FLAPS LDG 85 <...
Page 879 Supplement 62 Flight envelope protection Pilot's Operating Handbook SECTION 4 Normal procedures Information hereafter supplement or replace those of the standard airplane described in section 4 Normal Procedures of the basic POH. 4.4 - AMPLIFIED PROCEDURES Go-around with AP OFF GO AROUND push-button .
Page 880 Supplement 62 Flight envelope protection Pilot's Operating Handbook Go-around with AP OFF ► Continuing >> Weight above 6579 lbs (2984 kg) If speed has been maintained at 85 KIAS or more and TRQ 100 %, select flaps to TO position as soon as the 10° Up attitude has been attained. When the vertical speed is positive and when airspeed is at or above 90 KIAS : LANDING GEAR lever .
Page 881 Supplement 62 Flight envelope protection Pilot's Operating Handbook Go-around with AP ON GO AROUND push-button ........Press AP remains ON with the flight director moving up to + 10°...
Page 882 Supplement 62 Flight envelope protection Pilot's Operating Handbook 4.5 - Particular procedures Flight into known icing conditions CAUTION ▲ ▲ The stall warning system does not function properly in icing conditions and should not be relied upon to provide adequate stall warning in icing conditions and after leaving icing conditions, if ice accretion remains on the airplane.
Page 883 Supplement 62 Flight envelope protection Pilot's Operating Handbook SECTION 6 Weight and balance >> From S/N 1000 to S/N 1105, plus S/N 687 Information hereafter supplement or replace those of the standard airplane described in section 6 Weight and Balance of the basic POH when the airplane is equipped with the Flight envelope protection.
Page 884 Supplement 62 Flight envelope protection Pilot's Operating Handbook SECTION 7 Description Information hereafter supplement or replace those of the standard airplane described in section 7 Description of the basic POH when the airplane is equipped with the Flight envelope protection. - ELECTRICAL SYSTEM >>...
Page 885 Supplement 62 Flight envelope protection Pilot's Operating Handbook >> From S/N 1106 Figure 7.8.3 - Partial electrical distribution of bus bars Figure 7.8.4 - Partial circuit breaker panel (typical arrangement) Edition 0 - April 15, 2016 Page 9.62.13 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 886 Supplement 62 Flight envelope protection Pilot's Operating Handbook 7.14 - Miscellaneous equipment Stall warning system The stall warning system consists of : an electrically deiced lift transducer, installed in the leading edge of the right wing, an AoA computer, >> From S/N 1000 to S/N 1105, plus S/N 687 the AOA TEST pushbutton located at the bottom of the L.H.
Page 887 Supplement 62 Flight envelope protection Pilot's Operating Handbook >> All The system is operational if a stall aural warning alert is heard on the alarms speaker. For further information concerning the use of the system and its controls, refer to GARMIN Pïlot's guide at the latest issue.
Page 888 Supplement 62 Flight envelope protection Pilot's Operating Handbook Intentionally left blank Page 9.62.16 Edition 0 - April 15, 2016 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 889 Supplement 63 Lavatory compartment Pilot's Operating Handbook SUPPLEMENT Lavatory compartment Table of contents Page General ..........9.63.2 Limitations .
Page 890 Supplement 63 Lavatory compartment Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the TBM airplane is equipped with the option lavatory compartment. SECTION 2 Limitations The limitations hereafter supplement or replace those of the standard airplane described in section 2 Limitations of the basic POH when the TBM airplane is...
Page 891 Supplement 63 Lavatory compartment Pilot's Operating Handbook On fixed panel, toilet side On access door, cabin side and toilet side Behind access door, cabin side and toilet side Edition 1 - November 16, 2016 Page 9.63.3 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 892 Supplement 63 Lavatory compartment Pilot's Operating Handbook Inner face of toilet cover Front face of lavatory compartment, near opening/closing switches On the magazine rack Page 9.63.4 Edition 1 - November 16, 2016 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 893 Supplement 63 Lavatory compartment Pilot's Operating Handbook >> From S/N 1270 - Placards On fixed panel, cabin side On fixed panel, toilet side On access door, cabin side and toilet side Edition 1 - November 16, 2016 Page 9.63.5 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 894 Supplement 63 Lavatory compartment Pilot's Operating Handbook Behind access door, cabin side and toilet side Inner face of toilet cover Front face of lavatory compartment, near opening/closing switches Page 9.63.6 Edition 1 - November 16, 2016 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 895 Supplement 63 Lavatory compartment Pilot's Operating Handbook On the magazine rack SECTION 3 Emergency procedures The emergency procedures hereafter supplement those of the standard airplane described in section 3 Emergency procedures of the basic POH. 3.10 - Pressurization and air conditioning >>...
Page 896 Supplement 63 Lavatory compartment Pilot's Operating Handbook SECTION 4 Normal procedures The normal procedures hereafter supplement or replace those of the standard airplane described in section 4 Normal procedures of the basic POH when the TBM airplane is equipped with the option lavatory compartment. BRIEFING to passengers to be performed before entering the airplane Normal and Emergency stowing operations of the divider.
Page 897 Supplement 63 Lavatory compartment Pilot's Operating Handbook - Determining the new airplane empty weight and balance after application lavatory compartment option ● NOTE ● The new empty weight determination after lavatory compartment installation shall be performed from the 6-seat configuration airplane characteristics ●...
Page 898 Supplement 63 Lavatory compartment Pilot's Operating Handbook >> From S/N 1000 to S/N 1159 ( Arm (m) 4.392 ) − CG (MAC %) = × 100 Moment = Weight x Arm 1.51 Weight Moment Item (kg) (m.kg) (MAC %) Empty Weight (kg) (1a) (1b) (1c)
Page 899 Supplement 63 Lavatory compartment Pilot's Operating Handbook >> From S/N 1160 ( Arm (m) 4.392 ) − CG (MAC %) = × 100 Moment = Weight x Arm 1.51 Weight Moment Item (kg) (m.kg) (MAC %) Empty Weight (kg) (1a) (1b) (1c) Weight and moment variation after lavatory...
Page 900 Supplement 63 Lavatory compartment Pilot's Operating Handbook Using the weight and balance form CAUTION ▲ ▲ Empty weight, arm and CG % position to be considered are the ones from the last weight and balance report issued after the lavatory compartment option installation.
Page 901 Supplement 63 Lavatory compartment Pilot's Operating Handbook Weight and balance form and diagram (m, kg) - only applicable if lavatory compartment is installed >> From S/N 1000 to S/N 1159 ( Arm (m) 4.392 ) − CG (MAC %) = ×...
Page 902 Supplement 63 Lavatory compartment Pilot's Operating Handbook >> From S/N 1160 ( Arm (m) 4.392 ) − CG (MAC %) = × 100 Moment = Weight x Arm 1.51 Weight Moment Item (kg) (m.kg) (MAC %) Empty Weight (kg) Baggage FWD (<...
Page 903 Supplement 63 Lavatory compartment Pilot's Operating Handbook Figure 9.63.1 -- Weight and Balance diagram Edition 1 - November 16, 2016 Page 9.63.15 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 904 Supplement 63 Lavatory compartment Pilot's Operating Handbook Weight and balance form and diagram (in, lbs) - only applicable if lavatory compartment is installed >> From S/N 1000 to S/N 1159 ( Arm (in) 172.93 ) − CG (MAC %) = ×...
Page 905 Supplement 63 Lavatory compartment Pilot's Operating Handbook >> From S/N 1160 ( Arm (in) 172.93 ) − CG (MAC %) = × 100 Moment = Weight x Arm 59.45 Weight Moment Item (lbs) (in) (in.lbs) (MAC %) Empty Weight (lbs) Baggage FWD (<...
Page 906 Supplement 63 Lavatory compartment Pilot's Operating Handbook Figure 9.63.2 -- Weight and Balance diagram Page 9.63.18 Edition 1 - November 16, 2016 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 907 Supplement 63 Lavatory compartment Pilot's Operating Handbook SECTION 7 Description Information hereafter supplement or replace those of the standard airplane described in section 7 Description of the basic POH when the airplane is equipped with the option Lavatory compartment. For operation, refer to equipment User's Guide. The lavatory compartment is installed against right interior upholstery panel, facing large door.
Page 908 Supplement 63 Lavatory compartment Pilot's Operating Handbook Electric connection of the system is performed via a power plug : >> Without optional 12V power plugs (Pre-MOD70-0174-25) 28 volts >> With optional 12V power plugs (Post-MOD70-0174-25) 12 volts >> All The power plug is located on the right hand side upholstery panel. Connection is only accessible when the lavatory compartment structure is unscrewed from the floor and moved slightly aside to access the plug.
Page 909 Supplement 63 Lavatory compartment Pilot's Operating Handbook Figure 9.63.3 (1/2) -- Lavatory compartment Edition 1 - November 16, 2016 Page 9.63.21 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 910 Supplement 63 Lavatory compartment Pilot's Operating Handbook Figure 9.63.3 (2/2) -- Lavatory compartment Page 9.63.22 Edition 1 - November 16, 2016 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 911 Supplement 63 Lavatory compartment Pilot's Operating Handbook SECTION 8 Handling, servicing and maintenance Installation and operation of Lavatory compartment do not change the basic handling, servicing and maintenance procedures of the airplane described in section 8 Handling, servicing and maintenance of the basic POH. Edition 1 - November 16, 2016 Page 9.63.23 Rev.
Page 912 Supplement 63 Lavatory compartment Pilot's Operating Handbook Intentionally left blank Page 9.63.24 Edition 1 - November 16, 2016 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 913 Supplement 64 Stick shaker Pilot's Operating Handbook SUPPLEMENT Stick shaker Table of contents Page General ..........9.64.2 Limitations .
Page 914 Supplement 64 Stick shaker Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the airplane is equipped with the stick shaker. SECTION 2 Limitations Operation of the stick shaker does not change the limitations of the airplane described in section 2 Limitations of the basic POH.
Page 915 Supplement 64 Stick shaker Pilot's Operating Handbook 3.12 - Miscellaneous >> Airplane not equipped with AoA system (MOD70-0423-34) Stall warning sound ● NOTE ● Shaker will vibrate simultaneously with stall warning sound. ● AP/TRIMS switch ........PRESS twice Fly the airplane, wings level and nose down until stall warning stops Power as required...
Page 916 Supplement 64 Stick shaker Pilot's Operating Handbook SECTION 4 Normal procedures Operation of the stick shaker does not change the normal procedures of the airplane described in section 4 Normal procedures of the basic POH. SECTION 5 Performance Operation of the stick shaker does not change the basic performance of the airplane described in section 5 Performance of the basic POH.
Page 917 Supplement 64 Stick shaker Pilot's Operating Handbook SECTION 7 Description Information hereafter supplement or replace those of the standard airplane described in section 7 Description of the basic POH when the airplane is equipped with the stick shaker. 7.3 - Accomodations Before v15.11 GARMIN software (Pre-MOD70-0407-00D) >>...
Page 918 Supplement 64 Stick shaker Pilot's Operating Handbook The HORN TEST push-button allows to test the correct operation of aural warnings : set the SOURCE selector to BATT or GPU, push and hold the HORN TEST push-button : the loud-speakers emit “stall / stall” aural warning alert the shaker vibrates.
Page 919 Supplement 64 Stick shaker Pilot's Operating Handbook Control wheel assembly Elevators Lever assembly, fuselage rear part Elevator bellcrank Rod with presseal connection Lever assembly under floor Pedestal assembly Actuator Stick shaker Figure 7.4.3 - Elevator Edition 1 - May 29, 2017 Page 9.64.7 Rev.
Page 920 Supplement 64 Stick shaker Pilot's Operating Handbook 7.8 - Electrical system Figure 7.8.3 - Partial electrical distribution of bus bars Page 9.64.8 Edition 1 - May 29, 2017 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 921 Supplement 64 Stick shaker Pilot's Operating Handbook Figure 7.8.4 - Partial electrical distribution of bus bars Edition 1 - May 29, 2017 Page 9.64.9 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 922 Supplement 64 Stick shaker Pilot's Operating Handbook 7.14 - Miscellaneous equipment Stall warning system The airplane is equipped with an electrically deiced stall sensor in the leading edge of the right wing. This sensor fitted with a vane is electrically connected to an audible warning.
Page 923 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook SUPPLEMENT GARMIN G1000 NXi retrofit Table of contents Page General ..........9.66.2 Limitations .
Page 924 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the airplane is equipped with GARMIN G1000 NXi retrofit. Whenever this Supplement refers to the GARMIN Integrated Flight Deck Pilot's Guide, it states the one described in section 2.1.
Page 925 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook SECTION 3 Emergency procedures The emergency procedures hereafter supplement or replace those of the standard airplane described in section 3 Emergency procedures of the basic POH when the airplane is equipped with GARMIN G1000 NXi retrofit. Table of contents ●...
Page 926 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook 3.12 - MISCELLANEOUS CARGO DOOR Indicates that front cargo door is open. On ground : Check and close the door. In flight : ► Fly the airplane ◄ Airspeed ..........Reduce To minimum available ►...
Page 927 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook GPS approach alarm limits exceeded During a GPS LPV, LNAV/VNAV, or LNAV+V approach, if the Horizontal or Vertical alarm limits are exceeded, the GARMIN System will downgrade the approach. This will be annunciated by APR DWNGRADE and by an annunciation change on the HSI from LPV, L/VNAV, or LNAV+V to LNAV.
Page 928 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook AHRS failure Symptoms : Autopilot is disconnected On PFD(s) : Comparator window and/or and/or annunciation(s) On PFD(s) : Reversionary sensor window BOTH ON AHRS1 BOTH ON AHRS2 annunciation Lost systems : AHRS1 or AHRS2 Autopilot (AP) Systems still operative :...
Page 929 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook AHRS failure ► Continuing If all annunciations go off, refer to following condition. BOTH ON AHRS1 BOTH ON AHRS2 annunciation not associated to and/or and/or annunciation(s) : PFD1 and PFD2 SENSOR softkeys .
Page 930 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook ADC failure Symptoms : On PFD(s) : Comparator window and/or annunciation(s) On PFD(s) : Reversionary sensor window BOTH ON ADC1 BOTH ON ADC2 annunciation Lost systems : ADC1 or ADC2 Actions : Autopilot is still operative.
Page 931 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook ABORT APR Indicates a loss of GPS navigation. Perform procedure ..........Go-around Refer to chapter 4.4 of the basic POH End of procedure.
Page 932 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook XPDR1 FAIL XPDR2 FAIL Indicates transponder # 1 [or transponder # 2] is inoperative. ► Fly the airplane ◄ If transponder # 2 [or transponder # 1] is available : Set transponder # 2 [or transponder # 1] as active. Continue flight.
Page 933 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook TRAFFIC FAIL Indicates that Traffic advisory system is inoperative. ● NOTE ● No active traffic available, but ADSB-IN traffic may still be displayed. ● ► Fly the airplane ◄ Inform maintenance department. End of procedure.
Page 934 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook >> Airplane equipped with GWX70 Weather radar (MOD70-0394-34) GWX FAIL Indicates that GWX weather radar is inoperative. ● NOTE ● No real time weather data available. ● ► Fly the airplane ◄ GWX breaker .
Page 935 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook SECTION 4 Normal procedures Operation of the GARMIN G1000 NXi retrofit does not change the normal procedures of the airplane described in section 4 Normal procedures of the basic POH. SECTION 5 Performance Operation of the GARMIN G1000 NXi retrofit does not change the performance of the airplane described in section 5 Performance of the basic POH.
Page 936 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook SECTION 7 Description Description hereafter supplement or replace those of the standard airplane described in section 7 Description of the basic POH when the airplane is equipped with the GARMIN G1000 NXi retrofit. 7.3 - Accomodations Doors, windows and emergency exit FWD compartment door...
Page 937 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook Each visual approach has two transitions, the straight in transition and the Vectors-to-Final transition. The transitions will be labeled STRAIGHT and VECTORS, respectively. The FMS creates the VISUAL approach waypoints (fixes) based on the runway position and course specified in the navigation database.
Page 938 Supplement 66 GARMIN G1000 NXi retrofit Pilot's Operating Handbook SECTION 8 Handling, servicing and maintenance Operation of GARMIN G1000 NXi retrofit does not change the basic handling, servicing and maintenance of the airplane described in section 8 Handling, servicing and maintenance of the basic POH. Page 9.66.16 Edition 1 - November 9, 2017 Rev.
Page 939 SUPPLEMENT 67 DATA COLLECTION AND PILOT'S OPERATING HANDBOOK TRANSMISSION SYSTEM (FASTBOX) SUPPLEMENT DATA COLLECTION AND TRANSMISSION SYSTEM (FASTBOX) TABLE OF CONTENTS Page GENERAL ..........9.67.2 LIMITATIONS .
Page 940: General
SUPPLEMENT 67 DATA COLLECTION TRANSMISSION SYSTEM PILOT'S OPERATING HANDBOOK (FASTBOX) SECTION 1 GENERAL This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the airplane is equipped with the option DATA COLLECTION AND TRANSMISSION SYSTEM (FASTBOX). SECTION 2 LIMITATIONS Installation and operation of DATA COLLECTION AND TRANSMISSION SYSTEM...
Page 941: Performance
SUPPLEMENT 67 DATA COLLECTION AND PILOT'S OPERATING HANDBOOK TRANSMISSION SYSTEM (FASTBOX) SECTION 5 PERFORMANCE Installation and operation of DATA COLLECTION AND TRANSMISSION SYSTEM (FASTBOX) do not change the basic performance of the airplane described in Section 5 Performance of the basic Pilot's Operating Handbook. SECTION 6 WEIGHT AND BALANCE The weight and balance hereafter supplement or replace those of the standard...
Page 942: Description
SUPPLEMENT 67 DATA COLLECTION TRANSMISSION SYSTEM PILOT'S OPERATING HANDBOOK (FASTBOX) SECTION 7 DESCRIPTION Information hereafter supplement or replace those of the standard airplane described in Section 7 Description of the basic Pilot's Operating Handbook when the airplane is equipped with the DATA COLLECTION AND TRANSMISSION SYSTEM (FASTBOX).
Page 943 Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook SUPPLEMENT Baro-VNAV approaches Table of contents Page General ..........9.69.2 Limitations .
Page 944: General
Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the airplane is equipped with the Baro-VNAV approaches capability. SECTION 2 Limitations The limitations hereafter supplement or replace those of the standard airplane described in section 2 Limitations of the basic POH when the airplane is equipped with...
Page 945 Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook is, as installed in this airplane, complying with the equipment, performance, and functional requirements to conduct RNAV and RNP operations in accordance with the applicable requirements of the reference documents listed in the following table.
Page 946 Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook ICAO Flight Plan Code Approved Approved Reference Reference Phase of flight Phase of flight Operational limitations Operational limitations Notes Notes Item Item Documents Documents Capability Capability Code PBN/ Domestic, RNP 2 GNSS FDE availability Additional com- Offshore,...
Page 947 Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook ICAO Flight Plan Code Approved Approved Reference Reference Phase of flight Phase of flight Operational limitations Operational limitations Notes Notes Item Item Documents Documents Capability Capability Code PBN/ Approach At a minimum, the flight EASA Includes area...
Page 948 Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook Note 1 FDE/RAIM availability worldwide can be determined using the WFDE Prediction program, part number 006-A0154- - 01 or later approved version with GARMIN GA36 and GA37 antennas selected, or : - Within the United States, using the FAA's en- - route and terminal RAIM prediction website : www.raimprediction.net, or by contacting a Flight Service Station.
Page 949 Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook GNSS (GPS/SBAS) navigation system limitations Navigation database limitations The pilot must confirm at system initialization that the Navigation database is current. If the AIRAC cycle will change during flight, the pilot must ensure the accuracy of navigation data, including suitability of navigation facilities used to define the routes and procedures for flight.
Page 950 Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook GNSS integrity limitations For flight planning purposes, in areas where SBAS coverage is not available, the pilot must check RAIM availability. The availability of GPS integrity RAIM shall be confirmed for the intended route of flight. In the event of a predicted continuous loss of RAIM of more than five minutes for any part of the intended route of flight, the flight should be delayed, cancelled, or re-routed on a track where RAIM requirements can be met.
Page 951: Emergency Procedures
Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook SECTION 3 Emergency procedures The emergency procedures hereafter supplement or replace those of the standard airplane described in section 3 Emergency procedures of the basic POH when the airplane is equipped with the Baro-VNAV approaches capability. 3.12 - Miscellaneous ABORT APR Indicates a loss of GPS navigation.
Page 952 Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook in AP vertical mode during FD approach with vertical guidance Indicates the loss of vertical integrity signal during LPV or LNAV/VNAV. This may be indicated by an annunciation change on the HSI. Symptoms : AP mode from GP flashing 5 seconds to VDI is flagged and indicates NO GP ►...
Page 953: Normal Procedures
Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook SECTION 4 Normal procedures The normal procedures hereafter supplement or replace those of the standard airplane described in section 4 Normal procedures of the basic POH when the airplane is equipped with the Baro-VNAV approaches capability. - Particular procedures GPS navigation Set up conditions...
Page 954: Performance
Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook SECTION 5 Performance Operation of the airplane equipped with the Baro-VNAV approaches capability does not change the performance of the airplane described in section 5 Performance of the basic POH. SECTION 6 Weight and balance Operation of the airplane equipped with the Baro-VNAV approaches capability does not change the weight and balance of the airplane described in section 6 Weight and balance of the basic POH.
Page 955 Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook There is no guarantee that stepdown fix altitudes will be honored and the crew must level off at the MDA if the runway is not visible. LNAV approaches may be executed with or without SBAS, and advisory vertical guidance is dependent on sufficient GPS vertical error estimates rather than SBAS vertical integrity.
Page 956 Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook Temperature Compensation If SBAS is unavailable or disabled, the GIFD will provide automatic temperature compensated glidepath vertical guidance on approaches that have LNAV/VNAV minima published, or on some approaches that are not authorized for SBAS. No pilot action is required to receive the temperature compensated glide-path when SBAS is not available or allowed.
Page 957 Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook When using barometric altitude for vertical guidance along the final approach segment, temperature compensation is applied whether the temperature is above or below standard temperature. The actual compensated altitude is not displayed to the pilot during an approach.
Page 958: Handling, Servicing And Maintenance
Supplement 69 Baro-VNAV approaches Pilot's Operating Handbook Under certain circumstances, when the GNSS integrity requirement are not met nor approach level is available the approach may be aborted. This is annunciated through an ABORT APR and the service level annunciation being removed from the HSI.
Page 959 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Supplement Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Table of contents Page General ..........
Page 960: General
Section 2 Limitations The information in this section supplements and/or replaces the information in section 2: Limitations of the standard POH when the TBM 900 airplane is equipped with the PT6A-66D Build Spec 1354 engine. 2.3 - Powerplant limitations Normal oil pressure is 105 to 135 psi. Oil pressures under 105 psi are undesirable.
Page 961: Emergency Procedures
Section 3 Emergency procedures The information in this section supplements and/or replaces the information in section 3: Emergency procedures of the standard POH when the TBM 900 airplane is equipped with the PT6A-66D Build Spec 1354 engine. 3.3 - Engine failures...
Page 962: Normal Procedures
Pilot's Operating Handbook Section 4 Normal procedures Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane does not change the normal procedures of the airplane described in section 4: Normal procedures of the standard POH. Section 5...
Page 963 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane The following conditions are given for all the tables (pages 9.77.6 to 9.77.13) : ● NOTE ● Inertial separator must be OFF and BLEED HI msg OFF.
Page 964 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Maximum climb power (FL < 200) - 124 KIAS Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed.
Page 965 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Maximum climb power (FL > 200) - 124 KIAS Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed.
Page 966 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Maximum climb power (FL < 200) - 170 KIAS / M 0.40 Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ●...
Page 967 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Maximum climb power (FL > 200) - 170 KIAS / M 0.40 Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ●...
Page 968 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Maximum cruise power (FL < 200) Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Use preferably recommended cruise power.
Page 969 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Maximum cruise power (FL > 200) Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Use preferably recommended cruise power.
Page 970 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Normal (recommended) cruise power (FL < 200) Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 971 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Normal (recommended) cruise power (FL > 200) Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 972 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook 5.11 - Cruise performance Maximum cruise 7100 lbs 6300 lbs Figure 9.77.6 - Cruise performance (Maximum cruise) Page 9.77.14 Edition 0 - April 15, 2021 Rev.
Page 973 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Maximum cruise Conditions : ISA - 20°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power.
Page 974 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Maximum cruise Conditions : ISA - 10°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power.
Page 975 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Maximum cruise Conditions : ISA - 5°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power.
Page 976 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Maximum cruise Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power.
Page 977 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Maximum cruise Conditions : ISA + 5°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power.
Page 978 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Maximum cruise Conditions : ISA + 10°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power.
Page 979 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Maximum cruise Conditions : ISA + 20°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Use preferably recommended cruise power.
Page 980 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Normal cruise (Recommended) 7100 lbs 6300 lbs Figure 9.77.14 - Cruise performance (Recommended cruise) Page 9.77.22 Edition 0 - April 15, 2021 Rev.
Page 981 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Normal cruise (Recommended) Conditions : ISA - 20°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ●...
Page 982 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA - 10°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ●...
Page 983 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Normal cruise (Recommended) Conditions : ISA - 5°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ●...
Page 984 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Normal cruise (Recommended) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : Power recommended by PRATT & WHITNEY CANADA If BLEED HI msg ON, reduce TRQ by 5 %.
Page 985 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Normal cruise (Recommended) Conditions : ISA + 5°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ●...
Page 986 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Normal cruise (Recommended) Conditions : ISA + 10°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ●...
Page 987 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Normal cruise (Recommended) Conditions : ISA + 20°C Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ●...
Page 988 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Long range cruise (5500 lbs - 2495 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF...
Page 989 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Long range cruise (5500 lbs - 2495 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF...
Page 990 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Long range cruise (6300 lbs - 2858 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF...
Page 991 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Long range cruise (6300 lbs - 2858 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF...
Page 992 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Long range cruise (7100 lbs - 3220 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF...
Page 993 Supplement 77 Installation of the PT6A-66D Build Spec 1354 Pilot's Operating Handbook engine on the TBM 900 airplane Long range cruise (7100 lbs - 3220 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF...
Page 994: Weight And Balance
Section 6 Weight and balance The information in this section supplements and/or replaces the information in section 6: Weight and Balance of the standard POH when the TBM 900 airplane is equipped with the PT6A-66D Build Spec 1354 engine. Item...
Page 995: Description
Section 7 Description The information in this section supplements and/or replaces the information in section 7: Description of the standard POH when the TBM 900 airplane is equipped with the PT6A-66D Build Spec 1354 engine. 7.6 - Powerplant Engine accessories Torque limiter Torque limiter is located on right side of the reduction gearbox.
Page 996 Supplement 77 Installation of the PT6A-66D Build Spec 1354 engine on the TBM 900 airplane Pilot's Operating Handbook Intentionally left blank Page 9.77.38 Edition 0 - April 15, 2021 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

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