Daher TBM 940 Pilot's Information Manual

page of 946

/ 946
Contents
Table of Contents
Bookmarks

Table of Contents

Quick Links

Download this manual

PILOT'S INFORMATION

P/N DMKPIPYEE0 - Edition 0 - Revision 3

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 940

MANUAL

▲

CAUTION

intended for operation of the airplane.

basic Pilot's Operating Handbook.

▲

maintained.

the Copyright.

▲

Printed in FRANCE

Table of Contents

Chapters

Table of Contents

Need help?

Do you have a question about the TBM 940 and is the answer not in the manual?

Questions and answers

Summary of Contents for Daher TBM 940

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 Edition 0 - March 05, 2019 Page 0.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 3 Section 0 Pilot's Operating Handbook List of effective pages and validities Original issue of March 05, 2019 Airplane equipped with MOD70-0649-00 version A P/N DMKFM00EE0R3EN Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date Title MAY 20 0.18 MAY 20 0.19 MAY 20 0.20 MAY 20...
Page 4 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 1.4.2 MAR 19 2.6.6 MAR 19 1.4.3 MAR 19 2.6.7 MAR 19 1.4.4 MAY 20 2.6.8 MAR 19 1.4.5 MAY 20 2.6.9 MAR 19 1.4.6 MAY 20 2.6.10 MAR 19 1.4.7...
Page 5 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 3.0.4 NOV 19 3.6.1 MAR 19 3.0.5 MAY 20 3.6.2 MAR 19 3.0.6 MAR 19 3.6.3 MAR 19 3.6.4 MAR 19 3.1.1 AUG 19 3.1.2 MAR 19 3.7.1 MAR 19 3.1.3...
Page 6 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 3.9.11 NOV 19 3.12.15 NOV 19 3.9.12 MAR 19 3.12.16 MAR 19 3.12.17 MAR 19 3.10.1 MAR 19 3.12.18 MAR 19 3.10.2 MAR 19 3.12.19 MAR 19 3.10.3 MAR 19 3.12.20...
Page 7 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 4.3.8 MAR 19 4.4.30 MAR 19 4.3.9 AUG 19 4.4.31 MAR 19 4.3.10 AUG 19 4.4.32 MAR 19 4.3.11 AUG 19 4.4.33 MAR 19 4.3.12 AUG 19 4.4.34 MAR 19 4.3.13...
Page 8 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 5.4.2 MAR 19 4.5.1 MAR 19 4.5.2 MAR 19 5.5.1 MAR 19 4.5.3 MAR 19 5.5.2 MAR 19 4.5.4 MAR 19 4.5.5 MAR 19 5.6.1 MAR 19 4.5.6 MAR 19 5.6.2...
Page 9 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 5.11.4 NOV 19 6.3.4 MAR 19 5.11.5 NOV 19 5.11.6 NOV 19 6.4.1 MAR 19 5.11.7 NOV 19 6.4.2 MAR 19 5.11.8 NOV 19 6.4.3 MAR 19 5.11.9 MAR 19 6.4.4...
Page 10 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 7.2.8 MAR 19 7.4.1 MAR 19 7.4.2 MAR 19 7.3.1 MAY 20 7.4.3 MAR 19 7.3.2 MAR 19 7.4.4 MAR 19 7.3.3 MAR 19 7.4.5 MAR 19 7.3.4 MAR 19 7.4.6...
Page 11 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 7.6.12 MAR 19 7.9.12 AUG 19 7.6.13 MAR 19 7.9.13 MAY 20 7.6.14 MAR 19 7.9.14 AUG 19 7.6.15 MAR 19 7.9.15 AUG 19 7.6.16 MAR 19 7.9.16 MAY 20 7.6.17...
Page 12 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 8.1.2 MAR 19 7.12.1 NOV 19 7.12.2 AUG 19 8.2.1 MAR 19 7.12.3 AUG 19 8.2.2 MAR 19 7.12.4 AUG 19 7.12.5 AUG 19 8.3.1 MAR 19 7.12.6 AUG 19 8.3.2...
Page 13 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 8.9.3 MAR 19 8.9.4 MAY 20 8.9.5 MAY 20 8.9.6 MAY 20 8.9.7 MAY 20 8.9.8 MAY 20 8.9.9 MAR 19 8.9.10 NOV 19 8.9.11 MAR 19 8.9.12 MAR 19 8.10.1...
Page 14 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date Intentionally left blank Page 0.28 Edition 0 - March 05, 2019 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 15: Table Of Contents
Section 1 General Pilot's Operating Handbook Section 1 General Table of contents General ..........1.1.1 Three view drawing .
Page 16: General
Section 1 General Pilot's Operating Handbook Intentionally left blank 1.0.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 17 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 18 Section 1 General Pilot's Operating Handbook Intentionally left blank Page 1.1.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 19: 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 - March 05, 2019 Page 1.2.1 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 20 Section 1 General Pilot's Operating Handbook Figure 1.2.1 (2/2) - Three view drawing Page 1.2.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 21: 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 22: 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 23: 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 24: 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 25: 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 26: 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 27: 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 28: 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 29 Section 1 General Pilot's Operating Handbook : Emergency Descent Mode EGME : Ethylene glycol monomethyl ether : Engine Indication System EMER : Emergency ESHP : Estimated shaft horsepower : Electronic Stability Protection ESS. BUS TIE : Essential BUS tie EXT. LIGHTS : Exterior lightings °...
Page 30 Section 1 General Pilot's Operating Handbook INERT SEP : Inertial separator INDIC : Indicator in.Hg : Inch of mercury INT. LIGHTS : Interior lightings INSTR. : Instrument : Interturbine temperature : Kilogram : Knot (1 nautical mile/hr - 1852 m/hr) : Kilowatt : Litre L or L.H.
Page 31 Section 1 General Pilot's Operating Handbook MAX RPM : Maximum revolutions per minute : Minimum Descent Altitude : Multi-function Display : Minimum : Minute : Millimetre : Maximum Landing Weight : Maximum Ramp Weight : Message MTOW : Maximum Takeoff Weight MXCR : Maximum Cruise MZFW...
Page 32: Radio-Navigation Abbreviations
Section 1 General Pilot's Operating Handbook : Signalization : Sea level : Serial number : Speed SPKR : Speaker ST - BY : Stand-by STALL HTR : Stall heater : Standard T° : Temperature TEMP : Temperature : Takeoff TURN COORD : Turn coordinator : Gallon U.S : Under Speed Protection...
Page 33 Section 1 General Pilot's Operating Handbook : Course Deviation Indicator : Communications Transceivers : Distance Measuring Equipment : Emergency Locator Transmitter : Fault Detection and Exclusion : Flight Management System GNSS : Global Navigation Satellite System : Global Positioning System : High Frequency : Instrument Flight Rules : Instrument Landing System...
Page 34 Section 1 General Pilot's Operating Handbook : Visual Meteorological Conditions V NAV : Vertical NAVigation : VHF Omnidirectional Range VOR / LOC : VHF Omnidirectional Range LOCalizer WAAS : Wide Area Augmentation System WFDE : WAAS Fault Detection and Exclusion : World Geodetic System : Weather surveillance radar XPDR...
Page 35: 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 36 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 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 37 Section 1 General Pilot's Operating Handbook 1000 Figure 1.5.3 - Inches versus millimetres Edition 0 - March 05, 2019 Page 1.5.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 38 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 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 39: 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 40: 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 41 Section 2 Limitations EASA Approved Pilot's Operating Handbook Section 2 Limitations Table of contents General ..........2.1.1 Airspeed limitations .
Page 42 Section 2 Limitations EASA Approved Pilot's Operating Handbook Altitude operating limits ....... . 2.6.17 In-flight breaker use limits .
Page 43: General
EASA Approved - General TBM 940 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 44 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.1.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 45: 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 46 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.2.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 47: 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 48: 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 Normal oil pressure is 105 to 135 psi.
Page 49: 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 50: 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 51: 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 52 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.4.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 53: 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 54: 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 55: 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 56: 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 57: Homesafe Emergency Function (Post-Mod70-0650-34A)
Section 2 Limitations Pilot's Operating Handbook EASA Approved HomeSafe emergency function (Post-MOD70-0650-34A) HomeSafe must be activated only when the pilot is incapacitated. WARNING ▲ ▲ HomeSafe deactivation must be performed by a pilot : - fully capable of flying the airplane, - fully aware of all the actions the pilot will have to perform to reconfigure the airplane (the initial flight plan in the FMS is lost, the landing gear and flaps positions may not agree with...
Page 58 Section 2 Limitations EASA Approved 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 59 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/ Domestic, RNP 2 GNSS FDE availability Additional com- Offshore, must be verified prior to...
Page 60 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/ Approach At a minimum, the flight EASA Includes area...
Page 61: Gnss (Gps/Sbas) Navigation System Limitations
Section 2 Limitations Pilot's Operating Handbook EASA Approved BOTH ON GPS1 BOTH ON GPS2 Note 2 system annunciation does not necessarily mean that one GPS has failed. Refer to the MFD – GPS STATUS page to determine the state of the unused GPS. General considerations The route planning and WFDE prediction program may be downloaded from the GARMIN website on the internet.
Page 62 Section 2 Limitations EASA Approved Pilot's Operating Handbook RNP APCH including “GPS”, “or GPS”, “RNAV (GPS)” and “RNAV (GNSS)” instrument approaches using the Garmin integrated flight deck are prohibited unless the pilot verifies and uses the current Navigation database. GPS based instrument approaches must be flown in accordance with an approved instrument approach procedure that is loaded from the Navigation database into the flight plan by its name.
Page 63 Section 2 Limitations Pilot's Operating Handbook EASA Approved Approach operations limitations LNAV+V feature is a standard LNAV approach with advisory vertical guidance provided for assistance in maintaining a constant vertical glidepath similar to an ILS glideslope on approach. This guidance is displayed on the PFD in the same location as the ILS glideslope using a magenta diamond.
Page 64: Icing Conditions
Section 2 Limitations EASA Approved Pilot's Operating Handbook Icing conditions Except for certain phases of flight where the POH specifies that deicing boots should not be used (e.g. take-off, final approach, and landing), compliance with the following is required. 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 65: Flap Operating Envelope
Section 2 Limitations Pilot's Operating Handbook EASA Approved During flight, severe icing conditions that exceed those for which the airplane is certificated shall be determined by the following visual cues. If one or more of these visual cues exists, immediately request priority handling from air traffic control to facilitate a route or an altitude change to exit the icing conditions.
Page 66: Weather Radar
Section 2 Limitations EASA Approved Pilot's Operating Handbook Weather radar On ground, the radar radiation is inhibited when the landing gear shock absorbers are compressed. However, it is important to obey the following restrictions : Do not operate the radar during refueling operations or in the vicinity of trucks or containers containing flammables or explosives.
Page 67 Section 2 Limitations Pilot's Operating Handbook EASA Approved Day VFR Pilot instruments Airspeed indicator Sensitive and adjustable altimeter Stand-by heading reference instrument CAS warning and caution messages Oil pressure Low fuel pressure Fuel selector OFF Fuel auxiliary pump ON L.H. and R.H fuel tank low level Non functioning of fuel timer Battery stop Main generator OFF...
Page 68 Section 2 Limitations EASA Approved Pilot's Operating Handbook Engine instruments Torquemeter Propeller tachometer Interturbine temperature indicator (ITT) Gas generator tachometer (Ng) Oil pressure indicator Oil temperature indicator 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...
Page 69 Section 2 Limitations Pilot's Operating Handbook EASA Approved Miscellaneous Seats (each occupant) Belts (each occupant) Straps (each occupant) 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...
Page 70 Section 2 Limitations EASA Approved Pilot's Operating Handbook 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 71: Altitude Operating Limits
Section 2 Limitations Pilot's Operating Handbook EASA Approved 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 72: Enhanced Mode S
Section 2 Limitations EASA Approved Pilot's Operating Handbook 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 73: Chartview System Operating Limitations
Section 2 Limitations Pilot's Operating Handbook EASA Approved 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 74 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.6.20 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 75: 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 76: Weather Radar Limitation
Section 2 Limitations EASA Approved Pilot's Operating Handbook Weather radar limitation Weather radar can be displayed on : PFD 1, PFD 2, MFD, with different indications of mode. Example : PFD 1 : ”SBY” MODE MFD : ”SBY” MODE PFD 2 : ”ACTIVE” MODE CAUTION ▲...
Page 77: Markings
Section 2 Limitations Pilot's Operating Handbook EASA Approved - Markings Airspeed indicator on PFD(s) and on Standby airspeed indicator Markings and their color code significance are shown in fgure 2.8.1. KIAS Marking Significance (Value or range) Red strip Below 65 White strip 65 - 122 Full flap operating range...
Page 78: Engine Instruments
Section 2 Limitations EASA Approved Pilot's Operating Handbook Engine instruments Engine instrument markings and their color code significance are shown in figure 2.8.3. Yellow Green line or arc line or arc line or arc Red line Indication -------------- --------------- --------------- --------------- Minimum Caution...
Page 79: Placards
Section 2 Limitations Pilot's Operating Handbook EASA Approved - Placards Under L.H. front side window On pressurized baggage compartment partition wall Edition 0 - March 05, 2019 Page 2.9.1 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 80 Section 2 Limitations EASA Approved Pilot's Operating Handbook (2)a For the small cargo net, on the right lower upholstery panel (2)b For the large cargo net, on R.H. side upholstery panel, in the rear baggage compartment (2)c On FWD baggage compartment door frame (non pressurized) Page 2.9.2 Edition 0 - March 05, 2019 Rev.
Page 81 Section 2 Limitations Pilot's Operating Handbook EASA Approved On pedestal console On fuel selector Near fuel tank caps Edition 0 - March 05, 2019 Page 2.9.3 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 82 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 Under window, at L.H. Intermediate seat Above passenger's table Page 2.9.4 Edition 0 - March 05, 2019 Rev.
Page 83 Section 2 Limitations Pilot's Operating Handbook EASA Approved (10) Under R.H. control wheel (11) On nose gear door (12) On nose gear leg NOSE LANDING GEAR TIRE PRESSURE : 6,5 bar 94 psi Edition 0 - March 05, 2019 Page 2.9.5 Rev.
Page 84 Section 2 Limitations EASA Approved Pilot's Operating Handbook (13) On main gear leg MAIN LANDING GEAR TIRE PRESSURE : 8,96 bar 130 psi (14) 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 (15)
Page 85 Section 2 Limitations Pilot's Operating Handbook EASA Approved (16) On access door - External side (17) On outer fuselage skin aft of access door (18) In the cabin forward of access door Edition 0 - March 05, 2019 Page 2.9.7 Rev.
Page 86 Section 2 Limitations EASA Approved Pilot's Operating Handbook (19) On access door - Internal side (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 - March 05, 2019 Rev.
Page 87 Section 2 Limitations Pilot's Operating Handbook EASA Approved (22) Above emergency exit door (23) On last step of stairs (24) On rear passengers masks containers (25) On internal face of the oxygen cylinder service door Edition 0 - March 05, 2019 Page 2.9.9 Rev.
Page 88 Section 2 Limitations EASA Approved Pilot's Operating Handbook (26) On the oxygen service door (27) On emergency locator transmitter inspection door >> Airplane equipped with coat hanger (Post-MOD70-0641-25A) (28) On the L.H. rear cargo compartment panel upper edge >> Airplane equipped with coat and headset hanger (Post-MOD70-0683-25F) (29) On the L.H.
Page 89 Section 2 Limitations Pilot's Operating Handbook EASA Approved >> With HomeSafe emergency function (Post-MOD70-0650-34B) (30) Above AFCS control unit Edition 0 - March 05, 2019 Page 2.9.11 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 90 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.9.12 Edition 0 - March 05, 2019 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 91 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Section 3 CAS messages Table of contents ● NOTE ● CAS MESSAGES are in alphabetical order by either Chapter, Section, Paragraph or Supplement ● ABORT APR ........3.12.24 AC CONF MISMATCH .
Page 92 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook FLAPS ASYM ........3.7.3 FUEL IMBALANCE .
Page 93 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook O2 CYL CLOSED ........3.10.10 PARK BRAKE .
Page 94 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.A.4 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 95 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Section 3 Emergency procedures Table of contents General ..........3.1.1 Procedure format .
Page 96 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Fire and smoke ......... 3.5.1 Engine fire on ground .
Page 97 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Fire and smoke ......... 3.5.1 Engine fire on ground .
Page 98 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Electrical system ........3.9.1 BAT AMP .
Page 99 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 3.11 Deicing system ......... 3.11.1 AIRFRAME DEICE FAIL .
Page 100 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Autopilot or electric pitch trim malfunction ....3.12.21 Dual GPS/SBAS failure ( annunciation on HSI) 3.12.22 ABORT APR .
Page 101 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank 3.0.6 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 102: General
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 103 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Red or amber failure warnings are coupled with the lighting of a flashing red indicator/button a fixed amber indicator/button 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.
Page 104: Procedure Format
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 105 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 106: Rejected Takeoff
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved - Rejected takeoff Engine failure at takeoff before rotation THROTTLE ..........Flight IDLE Brakes .
Page 107: Rejected Takeoff For Any Other Reason
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Rejected takeoff for any other reason THROTTLE ..........Flight IDLE Reverse .
Page 108: Engine Failures
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 109 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Engine failure after rotation ► Continuing FUEL TANK SELECTOR ......Before touch down : FLAPS lever .
Page 110: Engine Failure In Flight
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 111: Oil Press Oil Press
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook OIL PRESS OIL PRESS Indicates that oil pressure is below 105 psi. ► Fly the airplane ◄ ► Land as soon as possible ◄ Oil pressure ..........Monitor .
Page 112: Engine Regulation Discrepancy, Power Loss, Throttle Control Loss
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, bad autothrottle behaviour if engaged. ► Fly the airplane ◄ If AT is engaged : .
Page 113 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Engine regulation discrepancy, power loss, throttle control loss ► Continuing Continue the flight. ► Land as soon as possible ◄ If the available power is weak : LANDING GEAR lever ......Only on a final approach glide path 10 - FLAPS lever...
Page 114 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Engine regulation discrepancy, power loss, throttle control loss ► Continuing 18 - Long final or ILS approach ..... . . Establish At IAS <...
Page 115: Governor Control Not Operating
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 116: Engine Does Not Stop On Ground
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 117 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook during takeoff ITT HI Continue takeoff normally. When takeoff procedure is completed : If AT is engaged : Disconnect ......... . THROTTLE Reduce .
Page 118 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved ITT HI Indicates that ITT is between 820°C and 839°C. ▲ CAUTION ▲ Autothrottle engine protection system does not relieve the pilot's responsibility to monitor and control the engine parameters within the limitations.
Page 119: Itt
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Indicates that ITT is more than 840°C. ▲ CAUTION ▲ Autothrottle engine protection system does not relieve the pilot's responsibility to monitor and control the engine parameters within the limitations. ▲ During engine start : Starting procedure .
Page 120: Chip
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 121 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook during takeoff NG HI Continue takeoff normally. When takeoff procedure is completed : If AT is engaged : Disconnect ......... . THROTTLE Reduce .
Page 122 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved NG HI Indicates that Ng speed is between 103 and 104 %. ▲ CAUTION ▲ Autothrottle engine protection system does not relieve the pilot's responsibility to monitor and control the engine parameters within the limitations.
Page 123 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Indicates that Ng speed is more than 104 %. ▲ CAUTION ▲ Autothrottle engine protection system does not relieve the pilot's responsibility to monitor and control the engine parameters within the limitations.
Page 124: Oil Temp
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 125 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.3.18 Edition 0 - March 05, 2019 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 126: Air Start
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 127: Air Start Procedures
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Air start procedures Oxygen masks ..........▲...
Page 128 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 -...
Page 129 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.4.4 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 130: 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 131: Cabin Fire On Ground
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Cabin fire on ground THROTTLE ..........CUT OFF Brakes .
Page 132: 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 133: Fire Or Smoke In Flight
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Fire or smoke in flight Symptoms: smoke or fire is detected in the cockpit or the cabin area. Oxygen masks and goggles ........Refer to chapter 3.12 PASSENGER OXYGEN switch .
Page 134 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Fire or smoke in flight ► Continuing If smoke or fire increases: 11 - EMERGENCY RAM AIR control knob ..... Push 12 - Cabin fire extinguisher...
Page 135 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Fire or smoke in flight ► Continuing ● NOTE ● In this configuration, the battery only supplies power to ESS BUS 1, ESS BUS 2, and BATT BUS, refer to chapter 3.9. ●...
Page 136 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Fire or smoke in flight ► Continuing 22 - Minimum airspeed according to conditions and flaps configuration Normal conditions Icing conditions Flaps UP Flaps TO Flaps LDG 23 - Land normally When airplane is stopped: 24 - THROTTLE...
Page 137 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.5.8 Edition 0 - March 05, 2019 TR30 - July 2023 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 138 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 139 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Smoke elimination Oxygen masks and goggles ........BLEED switch .
Page 140 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.5.6 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 141: Emergency Descents
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved - Emergency descents Emergency descents profiles Edition 0 - March 05, 2019 Page 3.6.1 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 142: Maximum Rate Descent
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Maximum rate descent THROTTLE ..........Flight IDLE Oxygen masks .
Page 143: Maximum Range Descent
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Maximum range descent Oxygen masks ..........THROTTLE .
Page 144 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Maximum range descent ► Continuing 19 - AP / TRIMS ..........20 - DIMMER / CABIN / ACCESS .
Page 145: 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 146: 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 147: 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 148: 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 149: 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 150: 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 151: 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 152 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 153 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 154: 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 155 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Landing with unlocked main landing gear ► Continuing If landing gear drags during landing : 12 - THROTTLE ........CUT OFF 13 - Crash lever...
Page 156: 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 157: 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 158: 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. ▲ AT / AP ..........Disconnect Before 200 ft LANDING GEAR lever...
Page 159: Landing Without Elevator Control
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Landing without elevator control LANDING GEAR lever ......... . FLAPS lever .
Page 160: Ac Conf Mismatch
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook >> With HomeSafe emergency function (Post-MOD70-0650-34A) AC CONF MISMATCH With or without GEAR UNSAFE Indicates that the flaps and/or landing gear positions do not agree with the FLAPS and LANDING GEAR levers positions. Flaps and landing gear configuration .
Page 161: Hs Abn Brakes
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved >> With HomeSafe emergency function (Post-MOD70-0650-34A) HS ABN BRAKES Indicates that the HomeSafe auto-brake servo is operating. When possible, and at the latest before 200 ft on final : AP/TRIM DISC push-button .
Page 162 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.7.18 Edition 0 - March 05, 2019 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 163: Fuel System
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 164 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 165 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 166: 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 167: 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 168: 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 169: Low Lvl Fail L-R
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.
Page 170: Hs Fuel Shutoff
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook >> With HomeSafe emergency function (Post-MOD70-0650-34A) HS FUEL SHUTOFF Indicates that the HomeSafe fuel shut-off valve is closed. WARNING ▲ ▲ This may quickly lead to an engine stop if the right fuel tank is selected.
Page 171: Electrical System
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved - Electrical system 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 ▲...
Page 172: Main Gen
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 173: Low Voltage
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved LOW VOLTAGE Normal functioning with GENERATOR selector on MAIN. Voltmeter voltages ......... .
Page 174: Main Gen And Low Voltage
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 175 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved MAIN GEN LOW VOLTAGE ► Continuing GENERATOR selector ......If altitude >...
Page 176 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook MAIN GEN LOW VOLTAGE ► Continuing WINDSHIELD ......OFF/LDG/TAXI light .
Page 177: Elec Feath Fault
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 178: Bus Bar
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Bus bar Figure 3.9.1 (1/3) - Electrical distribution of bus bars Page 3.9.8 Edition 0 - March 05, 2019 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 179 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 - March 05, 2019 Page 3.9.9 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 180 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Bus bar Figure 3.9.1 (3/3) - Electrical distribution of bus bars Page 3.9.10 Edition 0 - March 05, 2019 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 181: Total Loss Of Electrical Power
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Total loss of electrical power Maintain airplane control. Use the MD 302 for attitude, airspeed, altitude and/or heading. ► Fly the airplane ◄ ► Land as soon as possible ◄ ● NOTE ● Airplane power is provided to the MD302 display for normal operation.
Page 182 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.9.12 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 183: Pressurization And Air Conditioning
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 3.10 - Pressurization and air conditioning PRESSU OFF Possibly due to : system malfunction, BLEED switch on OFF position. If in flight : Oxygen masks ......... BLEED switch .
Page 184 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook PRESSU OFF ► Continuing If on ground : BLEED switch ......... . . Taxi back to apron.
Page 185: Gas Event
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved GAS EVENT Indicates a GASC system malfunction (only displayed 45 sec. after landing) Taxi back to the apron. Perform procedure ........Shutdown Refer to chapter 4.4 Inform maintenance department before next flight.
Page 186: Gas Degraded
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook GAS DEGRADED Indicates a GASC system malfunction Shorten the flight. Inform maintenance department before next flight. End of procedure. Page 3.10.4 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 187: Pressu Backup
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved PRESSU BACKUP 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 188: Cabin Altitude And Use Oxygen Mask
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook CABIN ALTITUDE USE OXYGEN MASK ● NOTE ● CABIN ALTITUDE is followed by USE OXYGEN MASK and 3 voice alerts “Use oxygen mask / Use oxygen mask”. ● Indicates a cabin altitude over 10000 ft ± 500 ft. Pressurization indicator .
Page 189: Edm
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved ● 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 190: Cabin Diff Press
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook CABIN DIFF PRESS Indicates a cabin pressure differential over 6.4 PSI ± 0.2 PSI. Pressurization indicator ........Check If ΔP >...
Page 191: Cabin Not Depressurized After Landing
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Cabin not depressurized after landing If ΔP cabin remains > 0 : DUMP switch ......... Actuate BLEED switch .
Page 192: O2 Cyl Closed
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook O2 CYL CLOSED Indicates that the oxygen cylinder isolation valve is closed. WARNING ▲ ▲ Flight is prohibited with oxygen cylinder closed. ▲ Oxygen cylinder ..........Open End of procedure.
Page 193: Door
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 194: Vacuum Low
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 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 195: Defog Malfunction
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 196 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.10.14 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 197: Deicing System
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 3.11 - Deicing system AIRFRAME DEICE FAIL Symptoms : failure on one of the two pneumatic deicing pulses : ice on wing outboard sections, or, ice on wing inboard sections and stabilizers, AIRFRAME DE ICE status light lit in red.
Page 198: Prop Deice Fail
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook PROP DEICE FAIL Symptoms : PROP DE ICE status light lit in red, propeller vibrations........... . . Disconnect .
Page 199: 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 200: 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, If symptoms result from overheat : DE ICE SYSTEM mode switch ......All deicing systems turn on WINDSHIELD switch .
Page 201: 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 selector ......Set to 12 o’clock position HOT AIR FLOW distributor .
Page 202: 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/R & STALL HTR switch is not ON while the engine is running. PITOT NO HT L Icing conditions may alter airspeed indications provided by ADC1.
Page 203: 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 L/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.
Page 204: Ice Detected
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook ICE DETECTED Indicates that icing conditions have been detected by the ice detector and all deicing systems have been automatically activated. ● NOTE ● ICE DETECTED will only be displayed in AUTO mode. ●...
Page 205: Ice Detection Fail
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved ICE DETECTION FAIL Indicates a failure of the ice detector or of the DE ICE SYSTEM panel printed circuit. DE ICE SYSTEM mode switch ........All deicing systems turn on ●...
Page 206 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.11.10 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 207: Miscellaneous
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 3.12 - Miscellaneous Unsuccessful AT disconnection Symptoms : AT is still engaged and active after having pressed the AT DISC push-button. AT key on AFCS control box ........Press If unsuccessfull to disconnect AT using AT key on AFCS control box : AP/TRIM DISC push-button...
Page 208: Trim Runaway
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Trim Runaway ► Fly the airplane ◄ AP / TRIM DISC push-button ......Press and hold ●...
Page 209: Crack In Cockpit Window Or Window Panel
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Crack in cockpit window or window panel ► Fly the airplane ◄ Descend slowly. Cabin ΔP ..........Reduce By setting Landing Field Elevation to 10000 ft End of procedure.
Page 210: Emergency Exit Use
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 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 211 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 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 212: Emergency Beacon (Elt) Use
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 213: Inadvertent Spins
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Inadvertent spins WARNING ▲ ▲ Voluntary spins are prohibited. ▲ AP / TRIM DISC push-button ... . Press and Hold until recovery Control wheel .
Page 214: Ap Off, Stall Warning
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved AP off, stall warning ● NOTE ● Shaker will vibrate simultaneously with stall warning aural alert. ● Fly the airplane, wings levelled and nose down until stall warning stops........... . As required Return to the desired flight path.
Page 215: Aural Wrn Fail
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook AURAL WRN FAIL Indicates that no aural warning alerts are available. ▲ CAUTION ▲ No aural stall warning. No aural overspeed warning. No landing gear warning. ▲ Maintain airspeeds. Flaps UP 105 <...
Page 216: Aural Wrn 1 Chnl
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved AURAL WRN 1 CHNL ● NOTE ● System switches automatically on the remaining valid aural channel. ● End of procedure. Edition 0 - March 05, 2019 Page 3.12.9 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 217: Esp Fail
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook ESP FAIL Indicates pitch, roll, high speed and AoA protections are inoperative. Autothrottle, including engine protection system, may also be inoperative. ► Fly the airplane ◄ Maintain the airplane inside the flight envelope. Flaps UP 105 <...
Page 218: Esp Degraded - Ias
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved ESP DEGRADED - IAS Indicates high speed protection is inoperative. Autothrottle, including engine protection system, may also be inoperative. ► Fly the airplane ◄ Maintain IAS below 266 KIAS. Continue flight. Inform maintenance department.
Page 219: Esp Degraded - Aoa
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook ESP DEGRADED - AOA Indicates AoA protection at low speed is inoperative. ► Fly the airplane ◄ Maintain airspeed above 1.3Vs. Flaps UP 105 < KIAS < 266 Flaps TO 100 < KIAS < 178 Flaps LDG 85 <...
Page 220: Oxygen Use
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 221 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 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. End of procedure.
Page 222: 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/R & STALL HTR switch ......Check ON If symptoms persist : ALTERNATE STATIC SOURCE selector...
Page 223: 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 224: Cargo Door
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 225: 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 226: 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 227 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 228: 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 229 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 230: 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 231: Abort Apr
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook ABORT APR Indicates a loss of GPS navigation. ► Perform a go-around◄ End of procedure. Page 3.12.24 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 232: Apr Dwngrade
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved APR DWNGRADE Indicates that the GARMIN system downgrades the approach upon navigation system integrity failure during a GPS LPV, LNAV/VNAV. This may be also indicated by an annunciation change on the HSI. System will automatically downgrade to LNAV/VNAV or LNAV.
Page 233: Pit In Ap Vertical Mode During Fd Approach With Vertical Guidance
Section 3 Emergency procedures EASA Approved 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 234: Vdi Vdi
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved on Approach Symptoms : VDI amber or VDI white at bottom of VDI window. ► Fly the airplane ◄ If possible : Use LNAV minimums. If not : ►Perform a go-around◄ End of procedure.
Page 235: Left Pfd Failure
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Left PFD failure ► Fly the airplane ◄ L.H. DISPLAY BACKUP ........Engage TAS system is lost.
Page 236: Ahrs Failure
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved AHRS failure Symptoms : Autopilot is disconnected On PFD(s) : Comparator window and/or and/or annunciation(s), On PFD(s) : Reversionary sensor window annunciation. BOTH ON AHRS1 BOTH ON AHRS2 Lost systems : AHRS1 or AHRS2, Autopilot (AP).
Page 237 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook AHRS failure ► Continuing and/or and/or If all annunciations go off, refer to following condition. annunciation not associated to BOTH ON AHRS1 BOTH ON AHRS2 and/or and/or annunciation(s) : PFD1 and PFD2 SENSOR softkeys .
Page 238: Adc Failure
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved ADC failure Symptoms : On PFD(s) : Comparator window and/or annunciation(s), On PFD(s) : Reversionary sensor window annunciation. BOTH ON ADC1 BOTH ON ADC2 Lost systems : ADC1 or ADC2 Actions : Autopilot and autothrottle are still operative.
Page 239: Mfd Failure
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook MFD failure ● NOTE ● If PFD2 is in fullscreen mode, it will be splitted a few seconds after MFD failure. ● Lost system : Actions : L.H. DISPLAY BACKUP button .
Page 240: Xpdr1 Fail Or Xpdr2 Fail
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 241: Xpdr1 Ads-B Fail Or Xpdr2 Ads-B Fail
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook XPDR1 ADS-B FAIL XPDR2 ADS-B FAIL Indicates ADS-B OUT function of transponder 1 [or transponder 2] is inoperative. Other functions may remain available. ► Fly the airplane ◄ If transponder 2 [or transponder 1] is available : Restore ADS-B OUT function by setting transponder 2 [or transponder 1] as active.
Page 242: Gwx Fail
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved GWX FAIL Indicates that GWX weather radar is inoperative. ● NOTE ● No real time weather data available. ● ► Fly the airplane ◄ WXR breaker ........Check pushed Continue flight by using other weather data source, and adjust flight route.
Page 243: Tcas Fail
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook TCAS FAIL Indicates that Traffic Advisory System is inoperative. ● NOTE ● No active traffic available, but ASDB-IN traffic may still be displayed. ● ► Fly the airplane ◄ Inform maintenance department. End of procedure.
Page 244: Traffic Fail
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved TRAFFIC FAIL Indicates that Traffic Advisory System is inoperative. ● NOTE ● No active traffic available, but ASDB-IN traffic may still be displayed. ● ► Fly the airplane ◄ Inform maintenance department. End of procedure.
Page 245: Homesafe Request
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook >> With HomeSafe emergency function (Post-MOD70-0650-34A) HOMESAFE REQUEST Indicates that HomeSafe is active and will take control and declare an emergency in 15 seconds. If the pilot wants to cancel the HomeSafe request : AP/TRIM DISC push-button .
Page 246: Homesafe Deactivation
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved >> With HomeSafe emergency function (Post-MOD70-0650-34A) HomeSafe deactivation WARNING ▲ ▲ HomeSafe deactivation must be performed by a pilot : - fully capable of flying the airplane, - fully aware of all the actions the pilot will have to perform to reconfigure the airplane (the initial flight plan in the FMS is lost, the landing gear and flaps positions may not agree with LANDING GEAR and FLAPS levers positions).
Page 247 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook >> With HomeSafe emergency function (Post-MOD70-0650-34A) HS CONFIG MODE Indicates that HomeSafe is still in configuration mode after a maintenance operation. Do not start the engine. Inform maintenance department. End of procedure. Page 3.12.40 Edition 0 - March 05, 2019 Rev.
Page 248 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 249 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook In-flight available oxygen quantity ......4.4.36 Before taxiing .
Page 250: 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 251 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 4.1.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 252: 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...
Page 253 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 4.2.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 254: 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 255 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Inside inspection ► Continuing 23 - BLEED ............24 - HOT AIR FLOW .
Page 256: Before Starting Engine
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before starting engine Crash lever ........... . ATIS .
Page 257: 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 258: 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 259: After Engine Start With Gpu
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook After engine start with GPU SOURCE ........... . BATT .
Page 260: Before Taxiing
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before taxiing Stand-by instruments ......... Check DE ICE SYSTEM .
Page 261: Before Line Up
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before line up LDG lights ............
Page 262: Takeoff With High Oat (> Isa + 30°C)
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Takeoff with high OAT (> ISA + 30°C) BLEED ............INERT SEP .
Page 263: Normal Takeoff
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Normal takeoff ADI, HSI, headings ......... . . Check .
Page 264: Short Takeoff
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Short takeoff ADI, HSI, headings ......... . . Check .
Page 265: After Takeoff
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook After takeoff LANDING GEAR ......... Check UP FLAPS .
Page 266: Climb
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Climb ALT SEL ........... Check Altimeters setting .
Page 267: Cruise
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Cruise Altimeters setting ..........Check .
Page 268: Before Descent
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before descent Briefing before approach ........Completed Altimeters setting .
Page 269: Approach
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Approach Altimeters setting (QNH) ........Set / Check Minimums .
Page 270: Final Approach (In Gs) Or Downwind Leg (Vmc)
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Final approach (in GS) or downwind leg (VMC) LDG lights ........... . . LANDING GEAR .
Page 271: Short Final (≈ 500 Ft)
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Short final (≈ 500 ft) LANDING GEAR ..........Check DN and 3 green FLAPS...
Page 272: Runway Clear
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Runway clear TAXI light ............
Page 273: Shutdown
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Shutdown 1 - PARK BRAKE ..........Set / ON 2 - EXT LIGHTS .
Page 274: 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 275 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 276 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 3/16 ► Continuing Initial inside inspection Cockpit A/C switch ........... . SEATS HTRS MASTER switch .
Page 277 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 4/16 ► Continuing 12 - FLAPS lever ........... 13 - FUEL TANK SELECTOR .
Page 278 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 5/16 ► Continuing 25 - STARTER switch ........●...
Page 279 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 6/16 ► Continuing If BATT source : 40 - Voltage ........Check >...
Page 280 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 7/16 ► Continuing DE ICE SYSTEM panel 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 281 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 8/16 ► Continuing 57 - STALL HEAT ON ....... . . Check ON ●...
Page 282 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 9/16 ► Continuing Outside inspection The preflight inspection described in figure 4.4.1 is recommended before each flight. ● NOTE ● If a preflight inspection is performed just after the engine shutdown, be careful because the leading edge of engine air inlet, as well as exhaust stubs may be very hot.
Page 283 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 10/16 ► Continuing 74 - OAT probe ..........Condition 75 - Fuel tank cap...
Page 284 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 11/16 ► Continuing 82 - Fuel tank drain (two on each wing) ......Drain Fuel free of water and contamination ●...
Page 285 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 12/16 ► Continuing Fuselage forward section IV Forward compartment 87 - Inside ..........Check 88 - Door...
Page 286 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 13/16 ► Continuing Air inlets 98 - Main ....... . . No cracks - Unobstructed ●...
Page 287 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 14/16 ► Continuing ● NOTE ● Crush or relieve the shock absorber one time or twice before the inspection to remove possible sticking. ● In case of doubt, request a check of the shock absorber pressure. 105 - R.H.
Page 288 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 15/16 ► Continuing Rear R.H. karman 121 - Oxygen cylinder ......... Open 122 - Oxygen pressure .
Page 289 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 16/16 ► Continuing 132 - Static dischargers ......... . Condition 133 - Vertical stabilizer deicer boots .
Page 290: 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 291 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Inside inspection ► Continuing >> With HomeSafe emergency function (Post-MOD70-0650-34A) ● NOTE ● Inform passengers that HomeSafe emergency function is intended to automatically land the airplane in case of pilot's incapacitation and that the activation button is located on top of instrument panel.
Page 292 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Inside inspection ► Continuing 21 - STARTER switch ..........●...
Page 293 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. ▲ 36 - MAN OVRD control ......Full backward (notched) CAUTION ▲...
Page 294: 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 295 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before starting engine ► Continuing 15 - O2 CYL CLOSED ........Check OFF O2 CYL CLOSED is ON :...
Page 296 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before starting engine ► Continuing 28 - PARK BRAKE ......... . Check ON ●...
Page 297: Engine Start
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Engine start STROBE switch ..........G3000 .
Page 298 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 299 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Engine start ► Continuing Abort starting procedure if : No ignition 10 seconds after having positioned THROTTLE to LO-IDLE, lights on (max ITT < 870°C for more than 20 seconds, < 1000°C for more than 5 seconds), Ng <...
Page 300: 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 301 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 302 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Motoring ► Continuing 23 - STARTER switch ........ABORT Then OFF 24 -...
Page 303: 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 304 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Motoring followed by an engine start ► Continuing 13 - Motor ..........For 30 sec.
Page 305 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 306: 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 307: 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 308 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 309: 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 310: Before Taxiing
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before taxiing Stand-by instruments ......... Check Check de-ice system ●...
Page 311 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before taxiing ► Continuing Increase ≈ 80 % ......... . . To check AIRFRAME DE ICE ●...
Page 312 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before taxiing ► Continuing 16 - Pitch trim ..........UP / DN 17 - Pitch trim...
Page 313 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before taxiing ► Continuing 32 - THROTTLE ......... FEATHER twice Flight IDLE to LO-IDLE then Flight IDLE, twice 33 -...
Page 314: 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 315: 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 316 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before line up ► Continuing Adjust trims for takeoff 16 - Pitch ........... . Adjust inside green index sector, depending on the current balance condition 17 -...
Page 317 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before line up ► Continuing 28 - CAS display ..........Check All messages OFF, PARK BRAKE...
Page 318 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before line up ► Continuing 40 - Rotation airspeed (V ........Check 41 - Pilot's / Passengers' belts...
Page 319: Takeoff With High Oat (> Isa + 30°C)
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Takeoff with high OAT (> ISA + 30°C) ● NOTE ● Autothrottle engine protection system is inhibited below 400 ft AGL. ● BLEED switch ..........INERT SEP switch .
Page 320: Normal Takeoff
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved 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 321 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Normal takeoff ► Continuing 11 - ............100 % ●...
Page 322 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Normal 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 323: 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 324 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Short takeoff ► Continuing 11 - Brakes ........... . Release ●...
Page 325 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. ▲ 18 - Airspeed .
Page 326: After Takeoff
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved After takeoff LANDING GEAR lever ........Check UP FLAPS lever .
Page 327: Climb
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Climb ALT SEL ........... Check Altimeters setting .
Page 328 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Climb ► Continuing A/C panel 11 - TEMP selector ..........Adjust 12 - FUEL gages...
Page 329: Cruise
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Cruise Altimeters setting ..........Check Autopilot .
Page 330 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Cruise ► Continuing ▲ CAUTION ▲ If heavy precipitation, turn IGNITION and INERT SEP switches to ON. ▲ 13 - DE ICE SYSTEM panel ......As required Refer to chapter 4.5 14 -...
Page 331: Before Descent
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before descent Briefing before approach ........Completed Altimeters settings .
Page 332: Approach
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Approach Altimeters settings (QNH) ....... . . Set / Check Minimums .
Page 333: 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 334: 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 335: 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 336: Go-Around With Ap Off
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Go-around with AP OFF GO AROUND push-button ........Press It provides the moving up of the flight director to + 10°...
Page 337 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Go-around with AP OFF ► Continuing When airspeed is at or above 115 KIAS : FLAPS lever ........10 - Climb airspeed .
Page 338: Go-Around With Ap On
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Go-around with AP ON GO AROUND push-button ........Press AP remains ON with the flight director moving up to + 10°...
Page 339: Touch And Go
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Touch and go Before wheels touch : WARNING ▲ ▲ AT engagement is prohibited for touch and go. 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 340 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved 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 341: Runway Clear
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Runway clear Runway clear - airplane stopped ▲ CAUTION ▲ Generator load < 200 amps ▲ TAXI lights ........... . . NAV switch .
Page 342: Shutdown
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Shutdown PARK BRAKE ..........Set ON PARK BRAKE .
Page 343 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Shutdown ► Continuing Fuel system check 17 - AUX BOOST PMP ON ........Check ON Wait for AUX BP operation, an audible operation of the auxiliary booster pump should be heard,...
Page 344 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Shutdown ► Continuing 26 - Turn the control knob to select POWER OFF on the menu and press the control knob to shut down the standby attitude module. End of procedure. Edition 0 - March 05, 2019 Page 4.4.71 Rev.
Page 345: 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 346: 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 347 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 348 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Flight into known icing conditions ► Continuing IGNITION switch ......... . ●...
Page 349 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook 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 350: Flight Into Severe Icing Conditions
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved 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 351: Flight Under Heavy Precipitations
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Flight under heavy precipitations IGNITION switch ..........●...
Page 352: Utilization On Runways Covered With Melting Or Not Tamped Snow
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved 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 353 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization on runways covered with melting or not tamped snow ► Continuing Rotation airspeed ..... Increased by 5 KIAS ●...
Page 354 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved 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 355: Utilization On Icy Or Covered With Tamped Snow Runways 1/2
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook 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 356 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved 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 357 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) ● NOTE ● The procedure hereafter supplements the normal procedures for the airplane use when operating under temperatures between 0°...
Page 358 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 ● 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 359 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 12 - INERT SEP ON ......Check ON 13 - PITOT L/R &...
Page 360 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 21 - PARK BRAKE ........Check OFF ●...
Page 361 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 ● 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 362 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 11 - IGNITION switch ......ON during 30 seconds 12 - IGNITION...
Page 363: Utilization By Cold Weather (0°C To - 25°C) And Very Cold Weather (- 25°C To - 40°C)
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 CAUTION ▲ ▲ When the engine is shut down, the THROTTLE must not be moved into the reverse area.
Page 364: Utilization By Cold Weather (- 0°C To - 25°C) And Very Cold Weather (- 25°C To - 40°C) - Envelope 2
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 When Ng > 50% : CAUTION ▲ ▲ If the starter does not go off automatically, disengage it using the ABORT position of the STARTER switch.
Page 365: Utilization By Cold Weather (- 0°C To - 25°C) And Very Cold Weather (- 25°C To - 40°C) - Envelope 3
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 After engine start : As soon as the current flow is lower than 100 A : A/C panel 46 - A/C switch...
Page 366 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 ● NOTE ● The procedures defined for the Envelope 2 are also applicable for the Envelope 3.
Page 367 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 ► Continuing Landing / After landing / Shutdown / 10 - Perform procedures defined for Envelope 1.
Page 368: Landing Procedure With Strong Headwind Or Crosswind 1/2
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved 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 369 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook 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 370: Utilization On Grass Runway
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved 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 371 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook 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 372: Gps Navigation
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved 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 373 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 4.5.28 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 374 Section 5 Performance Pilot's Operating Handbook Section 5 Performance Table of contents General ..........5.1.1 Noise level .
Page 375 Section 5 Performance Pilot's Operating Handbook 5.10 Climb performance ........5.10.1 MXCL - Speeds (IAS = 124 KIAS) .
Page 376: General
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 - March 05, 2019 Page 5.1.1 Rev.
Page 377 Section 5 Performance EASA Approved Pilot's Operating Handbook Intentionally left blank Page 5.1.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 378: 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...
Page 379 Section 5 Performance EASA Approved Pilot's Operating Handbook Intentionally left blank Page 5.2.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 380: 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 381 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 - March 05, 2019...
Page 382: 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 383 Section 5 Performance Pilot's Operating Handbook Intentionally left blank Page 5.4.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 384: 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...
Page 385 Section 5 Performance Pilot's Operating Handbook Intentionally left blank Page 5.5.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 386: 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 387 Section 5 Performance Pilot's Operating Handbook Intentionally left blank Page 5.6.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 388: 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 - March 05, 2019 Page 5.7.1 Rev.
Page 389 Section 5 Performance Pilot's Operating Handbook Intentionally left blank Page 5.7.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 390: 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 391 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 = 83 % for IAS = 124 KIAS (Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed), cf.
Page 392 Section 5 Performance Pilot's Operating Handbook Intentionally left blank Edition 0 - March 05, 2019 Page 5.8.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 393 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. INERT SEP ON Table not valid if and/or BLEED HI msg ON.
Page 394 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. INERT SEP ON Table not valid if and/or BLEED HI msg ON.
Page 395: 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. INERT SEP ON Table not valid if and/or BLEED HI msg ON.
Page 396: 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. INERT SEP ON Table not valid if and/or BLEED HI msg ON.
Page 397: 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. INERT SEP ON Table not valid if and/or BLEED HI msg ON.
Page 398: 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 399 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 400 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 401 Section 5 Performance Pilot's Operating Handbook Intentionally left blank Page 5.8.12 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 402: 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 403: Weight : 5512 Lbs (2500 Kg)
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 404: Weight : 6579 Lbs (2984 Kg)
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 405: Weight : 7394 Lbs (3354 Kg)
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 406: 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 407: 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 408: Mxcl - Time, Consumption And Climb Distance (Ias = 124 Kias)
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 409 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 410 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 411: Mxcl - Time, Consumption And Climb Distance (Ias = 170 Kias / M 0.40)
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 412 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 413 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 414: 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 415: 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 416: 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 - March 05, 2019 Page 5.11.1 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 417 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 418 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 419 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 420 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 421 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 422 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 423 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 424: 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 - March 05, 2019 Page 5.11.9 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 425 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 426 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 427 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 428 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 429 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 430 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 431 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 432: Long Range Cruise (5500 Lbs - 2495 Kg)
Section 5 Performance Pilot's Operating Handbook Long range cruise (5500 lbs - 2495 kg) Conditions : AT not engaged Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : If AT is engaged, TRQ setting is 50 % everywhere. Legend : OAT : °C...
Page 433 Section 5 Performance Pilot's Operating Handbook Long range cruise (5500 lbs - 2495 kg) Conditions : AT not engaged Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : If AT is engaged, TRQ setting is 50 % everywhere. Legend : OAT : °C...
Page 434: Long Range Cruise (6300 Lbs - 2858 Kg)
Section 5 Performance Pilot's Operating Handbook Long range cruise (6300 lbs - 2858 kg) Conditions : AT not engaged Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : If AT is engaged, TRQ setting is 50 % everywhere. Legend : OAT : °C...
Page 435 Section 5 Performance Pilot's Operating Handbook Long range cruise (6300 lbs - 2858 kg) Conditions : AT not engaged Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : If AT is engaged, TRQ setting is 50 % everywhere. Legend : OAT : °C...
Page 436: Long Range Cruise (7100 Lbs - 3220 Kg)
Section 5 Performance Pilot's Operating Handbook Long range cruise (7100 lbs - 3220 kg) Conditions : AT not engaged Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : If AT is engaged, TRQ setting is 50 % everywhere. Legend : OAT : °C...
Page 437 Section 5 Performance Pilot's Operating Handbook Long range cruise (7100 lbs - 3220 kg) Conditions : AT not engaged Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF ● NOTE ● : If AT is engaged, TRQ setting is 50 % everywhere. Legend : OAT : °C...
Page 438: 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 439 Section 5 Performance Pilot's Operating Handbook Intentionally left blank Page 5.12.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 440: 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 441 Section 5 Performance Pilot's Operating Handbook Intentionally left blank Page 5.13.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 442: 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 443: 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 444: 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 445: 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 446 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 447 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank 6.0.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 448: 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 449 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.1.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 450 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 451 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.2.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 452: 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 453 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 454 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 455 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.3.4 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 456: 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 457: Utilization Of Weight And Balance Graph
Section 6 Weight and balance Pilot's Operating Handbook Utilization of weight and balance graph This procedure determines the airplane weight and balance characteristics for flight. Select the units for the weight and balance determination, either m and kg, or lb and in, and use the dedicated form - see figures 6.4.3 or 6.4.4, appropriate to the chosen units.
Page 458 Section 6 Weight and balance Pilot's Operating Handbook Check that all points are within the weight and balance limits and check that they are vertically aligned. Record these data on your navigation log. Edition 0 - March 05, 2019 Page 6.4.3 Rev.
Page 459: 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 460 Section 6 Weight and balance Pilot's Operating Handbook Weight Item (kg) (1a) Empty weight Baggage (2a) (< 50 kg) (2a) Front seats -15.4 kg per seat (2a) removed * Inter. seats (2a) -21 kg per seat (2a) removed * Rear (2a) bench/net (2a)
Page 461: 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 Page 6.4.6 Edition 0 - March 05, 2019...
Page 462 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 Edition 0 - March 05, 2019 Page 6.4.7 Rev.
Page 463: 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 464 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.3 - Weight and balance diagram Edition 0 - March 05, 2019 Page 6.4.9 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 465: 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 466 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.4 - Weight and balance diagram Edition 0 - March 05, 2019 Page 6.4.11 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 467 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.4.12 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 468: 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 469 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 470 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.5 - Loading sample (in kg and m) Edition 0 - March 05, 2019 Page 6.4.15 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 471 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.4.16 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 472: 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 473 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 474 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.6 - Loading samples (in lbs and in) Edition 0 - March 05, 2019 Page 6.4.19 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 475: 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 476 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 - Blanking caps bag 8.31 128.00 (3.77)
Page 477 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) 0207-00 carpet (cargo use) 35.27 211.42...
Page 478: 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 8, 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 479 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.5.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 480 Section 7 Description Pilot's Operating Handbook Section 7 Description Table of contents General ..........7.1.1 Airframe .
Page 481 Section 7 Description Pilot's Operating Handbook Powerplant ..........7.6.1 Turboprop engine operation .
Page 482 Section 7 Description Pilot's Operating Handbook Electrical system ........7.9.1 Starter generator .
Page 483 Section 7 Description Pilot's Operating Handbook 7.15 Miscellaneous equipment ....... . 7.15.1 Stall warning system .
Page 484: 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 485 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.1.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 486: 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 487 Section 7 Description Pilot's Operating Handbook Figure 7.2.1 - Cabin arrangement 6-seat accommodation Page 7.2.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 488 Section 7 Description Pilot's Operating Handbook Figure 7.2.1A - Cabin arrangement 4-seat accommodation with large securing net Edition 0 - March 05, 2019 Page 7.2.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 489 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 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 490: 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 491 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 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 492 Section 7 Description Pilot's Operating Handbook Figure 7.2.2 (2/2) - Wing flaps Edition 0 - March 05, 2019 Page 7.2.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 493 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.2.8 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 494: 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, electrical systems, AP/TRIMS switch, ELT remote control switch and the FUEL control panel.
Page 495 Section 7 Description Pilot's Operating Handbook An adjustable air outlet is located on both sides of instrument panel lower part. 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.
Page 496 Section 7 Description Pilot's Operating Handbook Aural warning alerts According to the airplane configuration, different aural warning alerts sound : gear up and idle landing gear / landing gear gear up and extended flaps landing gear / landing gear stall stall / stall gear up, idle and stall stall / landing gear...
Page 497 Section 7 Description Pilot's Operating Handbook Figure 7.3.1 - Instrument panel assembly (Typical arrangement) Page 7.3.4 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 498 Section 7 Description Pilot's Operating Handbook Intentionally left blank Edition 0 - March 05, 2019 Page 7.3.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 499 Section 7 Description Pilot's Operating Handbook L.H. instrument panel emergency lighting Loud-speaker of GMA 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 7.6.8 ELECTRIC POWER switches - see figure 7.8.5 INT LIGHTS internal lighting switches - see figure 7.8.7...
Page 500 Section 7 Description Pilot's Operating Handbook Figure 7.3.2 (2/2) - Upper panel and cockpit overhead panel Edition 0 - March 05, 2019 Page 7.3.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 501 Section 7 Description Pilot's Operating Handbook DISPLAY BACKUP, A/C CONTROL and SEATS HTRS MASTER panels - see figure 7.9.2 General alarm red and amber indicators MD302 PFD 1 Landing gear configuration and control panel - see figure 7.5.1 Parking brake control - see figure 7.5.6 USB servicing plug Alternate station reception-micro jack L.H.
Page 502 Section 7 Description Pilot's Operating Handbook Figure 7.3.3 (2/2) - Left instrument panel (Typical arrangement) Edition 0 - March 05, 2019 Page 7.3.9 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 503 Section 7 Description Pilot's Operating Handbook BARO knob Micro LDR AFCS control unit LVL push-button >> With HomeSafe emergency function (Post-MOD70-0650-34B) HomeSafe activation button >> All Registration Touchscreen controllers PRESSURIZATION panel - see figure 7.10.2 Figure 7.3.4 (1/2) - Central instrument panel Page 7.3.10 Edition 0 - March 05, 2019 Rev.
Page 504 Section 7 Description Pilot's Operating Handbook Figure 7.3.4 (2/2) - Central instrument panel (Typical arrangement) Edition 0 - March 05, 2019 Page 7.3.11 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 505 Section 7 Description Pilot's Operating Handbook PFD 2 DISPLAY BACKUP push-button BARO knob Pitch & Yaw trim setting management Push To Talk button (PTT) AP / TRIM DISC push-button Adjustable air outlet Circuit breakers panel postlight R. H. station rudder pedals adjusting handle Right station reception-micro jacks USB servicing plugs Crew music...
Page 506 Section 7 Description Pilot's Operating Handbook Figure 7.3.5 (2/2) - Right instrument panel (Typical arrangement) Edition 0 - March 05, 2019 Page 7.3.13 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 507 Section 7 Description Pilot's Operating Handbook THROTTLE FLAPS lever THROTTLE and MAN OVRD 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 7.3.14 Edition 0 - March 05, 2019...
Page 508 Section 7 Description Pilot's Operating Handbook Figure 7.3.6 (2/2) - Pedestal console (Typical arrangement) Edition 0 - March 05, 2019 Page 7.3.15 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 509 Section 7 Description Pilot's Operating Handbook Figure 7.3.7 - Circuit breakers panel Page 7.3.16 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 510 Section 7 Description Pilot's Operating Handbook Figure 7.3.8 - General alarms warning lights Edition 0 - March 05, 2019 Page 7.3.17 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 511: Homesafe Interface Panel (Post-Mod70-0650-34B)
Section 7 Description Pilot's Operating Handbook HomeSafe interface panel (Post-MOD70-0650-34B) The activation button for HomeSafe emergency function is located in central area on top of instrument panel - see figure 7.3.4. 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.
Page 512 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 513 Section 7 Description Pilot's Operating Handbook Figure 7.3.9 - Cabin access door Page 7.3.20 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 514 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 515 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 516 Section 7 Description Pilot's Operating Handbook Figure 7.3.9A - Cockpit access door (pilot door) Edition 0 - March 05, 2019 Page 7.3.23 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 517 Section 7 Description Pilot's Operating Handbook Emergency exit - see figure 7.3.10A 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 518 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 519 Section 7 Description Pilot's Operating Handbook Figure 7.3.10 - Emergency exit Edition 0 - March 05, 2019 Page 7.3.25 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 520 • .r-Earn Section 7 ..!34D Description • Pilot's Operating Handbook "' » Pre-MOD70-0793-25 • Upholstery panel • � Opening handle � � 1,1. _':.J. " /"': •• & ..• • ._ � I Step 1 �...
Page 521 Section 7 Description Pilot's Operating Handbook Intentionally left blank Edition 0 - March 05, 2019 Page 7.3.25B TR29 - July 2022 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 522: Seats, Belts And Harnesses
Section 7 Description Pilot's Operating Handbook >> All Seats, belts and harnesses Heated seats - see figure 7.3.11 Cockpit and cabin seats are equipped with a heating system providing comfort to pilot and passengers. The system consists of : One heating element in the cushion and one heating element in the backrest of each seat, The SEATS HTRS MASTER switch located on the instrument panel, HI/OFF/LOW three positions switch located on each cockpit and cabin seat,...
Page 523 Section 7 Description Pilot's Operating Handbook Seats, belts and harnesses Heated seats - see figure 7.3.11 Cockpit and cabin seats are equipped with a heating system providing comfort to pilot and passengers. The system consists of : One heating element in the cushion and one heating element in the backrest of each seat, The SEATS HTRS MASTER switch located on the instrument panel, HI/OFF/LOW three positions switch located on each cockpit and cabin seat,...
Page 524 Section 7 Description Pilot's Operating Handbook SEATS HTRS MASTER switch Backrest surface heating Seat surface heating HI/OFF/LOW three position switch Tactile marks Figure 7.3.11 - Heated seat Edition 0 - March 05, 2019 Page 7.3.27 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 525 Section 7 Description Pilot's Operating Handbook The seats heating is only available when the airplane is connected to a GPU or when the main generator is supplying power. The system does not operate if GENERATOR selector is set to ST-BY. The SEATS HTRS MASTER switch allows the pilot to enable or not the electrical supply of all seats heaters.
Page 526 Section 7 Description Pilot's Operating Handbook Cockpit seats - see figure 7.3.12 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 527 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 528 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 (2) With seats heaters system (MOD70-0588-25) In this position, the seats heaters system cannot be connected to the rear seat. Each cross indicates that you have a seat at the correspondent location number.
Page 529: Baggage Compartments
Section 7 Description Pilot's Operating Handbook Belts and harnesses - see figure 7.3.13 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 530 Section 7 Description Pilot's Operating Handbook Maximum loads allowable in the baggage compartments depend on airplane equipment, refer to section 6 Weight and balance. 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.
Page 531 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 532: 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 533 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 534 Section 7 Description Pilot's Operating Handbook Figure 7.3.12 (2/2) - Seats Edition 0 - March 05, 2019 Page 7.3.37 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 535 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 7.3.12A (1/2) - Seats...
Page 536 Section 7 Description Pilot's Operating Handbook Figure 7.3.12A (2/2) - Seats Edition 0 - March 05, 2019 Page 7.3.39 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 537 Section 7 Description Pilot's Operating Handbook >> All Figure 7.3.13 - Front and rear seat belts,with movable straps, and harnesses Page 7.3.40 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 538: 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 539 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 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 540 Section 7 Description Pilot's Operating Handbook Figure 7.4.1 (2/2) - Roll Edition 0 - March 05, 2019 Page 7.4.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 541 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 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 542 Section 7 Description Pilot's Operating Handbook Figure 7.4.2 (2/2) - Lateral trim Edition 0 - March 05, 2019 Page 7.4.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 543: 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 stick shaker is fixed on the pitch lever linked to the pilot control column lever.
Page 544 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 Stick shaker Figure 7.4.3 (1/2) - Elevator Edition 0 - March 05, 2019 Page 7.4.7 Rev.
Page 545 Section 7 Description Pilot's Operating Handbook Figure 7.4.3 (2/2) - Elevator Page 7.4.8 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 546 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 - March 05, 2019 Page 7.4.9 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 547 Section 7 Description Pilot's Operating Handbook Figure 7.4.4 (2/2) - Pitch trim Page 7.4.10 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 548: 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 549 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 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 550 Section 7 Description Pilot's Operating Handbook Figure 7.4.5 (2/2) - Rudder Edition 0 - March 05, 2019 Page 7.4.13 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 551 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 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 552 Section 7 Description Pilot's Operating Handbook Figure 7.4.6 (2/2) - Rudder trim Edition 0 - March 05, 2019 Page 7.4.15 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 553 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.4.16 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 554: 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 555: 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 556 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 - March 05, 2019 Page 7.5.3 Rev.
Page 557: 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. Landing gear aural warning Landing gear / Landing gear aural warning alert sounds when : THROTTLE is on IDLE position and landing gear is not down-locked, flaps are beyond TO position (Takeoff) and landing gear is not down-locked.
Page 558 Section 7 Description Pilot's Operating Handbook Figure 7.5.2 - Emergency landing gear extension control Edition 0 - March 05, 2019 Page 7.5.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 559: 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 560 Section 7 Description Pilot's Operating Handbook Figure 7.5.3 - Minimum turn diameter (Full rudder pedals travel without using differential braking) Edition 0 - March 05, 2019 Page 7.5.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 561 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 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 562: Brake System
Section 7 Description Pilot's Operating Handbook Brake system - see figures 7.5.5 and 7.5.5A 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 563 Section 7 Description Pilot's Operating Handbook >> Without HomeSafe emergency function (Pre-MOD70-0650-34A) 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 - March 05, 2019 Rev.
Page 564 Section 7 Description Pilot's Operating Handbook Figure 7.5.5 (2/2) - Brake system Edition 0 - March 05, 2019 Page 7.5.11 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 565 Section 7 Description Pilot's Operating Handbook >> With HomeSafe emergency function (Post-MOD70-0650-34A) Reservoir Vent HomeSafe braking servo-actuator HomeSafe master cylinder 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 7.5.5A (1/2) - Brake system Page 7.5.12 Edition 0 - March 05, 2019...
Page 566 Section 7 Description Pilot's Operating Handbook Figure 7.5.5A (2/2) - Brake system Edition 0 - March 05, 2019 Page 7.5.13 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 567 Section 7 Description Pilot's Operating Handbook >> All Figure 7.5.6 - Brake system Page 7.5.14 Edition 0 - March 05, 2019 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 568: 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 569 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 570 Section 7 Description Pilot's Operating Handbook Figure 7.6.1 (2/2) - Powerplant Edition 0 - March 05, 2019 Page 7.6.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 571: 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 and its detent for reverse, GA push-button and AT DISC push-button, MAN OVRD control for emergency fuel regulation, Thumbwheel for lever friction.
Page 572 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 573 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 574 Section 7 Description Pilot's Operating Handbook Autothrottle mechanical assembly The autothrottle function actuates the THROTTLE by an assembly of rods and levers permitting to link the GARMIN servo-motor and the potentiometer. The THROTTLE movements are defined by the servo-motor. The THROTTLE position is measured by the potentiometer. The autothrottle controls are integrated within the AFCS control panel which is located above the MFD.
Page 575 Section 7 Description Pilot's Operating Handbook Pedestal assembly Potentiometer Servo-motor Lever Figure 7.6.4 - Autothrottle Page 7.6.8 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 576: Engine Instruments
Section 7 Description Pilot's Operating Handbook MAN OVRD control - see figure 7.6.2 MAN OVRD control (3) is normally notched in full backward position. In case of FCU or THROTTLE failure, it allows setting engine power manually. To quit full backward position (notched), move the MAN OVRD control forward overriding the indexation.
Page 577: Single Engine Indicator
Section 7 Description Pilot's Operating Handbook Single engine indicator - see figures 7.6.5, 7.6.6 and 7.6.7 The single engine indicator simplifies the monitoring of engines parameters : TRQ, NG and ITT gauges are merged into one display window. PROP RPM is always displayed with a digital indicator. TRQ, NG and ITT indications have a dedicated tab.
Page 578 Section 7 Description Pilot's Operating Handbook Figure 7.6.6 - Priority indication = NG Figure 7.6.7 - Priority indication = ITT Edition 0 - March 05, 2019 Page 7.6.11 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 579: Engine Lubrication
Section 7 Description Pilot's Operating Handbook Engine lubrication Engine oil is in a tank incorporated into the powerplant. It ensures lubrication and engine cooling. A cooler located on left side in engine compartment maintains oil temperature within limits. Oil flow into the cooler is metered by a thermostatic valve. Engine oil also supplies propeller governor and engine torquemeter.
Page 580 Section 7 Description Pilot's Operating Handbook Starter function Starting system consists of STARTER switch located on ENGINE START panel, starter generator and ignition circuit (Refer to paragraph Ignition function). Starting procedure is semi-automatic. Setting STARTER switch to ON connects the starter generator which drives powerplant.
Page 581 Section 7 Description Pilot's Operating Handbook Figure 7.6.8 - Engine starting Page 7.6.14 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 582: 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 583: Exhaust System
Section 7 Description Pilot's Operating Handbook Exhaust system Exhaust gases are evacuated through exhaust stubs located on sides of engine cowlings. Engine accessories All engine driven accessories, except power turbine tacho-generator (Np), propeller governor and overspeed governor, are installed on accessory gearbox located rearwards of engine.
Page 584: Propeller
Section 7 Description Pilot's Operating Handbook Torque limiter Torque limiter is located on right side of the reduction gear box. It is rated to limit engine torque to 109-110 % at sea level. Propeller Airplane is equipped with a composite five-bladed, constant-speed and full-feathering propeller.
Page 585 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.6.18 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 586: Use Of Autothrottle
Section 7 Description Pilot's Operating Handbook - Use of autothrottle General The Autothrottle (AT) function is fully integrated with the Automatic Flight Control System (AFCS) and is associated with the Single Engine Indicator (SEI). AT automatically actuates the THROTTLE lever to control engine power within operational limits, in order to reach and maintain the manually selected airspeed (MAN mode) or programmed flight phase schedule (FMS mode).
Page 587 Section 7 Description Pilot's Operating Handbook AT engine protections AT engine protections automatically reduce engine power, to ensure that all engine parameters never remain above the following cautionary threshold values : TRQ > 100 % Ng > 103.0 % ( NG HI CAS message) ITT >...
Page 588: At Engagement And Disengagement
Section 7 Description Pilot's Operating Handbook AT engagement and disengagement AT engagement To engage AT, press the AT button on the Garmin Mode Controller (GMC). status, and associated AT mode become active. If the AT is not engaged, AT may automatically engage if an engine or airspeed protection is triggered.
Page 589: Engine Start Or Engine Air Start
Section 7 Description Pilot's Operating Handbook Engine start or engine air start ● NOTE ● Autothrottle engine protection system is disabled during engine start, thus there is no protection against ITT exceedances. ● For additional information on SEI display during engine start, refer to section 7.6 Powerplant, Single engine indicator and to GARMIN Pilot’s Guide, Engine Indication System (EIS) section.
Page 590: Climb
Section 7 Description Pilot's Operating Handbook Climb Above 1 000 ft AGL : For climb with the AT engaged, it is recommended to use the FD vertical mode. When is active, AT engagement activates the CLIMB AT mode that sets and maintains engine power in accordance with the climb performance tables - refer to section 5.10 Climb performance.
Page 591 Section 7 Description Pilot's Operating Handbook Cruise in MAN Mode In MAN mode, AT engagement activates the SPD XXX AT mode that controls engine power within operational limits to reach and maintain the selected airspeed. ● NOTE ● If the selected airspeed cannot be reached (e.g. selected airspeed is too high with respect to maximum permitted engine power, or engine performance is affected when inertial separator is ON, etc.), the AT maintains the maximum permitted engine power and the resulting airspeed may remain below the...
Page 592 Section 7 Description Pilot's Operating Handbook Figure 7.7.2 - Optimum Cruise Range Figure 7.7.3 - Long Range Cruise Examples Example, with no speed constraints : FL 280, Selected Cruise Schedule : Maximum Cruise. No Speed Constraint. AT mode : MXCR Managed AT TRQ = 100 % IAS ≃...
Page 593: Descent
Section 7 Description Pilot's Operating Handbook Altitude 3 000 ft, Selected Cruise Schedule : Maximum Cruise. Speed Constraint = 120 kt. AT mode : SPD 120 KT Managed AT TRQ ≃ 30 % (torque corresponding to target airspeed) IAS = 120 kt Descent For descent with the AT engaged, it is recommended to use the vertical mode.
Page 594: Go-Around
Section 7 Description Pilot's Operating Handbook AT must be disengaged before 200 ft AGL. Then, engine torque must be manually adjusted to manage airspeed until touchdown. ● NOTE ● It is possible to perform an approach with the AT engaged and the AP/FD disengaged.
Page 595: Fd Vertical Modes And Corresponding At Modes Summary
Section 7 Description Pilot's Operating Handbook FD vertical modes and corresponding AT modes summary The following table provides the correspondence between FD vertical modes and AT modes, depending on the MAN/FMS mode. Corresponding Corresponding AT Mode Active FD Vertical Mode AT Mode (FMS) (MAN)
Page 596: Fuel System
Section 7 Description Pilot's Operating Handbook - Fuel system - see figures 7.8.1 and 7.8.1A 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 597 Section 7 Description Pilot's Operating Handbook >> Without HomeSafe emergency function (Pre-MOD70-0650-34A) 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...
Page 598 Section 7 Description Pilot's Operating Handbook Figure 7.8.1 (2/2) - Fuel system Edition 0 - March 05, 2019 Page 7.8.3 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 599 Section 7 Description Pilot's Operating Handbook >> With HomeSafe emergency function (Post-MOD70-0650-34A) Flow divider Filter drain Flowmeter HomeSafe fuel shut-off valve 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...
Page 600 Section 7 Description Pilot's Operating Handbook Figure 7.8.1A (2/2) - Fuel system Edition 0 - March 05, 2019 Page 7.8.5 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 601: Automatic Tank Selector
Section 7 Description Pilot's Operating Handbook >> All Automatic tank selector - see figures 7.8.2 and 7.8.3 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).
Page 602: Electric Boost Pump (Aux Bp)
Section 7 Description Pilot's Operating Handbook If airplane is on ground or in flight, low level CAS messages not visible, the new selected tank remains operating and a new sequence is initiated. ● NOTE ● This procedure allows the pilot to preferably choose the tank from which he/she wants to take fuel.
Page 603 Section 7 Description Pilot's Operating Handbook Figure 7.8.2 - Manual selector of fuel tanks Page 7.8.8 Edition 0 - March 05, 2019 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 604 Section 7 Description Pilot's Operating Handbook AUX BP switch FUEL SEL switch SHIFT push-button Figure 7.8.3 - Fuel control panel Edition 0 - March 05, 2019 Page 7.8.9 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 605: 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 606: Fuel System Draining And Clogging Indicator
Section 7 Description Pilot's Operating Handbook Fuel system draining and clogging indicator - see figure 7.8.4 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 607 Section 7 Description Pilot's Operating Handbook Lighting switch Mirror door Clogging indicator Central access door Filter drain Tank drain Drain bowl Figure 7.8.4 - Fuel system draining points and clogging indicator Page 7.8.12 Edition 0 - March 05, 2019 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 608: Electrical System
Section 7 Description Pilot's Operating Handbook - Electrical system - see figures 7.9.1, 7.9.2 and 7.9.5 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 609: 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 610: 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 611: 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 612 Section 7 Description Pilot's Operating Handbook Figure 7.9.1 - Electrical diagram Edition 0 - March 05, 2019 Page 7.9.5 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 613 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 614 Section 7 Description Pilot's Operating Handbook Figure 7.9.3 - (1/3) - Electrical distribution of bus bars Edition 0 - March 05, 2019 Page 7.9.7 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 615 Section 7 Description Pilot's Operating Handbook Figure 7.9.3 (2/3) - Electrical distribution of bus bars Page 7.9.8 Edition 0 - March 05, 2019 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 616 Section 7 Description Pilot's Operating Handbook Figure 7.9.3 (3/3) - Electrical distribution of bus bars Edition 0 - March 05, 2019 Page 7.9.9 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 617 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 618 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 XPDR 2 Transponder 2, if installed, protection AIRFRAME DE ICE...
Page 619 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 Angle of Attack protection RADIO ALTI RADIO ALTI, if installed protection DME protection, if installed FUEL SEL Tank selector timer protection...
Page 620 Section 7 Description Pilot's Operating Handbook Figure 7.9.4 (4/4) - Breaker panel (Typical arrangement) Edition 0 - March 05, 2019 Page 7.9.13 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 621: 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 622 Section 7 Description Pilot's Operating Handbook MAIN reset knob ST-BY reset knob Crash lever SOURCE selector GENERATOR selector Figure 7.9.5 - Electrical control Edition 0 - March 05, 2019 Page 7.9.15 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 623: Exterior Lighting
Section 7 Description Pilot's Operating Handbook Exterior lighting - see figure 7.9.6 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 624 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 625 Section 7 Description Pilot's Operating Handbook Taxi and landing light switch Pulselite system switch Navigation lights switch Strobe lights switch Figure 7.9.6 - External lighting controls Page 7.9.18 Edition 0 - March 05, 2019 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 626: Interior Lighting
Section 7 Description Pilot's Operating Handbook Interior lighting - see Figure 7.9.7 Interior lighting consists of access, cabin, instrument panel, instruments, baggage compartment and emergency lighting. Access lighting Access lighting consists of floodlights: two individual for front seats, four individual for rear passenger seats, one on the access door, one in the dome light of the baggage compartment, on the left side.
Page 627 Section 7 Description Pilot's Operating Handbook Emergency lighting Emergency lighting consists of two swiveling floodlights located on both sides of the cockpit overhead panel above front seats. It illuminates instrument panel assembly in case of visor lighting tubes and / or instrument integrated lighting failure. A rheostat located on the cockpit overhead panel controls emergency lighting operation and intensity.
Page 628 Section 7 Description Pilot's Operating Handbook Figure 7.9.7 (2/2) - Internal lighting controls Edition 0 - March 05, 2019 Page 7.9.21 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 629: Plug
Section 7 Description Pilot's Operating Handbook 115V Plug The 115V plug permits to connect external equipments (max power : 250 W). The plug is located on the right aft side of the cabin compartment, in the storage pocket. Page 7.9.22 Edition 0 - March 05, 2019 Rev.
Page 630: Air Conditioning And Pressurization
Section 7 Description Pilot's Operating Handbook 7.10 - Air conditioning and pressurization ● NOTE ● A list of abbreviations used in this chapter is given in figure 7.10.2. ● The airplane is equipped with a Global Air System (GAS), which ensures air conditioning and pressurization control - see figure 7.10.2.
Page 631: 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 632: Cabin Pressurization Control System
Section 7 Description Pilot's Operating Handbook System operation See figure 7.10.3. 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 633 Section 7 Description Pilot's Operating Handbook The GASC controls the OFV through a torque motor on the valve. 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.
Page 634 Section 7 Description Pilot's Operating Handbook CAS messages are displayed in the MFD CAS window : PRESSU OFF indicates that the BLEED switch is in OFF position or that the Flow Control and Shut Off Valve (FCSOV) is closed due to a system malfunction (cabin inlet overtemperature, BDPS or FCSOV failure).
Page 635: Dual Zones Environmental Control System (Ecs)
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 636 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 7.10.3 and paragraph Air temperature management. A/C control panel selection : If the A/C switch is set to OFF : >>...
Page 637 Section 7 Description Pilot's Operating Handbook >> After GASC software evolution (Post-MOD70-0689-21) If the pilot or passengers set the TEMP 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 638 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, CAB FAN, CKPT FAN and GND FAN.
Page 639 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 : Air temperature Cockpit panel selection Cabin panel selection expectations Cockpit Warm...
Page 640 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 selector is set in the blue arc.
Page 641 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 selectors set in the blue arc, 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 642 Section 7 Description Pilot's Operating Handbook Cabin override Selecting the switch to PILOT position disables TEMP and FAN speed selectors in the cabin area. The PILOT position also distributes warm air equally to the cockpit and cabin. Only the cockpit TEMP and FAN selectors inputs are used by the GASC for air temperature management.
Page 643 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 selector set in the blue arc, 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 644 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 selector settings.
Page 645 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.10.16 Edition 0 - March 05, 2019 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 646 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 647 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 648 Section 7 Description Pilot's Operating Handbook Figure 7.10.2 (3/3) -- GAS Edition 0 - March 05, 2019 Page 7.10.19 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 649 Section 7 Description Pilot's Operating Handbook A/C switch FAN speed selector (cockpit/cabin) TEMP selector (cockpit/cabin) DUMP switch HOT AIR FLOW distributor BLEED switch FAN speed selector (cabin) TEMP selector (cabin) Figure 7.10.3 (1/2) - GAS controls Page 7.10.20 Edition 0 - March 05, 2019 Rev.
Page 650 Section 7 Description Pilot's Operating Handbook Figure 7.10.3 (2/2) - GAS controls Edition 0 - March 05, 2019 Page 7.10.21 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 651 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.10.22 Edition 0 - March 05, 2019 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 652: Emergency Oxygen System
Section 7 Description Pilot's Operating Handbook 7.11 - Emergency oxygen system - see figure 7.11.1 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 653 Section 7 Description Pilot's Operating Handbook MICRO / MASK switch OXYGEN switch PASSENGER OXYGEN switch Figure 7.11.1 - Emergency oxygen system Page 7.11.2 Edition 0 - March 05, 2019 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 654 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 DEPLOY/STBY (PASSENGER OXYGEN switch) with guard to permit the supply of the passengers four masks, when the first valve is open.
Page 655: Flight Above 15000 Ft With Possible Emergency Descent
Section 7 Description Pilot's Operating Handbook WARNING ▲ ▲ Do not smoke during oxygen system use. Oil, grease, soap, make up, lipstick and any other greasy substances constitute a serious fire or burning hazard, when on contact with oxygen. ▲ Flight above 15000 ft with possible emergency descent Minimum oxygen pressure (PSIG) for following conditions : 4 minutes from 31000 to 15000 ft.
Page 656: 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 657: 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 658: O 2 Smart Mike Mask
Section 7 Description Pilot's Operating Handbook smart mike mask 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.
Page 659 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.11.8 Edition 0 - March 05, 2019 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 660: Air Data System And Instruments
Section 7 Description Pilot's Operating Handbook 7.12 - Air data system and instruments - see figure 7.12.1 Airplane air data system consists of : two separate static pressure systems supplying the standby attitude module 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 661: 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 standby attitude module and one ADC. The second one supplies the other ADC. Both lines incorporate a drain plug located in the root of L.H.
Page 662 Section 7 Description Pilot's Operating Handbook Intentionally left blank Edition 0 - March 05, 2019 Page 7.12.3 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 663 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 664 Section 7 Description Pilot's Operating Handbook Figure 7.12.1 (2/2) - Air data system Edition 0 - March 05, 2019 Page 7.12.5 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 665 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.12.6 Edition 0 - March 05, 2019 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 666: Vacuum System And Instruments
Section 7 Description Pilot's Operating Handbook 7.13 - Vacuum system and instruments - see figure 7.13.1 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 667 Section 7 Description Pilot's Operating Handbook Pressure regulator Ejector Valve Regulating and relief valve Pressure switch Failure CAS message Figure 7.13.1 (1/2) - Vacuum system Page 7.13.2 Edition 0 - March 05, 2019 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 668 Section 7 Description Pilot's Operating Handbook Figure 7.13.1 (2/2) - Vacuum system Edition 0 - March 05, 2019 Page 7.13.3 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 669 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.13.4 Edition 0 - March 05, 2019 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 670: Ice Protection Equipment
Section 7 Description Pilot's Operating Handbook 7.14 - Ice protection equipment Ice protection equipment is as follows : Ice Detection System 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/R &...
Page 671 Section 7 Description Pilot's Operating Handbook In AUTO mode, when ice is detected, all the ice protection systems are automatically activated - see figure 7.14.2, and ICE DETECTED is displayed in the CAS window. Figure 7.14.2 - DE ICE SYSTEM panel - AUTO mode with ice detected Pilot action is required to revert the system in MAN mode by pressing the DE ICE SYSTEM mode switch.
Page 672: Wing And Empennage Deicing
Section 7 Description Pilot's Operating Handbook is displayed in the CAS window in the following cases : ICE DETECTION FAIL failure of the ice detector. The system shall be reverted in MAN mode by the pilot, failure of the DE ICE SYSTEM panel printed circuit. The system is automatically reverted in MAN mode.
Page 673: 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 when PROP DE ICE system is activated either manually or automatically. Each cycle is 180 seconds long.
Page 674: Windshield Deicing
Section 7 Description Pilot's Operating Handbook Windshield deicing The windshields are deiced electrically by integrated heating resistors. The system includes two controllers and two heat probes embedded in each windshield. They are operated by the WINDSHIELD switch. When WINDSHIELD deice system is activated either manually or automatically, the controllers supply the heating resistors, the windshield temperature is controlled via heat probes.
Page 675: Heating Of Pitots And Stall Warning Sensor (Pitot L/R & Stall Htr)
Section 7 Description Pilot's Operating Handbook Heating of pitots and stall warning sensor (PITOT L/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 676: Stall Warning System
Section 7 Description Pilot's Operating Handbook 7.15 - 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 677: Cabin Fire Extinguisher
Section 7 Description Pilot's Operating Handbook Static dischargers As an aid in flight, static dischargers are installed to improve radio communications during flight by reducing interference from dust or various forms of precipitations (rain, snow or ice crystals). Under these conditions, the build-up and discharge of static electricity from the trailing edges of the wings (flaps and ailerons), rudder, stabilator, propeller tips and radio antennas can result in loss of usable radio signals on all communications and navigation radio equipment.
Page 678: Weather Radar
Section 7 Description Pilot's Operating Handbook Weather radar The weather information can be displayed on PFD1, PFD2 and MFD. Refer to section 2 Limitations of this POH and to GARMIN Pilot's Guide for further details. The controls for the weather radar are located on the touchscreen controllers. The weather radar is protected by the WXR breaker.
Page 679 Section 7 Description Pilot's Operating Handbook Radar mode Area of weather display Antenna stabilization status Touchscreen controllers Scale for weather display Figure 7.15.1 (1/2) - Weather radar display and controls Page 7.15.4 Edition 0 - March 05, 2019 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 680 Section 7 Description Pilot's Operating Handbook Figure 7.15.1 (2/2) - Weather radar display and controls Edition 0 - March 05, 2019 Page 7.15.5 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 681: Emergency Locator Transmitter
Section 7 Description Pilot's Operating Handbook Emergency locator transmitter The airplane is equipped with an ELT ARTEX 1000 emergency locator transmitter which enables to locate it in case of distress. It is located in fuselage rear section with a service door on fuselage R.H. side. The emergency locator transmitter assembly is constituted of a transmitter supplied by a battery, of an antenna attached on upper fuselage and of a remote control located on the upper panel.
Page 682: Lightweight Data Recorder (Ldr 1000)
Section 7 Description Pilot's Operating Handbook Set remote control switch to ARM/OFF or ELT switch to ARM/OFF. a) The ELT does not transmit emergency signal any longer. b) On remote control box, red indicator light illuminates for about 1 second, then goes off.
Page 683: Ads-B Out Function
Section 7 Description Pilot's Operating Handbook ADS-B OUT function The ADS-B OUT function enables the airplane to broadcast data, such as position information, to ground stations and to other airplanes equipped with ADS-B IN system. The loss of an interfaced input to the selected extended squitter transponder may cause the transponder to stop transmitting ADS-B OUT data.
Page 684: Data Collection And Transmission System (Fastbox)
Section 7 Description Pilot's Operating Handbook Data collection and transmission system (FASTBOX) The data collection and transmission system collects data from airplane data buses and discrete inputs and stores it in resident non-volatile memory. When the airplane is on the ground and a few minutes after the engine shut-down, recorded data are automatically transmitted to a ground station via the cellular or WiFi network.
Page 685 Section 7 Description Pilot's Operating Handbook 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. LNAV+V approaches do not downgrade in general because they do not require SBAS, although high GPS vertical error estimate anomalies could result in loss of advisory vertical guidance.
Page 686 Section 7 Description 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 687 Section 7 Description 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 688 Section 7 Description 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. If SBAS becomes unavailable on an RNAV LNAV/VNAV approach, L/VNAV shown in yellow, the system switches to LNAV/VNAV (Baro-VNAV) service level and...
Page 689 Section 7 Description 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 690: Homesafe Emergency Function (Post-Mod70-0650-34A)
Section 7 Description Pilot's Operating Handbook Advisory vertical guidance for VOR and NDB approaches, if installed CAUTION ▲ ▲ Advisory vertical guidance does not change the published approach minima. ▲ For VOR and NDB approaches, when a published glide path angle is resident in the navigation databases, the system will provide a GPS-based advisory vertical guidance.
Page 691 Section 7 Description Pilot's Operating Handbook When HomeSafe is activated, HOMESAFE REQUEST is displayed in the CAS window for 15 seconds before HomeSafe starts the automatic landing process. During those 15 seconds, if the autopilot was not engaged prior to HomeSafe activation, the Level mode is activated.
Page 692 Section 7 Description Pilot's Operating Handbook WARNING ▲ ▲ HomeSafe deactivation must be performed by a pilot : - fully capable of flying the airplane, - fully aware of all the actions the pilot will have to perform to reconfigure the airplane (the initial flight plan in the FMS is lost, the landing gear and flaps positions may not agree with LANDING GEAR and FLAPS levers positions).
Page 693: Optional Equipment
Section 7 Description Pilot's Operating Handbook Protection - Safety HS CONFIG MODE is displayed in the CAS window when HomeSafe is in configuration mode. HomeSafe function is protected by the HOMESAFE breaker. Optional equipment For optional equipment such as stormscope, SVS or TAWS, refer to section 9 Supplements.
Page 694 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 695 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Airplane cleaning and care ....... 8.8.1 Windshield and windows .
Page 696: 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.
Page 697 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.1.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 698: 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 699 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.2.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 700: 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 701 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.3.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 702: 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 703 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.4.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 704: 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 705 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.5.2 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 706: 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 707: 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 708 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Figure 8.6.1 - Turning angle limits Edition 0 - March 05, 2019 Page 8.6.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 709: 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 710 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Figure 8.6.2 - Control lock device Edition 0 - March 05, 2019 Page 8.6.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 711 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.6.6 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 712: 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 713: 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 714 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 715 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 716 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 717 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 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 718: 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 719: 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 720 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 721 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 722 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 723 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 724 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.
Page 725: Batteryminder Charger
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook BatteryMINDer charger CAUTION ▲ ▲ - Read carefully charger manufacturer instructions before use. - The charger shall be used only on ground. - The charger is not designed to be installed permanently on the airplane.
Page 726 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Figure 8.7.5 (2/2) - Removal / Installation of BatteryMINDer charger Edition 0 - March 05, 2019 Page 8.7.15 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 727 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.7.16 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 728: 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 729: 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 730: 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 731 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Unlock backrest using backrest tilting handle (6) and fold it forward. ● NOTE ● For the R.H. rear seat, backrest tilting handle is located behind backrest. ● Unlock seat using seat tilting handle (1) and tilt it forward. CAUTION ▲...
Page 732 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook CAUTION ▲ ▲ Make sure to disconnect the seat heating system before the removal of the seat to prevent harness damage. ▲ Disconnect heating system harness and clip the loose connector to the holder located on the seat structure.
Page 733 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Remove blanking plugs (31) located in line with R.H. front side window - see figure 8.9.3 detail C, and install them on holes located in line with card table - see figure 8.9.3 detail D. ●...
Page 734 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Release locking handle (21) to lock the seat. WARNING ▲ ▲ Verify that lock (22) and all pads (23) are engaged and locked into rails, trying to move seat forward and backward. ▲...
Page 735 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook C - Cabin comfort - see figure 8.9.3 Remove blanking plugs (32) from their storage bag and install them on holes located forward the large door - see figure 8.9.3 detail B. Remove blanking device assy (33) from the hot air outlet, located forward the large door, and store it into storage bag - see figure 8.9.3 detail A.
Page 736 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 737 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook ● NOTE ● After these operations, determine weight and balance with the new C.G. - refer to section 6. ● Description Equipment Action operation Removal Paragraph 1.C. Rear seat Installation Paragraph 2. F. Removal Paragraph 1.D.
Page 738 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Figure 8.9.1 (2/2) - Removal / installation of rear seat Edition 0 - March 05, 2019 Page 8.9.9 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 739 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook 21) Locking handle 22) Lock 23) Pad 24) Rail 25) Backrest bottom upholstery 26) Seats heaters connector Figure 8.9.2 - Removal / installation of intermediate seat Page 8.9.10 Edition 0 - March 05, 2019 Rev.
Page 740 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook 31) Blanking plug 32) Blanking plug 33) Blanking device assy 34) Deflector Figure 8.9.3 - Cabin comfort - Installation of blanking plugs and deflector Edition 0 - March 05, 2019 Page 8.9.11 Rev.
Page 741 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook 34) Deflector 35) Deflector hole 36) Red mark 37) Color mark Figure 8.9.4 - Cabin comfort - Installation of deflector Page 8.9.12 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 742: Utilization By Cold Weather (- 0°C To - 25°C) Or Very Cold Weather (- 25°C To - 40°C)
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 743 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 744 Supplement 6 WX-500 stormscope Pilot's Operating Handbook SUPPLEMENT WX-500 stormscope Table of contents Page General ..........9.6.2 Limitations .
Page 745: Pilot's Operating Handbook
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 746 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 747 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 748: Supplement
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 749: 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 750: 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 751 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 752: 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 753: Weight And Balance
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 754: Description
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 755 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 756 Supplement 45 Mexico specifics Pilot's Operating Handbook SUPPLEMENT Mexico specifics Table of contents Page General ..........9.45.2 Limitations .
Page 757 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 758 Supplement 45 Mexico specifics Pilot's Operating Handbook For the small cargo net, on R.H. side lower upholstery panel 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 Edition 3 - December 20, 2018 Page 9.45.3 Rev.
Page 759 Supplement 45 Mexico specifics Pilot's Operating Handbook On rear passengers masks containers On internal face of rear passengers masks containers doors On rear passenger's table casing Page 9.45.4 Edition 3 - December 20, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 760 Supplement 45 Mexico specifics Pilot's Operating Handbook Door internal side On access door On pilot door, if installed On emergency exit handle Edition 3 - December 20, 2018 Page 9.45.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 761 Supplement 45 Mexico specifics Pilot's Operating Handbook Above emergency exit door On landing gear emergency control access door 10 - On cabinet drawer (optional) Page 9.45.6 Edition 3 - December 20, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 762 Supplement 45 Mexico specifics Pilot's Operating Handbook >> Airplane equipped with coat hanger (Post-MOD70-0557-25B) 11 - On the upper edge of the L.H. Passenger access door panel >> Airplane equipped with lavatory compartment (Post-MOD70-0505-25) 12 - On fixed panel, cabin side 13 - On fixed panel, toilet side Edition 3 - December 20, 2018...
Page 763 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 3 - December 20, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 764 Supplement 45 Mexico specifics Pilot's Operating Handbook 16 - Front face of lavatory compartment, near opening / closing switches 17 - On the magazine rack Edition 3 - December 20, 2018 Page 9.45.9 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 765 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 3 - December 20, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 766 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 3 - December 20, 2018 Page 9.45.11 Rev.
Page 767 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 3 - December 20, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 768 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 3 - December 20, 2018 Page 9.45.13 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 769 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 3 - December 20, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 770 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 3 - December 20, 2018 Page 9.45.15 Rev.
Page 771 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 3 - December 20, 2018 Rev.
Page 772 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 773 Supplement 45 Mexico specifics Pilot's Operating Handbook SECTION 7 Description No specifics SECTION 8 Handling, servicing and maintenance No specifics Page 9.45.18 Edition 3 - December 20, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 774 Supplement 49 GARMIN TAWS system Pilot's Operating Handbook SUPPLEMENT GARMIN TAWS system Table of contents Page General ..........9.49.2 Limitations .
Page 775 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 776 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 777 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 778 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 779 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 780 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 781 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 782 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 783 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 784 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 785 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 786 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 787 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 788 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 789 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 790 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 791 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 792 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 793 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 794 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 795: 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 796 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 797: 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 798 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 799 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 800: 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 801: 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 802 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 803 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 804 Supplement 59 Brazil specifics Pilot's Operating Handbook SUPPLEMENT Brazil specifics Table of contents Page General ..........9.59.2 Limitations .
Page 805: General
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 806 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 807 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 Page 9.59.4 Edition 3 - February 15, 2019 Rev.
Page 808 Supplement 59 Brazil specifics Pilot's Operating Handbook Near fuel tank caps On internal face of L.H. engine cowling CAPACIDAD DE ÓLEO 12 L Above passenger's table Edition 3 - February 15, 2019 Page 9.59.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 809 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 3 - February 15, 2019...
Page 810 Supplement 59 Brazil specifics Pilot's Operating Handbook On access door - External side On outer fuselage skin aft of access door In the cabin forward of access door Edition 3 - February 15, 2019 Page 9.59.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 811 Supplement 59 Brazil specifics Pilot's Operating Handbook On access door - Internal side >> Airplane equipped with MOD70-0619-11 version B >> Airplane equipped with MOD70-0619-11 version G >> All On pilot door - Internal side, if installed Page 9.59.8 Edition 3 - February 15, 2019 Rev.
Page 812 Supplement 59 Brazil specifics Pilot's Operating Handbook On emergency exit handle Marking on cover Marking on handle Above emergency exit door On rear passengers masks containers Edition 3 - February 15, 2019 Page 9.59.9 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 813 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 3 - February 15, 2019 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 814 Supplement 59 Brazil specifics Pilot's Operating Handbook On access door, cabin side and toilet side Behind access door, cabin side Behind access door, toilet side Edition 3 - February 15, 2019 Page 9.59.11 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 815 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 >> Airplane equipped with coat hanger (Post-MOD70-0641-25A) On the L.H. rear cargo compartment panel upper edge Page 9.59.12 Edition 3 - February 15, 2019 Rev.
Page 816 Supplement 59 Brazil specifics Pilot's Operating Handbook >> Airplane equipped with coat and headset hanger (Post-MOD70-0783-25B) On each coat and headset hanger >> Airplane equipped with extended large storage cabinet (Post-MOD70-0684-25) On the upper surface of the cabinet Inside large drawers, on side wall Edition 3 - February 15, 2019 Page 9.59.13 Rev.
Page 817: Emergency Procedures
Supplement 59 Brazil specifics Pilot's Operating Handbook Inside small internal drawer, on side wall SECTION 3 Emergency procedures No specifics SECTION 4 Normal procedures No specifics SECTION 5 Performance No specifics Page 9.59.14 Edition 3 - February 15, 2019 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 818: Description
Supplement 59 Brazil specifics 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. Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70...
Page 819 Supplement 59 Brazil specifics Pilot's Operating Handbook Intentionally left blank Page 9.59.16 Edition 3 - February 15, 2019 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 820 Supplement 63 Lavatory compartment Pilot's Operating Handbook SUPPLEMENT Lavatory compartment Table of contents Page General ..........9.63.2 Limitations .
Page 821 Supplement 63 Lavatory compartment Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, emergency procedures, normal procedures, and description necessary following the installation of the lavatory compartment option. SECTION 2 Limitations The information in this section supplements and/or replaces the information in section 2: Limitations of the standard POH.
Page 822 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 823 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 824 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 825 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 826 Supplement 63 Lavatory compartment Pilot's Operating Handbook On the magazine rack SECTION 3 Emergency Procedures The information in this section supplements and/or replaces the information in section 3: Emergency Procedures of the standard POH. 3.10 - Pressurization and air conditioning >>...
Page 827 Supplement 63 Lavatory compartment Pilot's Operating Handbook SECTION 4 Normal Procedures The information in this section supplements and/or replaces the information in section 4: Normal Procedures of the standard POH. BRIEFING to passengers to be performed before entering the airplane Normal and Emergency stowing operations of the divider.
Page 828 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 829 Supplement 63 Lavatory compartment Pilot's Operating Handbook SECTION 7 Description The information in this section supplements and/or replaces the information in section 7: Description of the standard POH. For operation, refer to equipment User's Guide. The lavatory compartment is installed against right interior upholstery panel, facing large door.
Page 830 Supplement 63 Lavatory compartment Pilot's Operating Handbook Electric connection of the system is performed via a power plug: >> Up to S/N 1407 without optional 12V power plugs (Pre-MOD70-0174-25) 28 volts >> Up to S/N 1407 with optional 12V power plugs (Post-MOD70-0174-25) 12 volts >>...
Page 831 Supplement 63 Lavatory compartment Pilot's Operating Handbook Figure 9.63.3 (1/2) -- Lavatory compartment Page 9.63.12 Edition 1 - November 16, 2016 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 832 Supplement 63 Lavatory compartment Pilot's Operating Handbook Figure 9.63.3 (2/2) -- Lavatory compartment Edition 1 - November 16, 2016 Page 9.63.13 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 833 Supplement 63 Lavatory compartment Pilot's Operating Handbook SECTION 8 Handling, Servicing and Maintenance The installation of the Lavatory compartment system does not change the handling, servicing and maintenance of the airplane described in section 8: Handling, Servicing and Maintenance of the standard POH. Page 9.63.14 Edition 1 - November 16, 2016 Rev.
Page 834 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook SUPPLEMENT JCAB Supplement for TBM940 airplane Table of contents Page General ..........9.71.2 Limitations .
Page 835 Model Basic Pilot’s Operating Handbook TBM940 From S/N 1272 Doc No. DMKFM00EEN Table 1 - Applicable coverage TC Holder DAHER AEROSPACE 23 Route de Tours 41400 SAINT-JULIEN-DE-CHEDON FRANCE (Refer to the JCAB TCDS No. 99 for details.) Aircraft Manufacturer COMPAGNIE DAHER...
Page 836 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook Type and Number of Engine, Propeller Make/Manufacturer: Pratt & Whitney Canada Model: PT6A - 66D Number: One (1) Type of Propeller: HARTZELL, HC-E5N-3C / NC8834K, 5 blades Dimensions Length: 10.736 m Width: 12.833 m Height: 4.355 m Refer...
Page 837 Supplement 71 JCAB Supplement for TBM940 airplane 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. General The limitations are the same as those in the basic EASA Approved Pilot’s Operating Handbook except: Japanese Placards On pressurized baggage compartment partition wall...
Page 838 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook (1)b For the large cargo net, on R.H. side upholstery panel, in the rear baggage compartment (1)c On FWD baggage compartment door frame (non pressurized) Above passenger's table Edition 0 - June 26, 2019 Page 9.71.5 Rev.
Page 839 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook On pilot door - External side, if installed On access door - External side Page 9.71.6 Edition 0 - June 26, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 840 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook On outer fuselage skin aft of access door In the cabin forward of access door On access door - Internal side Edition 0 - June 26, 2019 Page 9.71.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 841 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook On pilot door - Internal side, if installed On emergency exit handle Marking on cover Marking on handle (10) Above emergency exit door Page 9.71.8 Edition 0 - June 26, 2019 Rev.
Page 842 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook (11) On rear passengers masks containers >> Aircraft equipped with coat hanger (MOD70-0557-25) (12) On the L.H. Rear cargo compartment panel upper edge Occupants limits Maximum Occupancy: The number of persons on board is limited by approved seating configuration installed but must not exceed six, including the pilot.
Page 843 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook Operating limitations This airplane may be operated in the following kinds of operations when appropriate equipment is installed. ● NOTE ● Refer to the Appendix B, "Judgement table for operating method limitation." ●...
Page 844 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook Category Il operations The installed equipment for Category Il operations complies with the equipment requirements described in the Appendix 2 of the JCAB Circular No.5-002, "Criteria for approval of Category Il operations and Evaluation guideline of Category Il operations."...
Page 845 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook ADS-B (Automatic Dependent Surveillance-Broadcast) The installed ADS-B OUT complies with the equipment requirements described in the JCAB Circular No.5-019, "lmplementation Approval Criteria using ADS-B OUT", Chapter 3. The installed ADS-B OUT system is compliant with 14 CFR 91.225 and 91.227, CS ACNS.D.ADSB (1090 MHz Extended Squitter ADS-B Out), and CS ACNS.D.ELS/EHS (Mode S Elementary/Enhanced Surveillance).
Page 846 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook SECTION 3 Emergency procedures No specifics SECTION 4 Normal procedures No specifics Edition 0 - June 26, 2019 Page 9.71.13 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 847 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook SECTION 5 Performance Noise levels This aircraft complies with the requirements of Civil Aeronautics Regulations, Annex 2, ”Aircraft Noise Standard” and ICAO Annex 16, Volume I, Appendix 2, Amendment 7, Aircraft Noise, Chapter 4 (effective March 21, 2002) This Noise Document is made pursuant to Annex 16, Volume I, Attachment G to the Convention on International Civil Aviation (hereinafter referred to as "ICAO Format") and approved as a part of the Pilot’s Operating Handbook.
Page 848 2. Noise Document 4. Nationality and 5. Manufacturer and 6. Aircraft serial number registration marks: (if manufacturer's designation of necessary) aircraft: DAHER AEROSPACE TBM940 airplane 7. Engine 8. Propeller: * Pratt & Whitney Canada, HARTZELL PT6A-66D HC-E5N-3C / NC8834K 9. Maximum takeoff mass: 10.
Page 849 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook Engine emissions Fuel venting This aircraft complies with the requirements of Civil Aeronautics Regulations, Annex 3, Chapter 1. ● NOTE ● The fuel venting has been demonstrated under the ICAO Annex 16, Volume Il, Third Edition, Part Il, Chapter 2.
Page 850 Supplement 71 JCAB Supplement for TBM940 airplane 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. Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O)
Page 851 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook APPENDIX A JCAB Approved Pilot’s Operating Handbook List for TBM940 airplane Pilot’s Operating Handbook (Basic) and Pilot’s Operating Handbook Supplement(s) approved by JCAB are as below. Pilot’s Operating Pilot’s Operating Certifying Authority JCAB approval date Handbook Doc.
Page 852 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook APPENDIX B Judgement table for operating method limitation (Required equipment, etc on each operating method) Equipment, etc Mini. Operating method Gyroscopic attitude   (Note 2) indicator Gyroscopic directional  ...
Page 853 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook Category of Operating Methods A Flight under instrument flight rules (Flight under instruction of air traffic control all times) B Instrument flight (Flight in the instrument meteorological condition) C Flight under instrumental navigation (Flight over cloud or over water beyond the distance and time specified in Article 66 of the Regulations under visual meteorological condition) D Visual flight other than flight under instrumental navigation...
Page 854 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook (Note 5) Either of direction finder, VOR receiver, onboard TACAN equipment will receive radio signals which are dependent on air route related to the flight from NDB, VOR or TACAN stations which exist compose air route. However, direction finder can be substituted with GNSS receiver.
Page 855 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook APPENDIX C Table of TCD insertion Status (Template) Figure 1.1.1 - Page 9.71.22 Edition 0 - June 26, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 856 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook APPENDIX D Table of Supplemental Pilot’s Operating Handbook (Template) Edition 0 - June 26, 2019 Page 9.71.23 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 857 Supplement 71 JCAB Supplement for TBM940 airplane Pilot's Operating Handbook Intentionally left blank Page 9.71.24 Edition 0 - June 26, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 858 Supplement 72 France specifics Pilot's Operating Handbook SUPPLEMENT France specifics Table of contents Page General ..........9.72.2 Limitations .
Page 859: General
Supplement 72 France 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 French registered TBM airplane). SECTION 2 Limitations The limitations hereafter supplement or replace those of the standard airplane...
Page 860 Supplement 72 France specifics Pilot's Operating Handbook On access door - Internal side >> Airplane equipped with MOD70-0619-11E >> Airplane equipped with MOD70-0619-11H >> All On pilot door - Internal side, if installed Edition 0 - December 04, 2019 Page 9.72.3 Rev.
Page 861 Supplement 72 France specifics Pilot's Operating Handbook On emergency exit handle Marking on cover Marking on handle Above emergency exit door Page 9.72.4 Edition 0 - December 04, 2019 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 862 Supplement 72 France specifics Pilot's Operating Handbook On rear passengers masks containers On internal face of rear passengers masks containers doors >> Airplane equipped with lavatory compartment (Post-MOD70-0505-25) On access door, cabin side and toilet side Edition 0 - December 04, 2019 Page 9.72.5 Rev.
Page 863: Emergency Procedures
Supplement 72 France specifics Pilot's Operating Handbook Behind access door, cabin side and toilet side SECTION 3 Emergency procedures No specifics SECTION 4 Normal procedures No specifics SECTION 5 Performance No specifics Page 9.72.6 Edition 0 - December 04, 2019 Rev.
Page 864: Weight And Balance
Supplement 72 France specifics 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. Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70...
Page 865 Supplement 72 France specifics Pilot's Operating Handbook Intentionally left blank Page 9.72.8 Edition 0 - December 04, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 866 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook SUPPLEMENT Extended large storage cabinet Table of contents Page General ..........9.73.2 Limitations .
Page 867 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and procedures necessary for operation when the airplane is equipped with the Extended large storage cabinet option. SECTION 2 Limitations The information in this section supplements and/or replaces the information in...
Page 868 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook Inside small internal drawer, on side wall >> Cabinet equipped with electrical supply Beside 115 VAC plug SECTION 3 Emergency procedures Installation and operation of the Extended large storage cabinet do not change the emergency procedures of the airplane described in section 3 Emergency procedures of the standard POH.
Page 869 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook SECTION 5 Performance Installation and operation of the Extended large storage cabinet do not change the performance of the airplane described in section 5 Performance of the standard POH. 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 airplane is equipped with...
Page 870 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook Using the weight and balance form CAUTION ▲ ▲ Use the empty weight, arm and CG % from the weight and balance report that includes the Extended large storage cabinet option. ▲...
Page 871 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook Airplane loading form (m, kg) Moment = Weight x Arm ( Arm (m) 4.392 ) − CG (MAC %) = × 100 1.51 Weight Moment Item (kg) (m.kg) (MAC %) Empty weight (kg) Baggage 3.250...
Page 872 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook Figure 9.73.1 - Weight and balance diagram Edition 0 - February 14, 2020 Page 9.73.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 873 Supplement 73 Extended large storage cabinet 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...
Page 874 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook Figure 9.73.2 - Weight and balance diagram Edition 0 - February 14, 2020 Page 9.73.9 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 875 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook SECTION 7 Description The information in this section supplements and/or replaces the information in section 7 Description of the standard POH when the airplane is equipped with the Extended large storage cabinet option. The Extended large storage cabinet is installed at the place of the left intermediate seat.
Page 876 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook The cabinet is composed of two large drawers and a small drawer completing the storage volume of a large drawer. One large drawer opens sideways into the aisle. A small drawer is installed inside this large storage volume.
Page 877 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook The cabinet is electically supplied by the BUS 4 bar and is protected by the CABINET breaker located on frame C13bis. Circuit breakers are located under the roof of the aft large drawer (refer to A). Figure 9.73.6 - Circuit breakers and plugs List of circuit breakers located inside the cabinet : BUS 4...
Page 878 Supplement 75 Garmin GDR66 CPDLC Pilot's Operating Handbook Supplement Garmin GDR66 CPDLC Table of contents Page General ..........9.75.2 Limitations .
Page 879: General
Supplement 75 Garmin GDR66 CPDLC Pilot's Operating Handbook Section 1 General This supplement is intended to inform the pilot about the equipment limitations, descriptions and procedures necessary for operation when the airplane is equipped with the GDR66 transceiver. The information in this section supplements and/or replaces the information in section 1: General of the standard POH when the airplane is equipped with the GDR66 transceiver.
Page 880: Limitations
Supplement 75 Garmin GDR66 CPDLC Pilot's Operating Handbook Aircraft-Allocated Performance: CPDLC: RCP 130, RCP 240, RCP 400 for FANS 1/A-CPDLC Additional capabilities: Multi-frequency VDL Mode 2 1.4 - Abbreviations and terminology General abbreviations AMSL : Above Mean Sea Level Radio-navigation abbreviations CPDLC : Controller Pilot Data Link Communications : VHF Data Link...
Page 881: Emergency Procedures
Supplement 75 Garmin GDR66 CPDLC Pilot's Operating Handbook 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 airplane is equipped with the GDR66 transceiver. CPDLC FAIL Indicates that the GDR66 transceiver is inoperative or the data link is lost.
Page 882 Supplement 75 Garmin GDR66 CPDLC Pilot's Operating Handbook 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 airplane is equipped with the GDR66 transceiver. Item Weight per OPT70...
Page 883 Supplement 75 Garmin GDR66 CPDLC Pilot's Operating Handbook Section 7 Description The information in this section supplements and/or replaces the information in section 7: Description of the standard POH when the airplane is equipped with the GDR66 transceiver. 7.15 - Miscellaneous equipment The GDR 66 is a digital communications transceiver.
Page 884 Supplement 75 Garmin GDR66 CPDLC Pilot's Operating Handbook >> Airplane with G1000 Flight deck equipped with MOD70-0722-23H One CPDLC data link mode is available: Link2000+ (for Europe) >> All Refer to Garmin Pilot's Guide for further information. >> Airplane with G3000 Flight deck VHF COM3 communications ●...
Page 885 Supplement 75 Garmin GDR66 CPDLC Pilot's Operating Handbook >> Airplane with G3000 Flight deck Figure 9.75.2 - Partial electrical distribution of BUS bars Page 9.75.8 Edition 0 - March 15, 2021 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 886 Supplement 75 Garmin GDR66 CPDLC Pilot's Operating Handbook >> Airplane with G1000 Flight deck Figure 9.75.3 - Partial electrical distribution of BUS bars Edition 0 - March 15, 2021 Page 9.75.9 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 887 Supplement 75 Garmin GDR66 CPDLC Pilot's Operating Handbook >> All Section 8 Handling, servicing and maintenance Installation and operation of the GDR66 transceiver do not change the handling, servicing and maintenance of the airplane described in section 8: Handling, servicing and maintenance of the standard POH.
Page 888 Supplement 76 Buckle positioner Pilot's Operating Handbook Supplement Buckle positioner Table of contents Page General ..........9.76.2 Limitations .
Page 889: General
Supplement 76 Buckle positioner Pilot's Operating Handbook Section 1 General This supplement is intended to inform the pilot about the procedures and description necessary for operation when the airplane is equipped with the buckle positioner. Section 2 Limitations The information in this section supplements and/or replaces the information in Section 2: Limitations of the standard POH when the airplane is equipped with the buckle positioner.
Page 890: Normal Procedures
Supplement 76 Buckle positioner Pilot's Operating Handbook Section 4 Normal procedures The information in this section supplements and/or replaces the information in Section 4: Normal procedures of the standard POH when the airplane is equipped with the buckle positioner. 4.4 - Amplified procedures Inside inspection Ensure correct positioning of front seat occupiers’...
Page 891 Supplement 76 Buckle positioner Pilot's Operating Handbook 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 airplane is equipped with buckle positioner. Item Weight per OPT70...
Page 892 Supplement 76 Buckle positioner Pilot's Operating Handbook Figure 9.76.1 - Correct pre-positioning of the buckle WARNING ▲ ▲ The central buckle must be positioned so that the belt straps remain at hip level (just below the center of gravity) to prevent the body from slipping under the belts.
Page 893 Supplement 76 Buckle positioner Pilot's Operating Handbook Figure 9.76.2 - Front and rear seat belts, with movable straps and harnesses Page 9.76.6 Edition 0 - October 12, 2021 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 894 Supplement 76 Buckle positioner Pilot's Operating Handbook Fastening the seat belts on front seats Fasten the belt straps. Fasten the buckle positioner in the buckle and adjust its length so that the belt straps remain at hip level. Adjust the belt straps. Fasten and adjust the harnesses.
Page 895 Supplement 76 Buckle positioner Pilot's Operating Handbook Section 8 Handling, servicing and maintenance The buckle positioner does not change the handling, servicing and maintenance of the airplane described in Section 8: Handling, servicing and maintenance of the standard POH. Page 9.76.8 Edition 0 - October 12, 2021 Rev.
Page 896 Supplement 80 Beacon lights Pilot's Operating Handbook Supplement Beacon lights Table of contents Page General ..........9.80.2 Limitations .
Page 897 Supplement 80 Beacon lights Pilot's Operating Handbook Section 1 General This supplement is intended to inform the pilot about the description necessary for operation when the TBM airplane is equipped with beacon lights. Section 2 Limitations Installation of beacon lights does not change the limitations of the airplane described in section 2: Limitations of the standard POH.
Page 898 Supplement 80 Beacon lights Pilot's Operating Handbook 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 airplane is equipped with beacon lights. Item Weight per OPT70...
Page 899 Supplement 80 Beacon lights Pilot's Operating Handbook Section 7 Description The information in this section supplements and/or replaces the information in section 7: Description of the standard POH when the airplane is equipped with beacon lights. 7.9 - Electrical system Exterior lighting Beacon lights The airplane is equipped with two beacon lights located:...
Page 900 With MOD70-0649-00 Version A List of equipment Report reference NAV No. 34/90-RJ-App 8 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. 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.
Page 901 List of equipment Pilot's Operating Handbook List of effective pages and validities Edition 0 of March 05, 2019 Airplane equipped with MOD70-0649-00 version A Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date Title MAR 19 MAR 19 MAR 19 MAR 19 MAR 19 MAR 19 MAR 19...
Page 902 List of equipment Pilot's Operating Handbook Intentionally left blank Page 0B Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 903 List of equipment Pilot's Operating Handbook List of amendments Revision 0 dated March 05, 2019 Pages Description All pages Creation Edition 0 - March 05, 2019 Page 0C Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 904 List of equipment Pilot's Operating Handbook Intentionally left blank Page 0D Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 905 List of equipment Pilot's Operating Handbook Table of contents Page ATA 01 - Specific optional equipment ........ATA 21 - Environmental system .
Page 906 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 907 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 : - GDC72B (Air data computer) P/N 011-03734-40 - GDU1250W (Display) P/N 011-04186-00 Autopilot Altitude Hold function : - GMC710 (AFCS mode controller) P/N 011-01020-10 - GIA64W (Integrated Avionics Computer)
Page 908: 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 - March 05, 2019 Rev.
Page 909 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 0454-21A General Air System Controller (GASC) 1.98 311.02 82024A040701 (0.900) (7.900) 21-20 - Distribution Mixing unit 9723A010001 0.53 151.57...
Page 910 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 911 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) Inlet temperature sensor 93276A010001 0.11 153.54 (0.050) (3.900) Cockpit ventilated sensor 92279A010002 0.18 182.09 (0.080) (4.625) Cabin ventilated sensor 92279A010002 0.18 250.00...
Page 912: 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 913: 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 0633-34A Antenna CI105-16 0.397 237.32 (0.180) (6.028) 155.94 (3.961) 161.33 (4.098) Static dischargers 2-31 SCY (Qty: 2) Neglig.
Page 914 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) 0410-23B HF Communication System KHF1050 of which 38.03 302.70 (17.250) (7.689) - Control Display unit 1.56 155.43 (0.707) (3.948)
Page 915 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) 0564-31A G3000 COM # 2 system - Transceiver (integrated in GIA 64W Integrated Avionics Unit # 2 - refer to ATA 34-28) - VHF antenna (above fuselage) 16-21B-P3 0.86 271.65...
Page 916: 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 917: 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 Δ + 33.07 0505-25C Installation of the lavatory compartment, of which: 269.45 (Δ...
Page 918 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) 0530-25A Hi-power USB servicing plugs, of which : 0.33 188.00 (0.15) (4.775) - one 5 VDC servicing single plug (USB type) 6430202-9 - on instrument panel, pilot side - one 5 VDC servicing double plug unit (USB type) 6430202-5 - on instrument panel, front R.H.seat...
Page 919 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) Seats 0588-25A Pilot's seat T700J2500005 49.98 185.86 with seat heaters system (22.67) (4.721) 0588-25A Front R.H. seat T700J2500005 49.98 185.86 with seat heaters system...
Page 920: 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 0391-26 Portable fire extinguisher unit 74-00 - Version A (on R.H. Station R.H. Upholstering) 4.89 170.11 (2.220)
Page 921: 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 922: 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 923: 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, L.H. horizontal stabilizer 4.189 398.42 (1.900) (10.120) Deicer T700A3013003001, R.H.
Page 924 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) 30-40 - Windshield deicing Windshield heater controllers 1.984 149.61 (Qty 2 : L.H. + R.H.) TWH 93-01 (0.900) (3.800) 30-60 - Propeller deicing...
Page 925: 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 31-30 - Recorders 0455-31D Light weight Flight Data Recorder (ADRS - CARS), 5.659 256.50 of which :...
Page 926: 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 927 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) 32-40 - Wheels and brakes 0606-32 Brake assembly 30-311 14.991 204.33 (6.800) (5.190) Main tire 18x5.5-10PR 13.50 204.33 (6.123)
Page 928: 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) 0322-00 PULSELITE unit Neglig.
Page 929 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) Lights : - L.H. navigation/strobe/recognition lights 0.499 184.29 01-0771170-02 (0.227) (4.681) - R.H. navigation/strobe/recognition lights 0.499 184.29 01-0771170-01 (0.227)
Page 930: 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 Pitot L heated probe AN 5812-1 0.750 200.79 (0.340) (5.100) Pitot R heated probe AN 5812-1...
Page 931 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) 34-21 - Heading reference system 0543-34B Attitude and Heading Reference System # 1 GRS 79 3.20 171.77 (1.45) (4.363)
Page 932 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) 0585-34 - Touch Controller Unit # 1 GTC 585 and 3.99 156.69 (1.81) (3.980) - Touch Controller Unit # 2 GTC 585 3.99 156.69 (1.81)
Page 933 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) 34-43 - Radioaltimeter 0451-34D GRA 55 radar altimeter, of which : 4.127 220.47 (1.872) (5.600) - Transceiver 3.527 228.82 (1.600)
Page 934 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) 34-51 - NAV 1 installation VHF GS-NAV antenna DM N4-17N 3.307 401.57 (1.500) (10.200) Receiver (integrated in the MOD70-0564-31A GIA 64W Integrated Avionics Unit # 1 : refer to ATA 34-28) 34-52 - NAV 2 installation Receiver...
Page 935 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) 0542-34R Transponder # 2 GTX 345R - full Mode S enhanced 2.90 147.20 surveillance capability, without antenna diversity, (1.32) (3.738) with extended squitter and ADS-B IN acquisition...
Page 936: 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 with ZODIAC oxygen 22.73 226.77 masks (10.31) (5.760) 0597-35A MC10 Smartmike oxygen masks (pilot and front 1.290 188.98...
Page 937: 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 938: 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 system 0545-46A Pdf viewer installation (SD card) Neglig. 0547-46C Flight stream transceiver FS510 (SD card) Neglig.
Page 939: 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 0320-52B New ”Pilot” door 45.607 173.23 (20.687) (4.400) 0342-52 Additional landing gear doors 6.613 204.33 (3.000)
Page 940: 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 1.764 (4.020) ( 0.800) Page 36 Edition 0 - March 05, 2019 Rev.
Page 941: 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 with melting snow 200.00 - 7.716 (5.080) ( - 3.500) Edition 0 - March 05, 2019 Page 37 Rev.
Page 942: 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 0345-61 Propeller (5-blade) HC-E5N-3C / NC 8834 K 171.08 43.11 + spinner 104552P (77.60)
Page 943: 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 944: 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-26611 GEU-7/A / 32005-007 (0.445) (2.750) Power turbine tacho-generator (Np) 0.981 55.12...
Page 945: 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 0327-79A Oil pressure transmitter 0.337...
Page 946 List of equipment Pilot's Operating Handbook Intentionally left blank Page 42 Edition 0 - March 05, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

Daher TBM 940 Pilot's Information Manual

Quick Links

Chapters

Need help?

Questions and answers

Related Manuals for Daher TBM 940

Summary of Contents for Daher TBM 940