Daher TBM 930 Pilot's Information Manual

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PILOT'S INFORMATION

P/N DMJPIPYEE0 - Edition 1 - Revision 5

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 930

MANUAL

CAUTION

▲

intended for operation of the airplane.

basic Pilot's Operating Handbook.

maintained.

the Copyright.

▲

Printed in FRANCE

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Summary of Contents for Daher TBM 930

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 List of amendments Revision 1 dated April 3, 2018 Pages Description Title, Approval page Change of legal entity name from SOCATA SAS to DAHER AEROSPACE 0.9 and 0.10 List of amendments Revision 1 0.11 thru 0.20 List of effective pages and validities 6.5.1...
Page 3 Section 0 Pilot's Operating Handbook List of amendments Revision 2 dated April 8, 2019 Pages Description Title Updating of copyright date Approval page Website address updating 0.10 thru 0.12 List of amendments 0.13 thru 0.22 List of effective pages 1.4.7 Deletion of ”ESI”...
Page 4 Section 0 Pilot's Operating Handbook List of amendments Revision 2 dated April 08, 2019 (Cont'd) Pages Description 3.9.2, 3.9.3 Deletion of right windshield restriction for deicing systems 3.10.3 GAS EVENT Modification of ” ” procedure 3.10.7 Addition of Pre-MOD70-0657-34 validity 3.10.8 Addition of ”...
Page 5 Section 0 Pilot's Operating Handbook List of amendments Revision 2 dated April 08, 2019 (Cont'd) Pages Description 7.6.10 Engine air inlet : modification/addition of data related to vane deflection 7.8.19 Cabin lighting : modification/deletion of data related to floodlights 7.14.3 Addition of weather radar data 2.0.1, 2.6.6, Terminology, text moving and/or presentation...
Page 6 Section 0 Pilot's Operating Handbook List of amendments Revision 3 dated February 14, 2020 Pages Description Title Modification of the date of the copyright Approval page 0.13 to 0.16 List of amendments 0.17 to 0.26 List of effective pages 1.1.1 Addition of requirement compliance for transponder and ADS-B OUT systems 2.3.1...
Page 7 Section 0 Pilot's Operating Handbook List of amendments Revision 3 dated February 14, 2020 (Cont'd) Pages Description 5.4.1 Addition of a note explaining the curve for pressurization envelope 5.9.2 to 5.9.4 Modification of rotation airspeed graph 5.10.1, 5.10.2 Correction of conditions regarding BLEED HI message 5.10.3 to 5.10.8 Integration of a fixed torque reduction instruction when BLEED HI message ON with associated impacts on climb peformance...
Page 8 Section 0 Pilot's Operating Handbook List of amendments Revision 3 dated February 14, 2020 (Cont'd) Pages Description 2.6.2, 2.9.3, 3.1.1, Terminology, text moving and/or presentation 3.9.4, 3.9.5, 3.11.6, 3.12.12, 3.12.14, 4.4.24, 7.3.33, 7.3.34, 7.9.16 to 7.9.22, 7.14.9 to 7.14.14 Edition 1 - January 15, 2018 Page 0.15 Rev.
Page 9 3.0.3, 3.10.8 Addition of "After GDU v20.92 software" in the procedure validity (MOD70-0549-00E) Introduction of data to make this POH TBM 930 at Edition 1 valid for airplanes from S/N 1111 to 1215, equipped with MOD70-0549-00 Version E : 2.1.1 Addition of Pilot's Guide reference for airplanes up to S/N 1215 2.6.2...
Page 10 Section 0 Pilot's Operating Handbook List of amendments Revision 4 dated June 15, 2020 (Cont'd) Pages Description 6.4.19 to 6.4.21 Addition of a weight and balance sample (m,kg) for airplanes up to S/N 1159 6.4.27, 6.4.28 Addition of upholstery and cabinets data for airplanes up to S/N 1159 6.4.28, 6.4.29 Addition of seats data for airplanes up to S/N 1214...
Page 11 Section 0 Pilot's Operating Handbook List of amendments Revision 4 dated June 15, 2020 (Cont'd) Pages Description 6.4.28, 6.4.29 Addition of validity on seats for airplanes from S/N 1215 7.3.14, 7.3.15 Addition of validity on illustration for right instrument panel of airplanes from S/N 1160 7.8.14 Addition of validity for airplanes up to S/N 1160...
Page 12 Section 0 Pilot's Operating Handbook List of amendments Revision 5 dated January 20, 2021 Pages Description Title Updating of copyright date Approval page 0.19, 0.20 List of amendments 0.21 to 0.30 List of effective pages 1.4.7, 1.4.8 Addition of abbreviations 3.4.2, 3.4.3 Update of Air start procedure : instruction to keep AUX BP switch to ON for the remainder of the flight...
Page 13 Section 0 Pilot's Operating Handbook List of amendments Revision 5 dated January 20, 2021 (Cont'd) Pages Description 8.7.10 Addition of information related to the minimum oxygen cylinder pressure and requirement to purge the cylinder 1.4.7 to 1.4.10, Terminology, text moving and/or presentation 2.3.3, 2.6.9, 2.8.1, 3.9.5, 3.10.7, 3.10.8 4.3.20, 4.4.17,...
Page 14 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 1 - January 15, 2018 Page 0.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 15 Section 0 Pilot's Operating Handbook List of effective pages and validities Original issue of January 15, 2018 Airplane equipped with MOD70-0549-00 P/N DMJFM00EE1R5EN Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date Title JAN 21 0.18 JUN 20 0.19 JAN 21 0.20 JAN 21 JAN 18...
Page 16 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 2.6.4 JUN 20 1.4.1 JAN 18 2.6.5 JUN 20 1.4.2 JAN 18 2.6.6 JUN 20 1.4.3 JAN 18 2.6.7 JUN 20 1.4.4 JAN 18 2.6.8 JUN 20 1.4.5 JAN 18 2.6.9...
Page 17 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 3.0.2 JAN 18 3.0.3 JUN 20 3.7.1 JAN 18 3.0.4 JAN 18 3.7.2 JAN 18 3.0.5 APR 19 3.7.3 JAN 18 3.0.6 JAN 18 3.7.4 JAN 18 3.7.5 JAN 18 3.1.1...
Page 18 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 3.10.4 APR 19 3.12.23 JAN 18 3.10.5 APR 19 3.12.24 JAN 18 3.10.6 FEB 20 3.12.25 JAN 18 3.10.7 JAN 21 3.12.26 JAN 18 3.10.8 JAN 21 3.12.27 APR 19 3.10.9...
Page 19 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 4.3.20 JAN 21 4.4.42 APR 19 4.4.43 APR 19 4.4.1 APR 19 4.4.44 APR 19 4.4.2 JAN 18 4.4.45 FEB 20 4.4.3 JUN 20 4.4.46 APR 19 4.4.4 JAN 18 4.4.47...
Page 20 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 4.5.14 JAN 18 5.8.4 JAN 18 4.5.15 JAN 18 5.8.5 JAN 18 4.5.16 JAN 21 5.8.6 JAN 18 4.5.17 JAN 18 5.8.7 JAN 18 4.5.18 JAN 18 5.8.8 JAN 18 4.5.19...
Page 21 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 5.11.18 JAN 18 6.4.13 JUN 20 5.11.19 JAN 18 6.4.14 JUN 20 5.11.20 JAN 18 6.4.15 JUN 20 5.11.21 JAN 18 6.4.16 JUN 20 5.11.22 JAN 18 6.4.17 JUN 20 6.4.18...
Page 22 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 7.3.5 JAN 18 7.4.5 JAN 18 7.3.6 JAN 18 7.4.6 JAN 18 7.3.7 JAN 18 7.4.7 JAN 18 7.3.8 JUN 20 7.4.8 JAN 18 7.3.9 JAN 18 7.4.9 JAN 18 7.3.10...
Page 23 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 7.7.5 JAN 21 7.9.14 JAN 21 7.7.6 JAN 18 7.9.15 FEB 20 7.7.7 JAN 18 7.9.16 FEB 20 7.7.8 JAN 21 7.9.17 FEB 20 7.7.9 JAN 18 7.9.18 FEB 20 7.7.10...
Page 24 Section 0 Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date 7.14.6 JAN 18 8.7.7 JAN 18 7.14.7 JAN 18 8.7.8 JAN 21 7.14.8 JUN 20 8.7.9 JAN 21 7.14.9 JUN 20 8.7.10 JAN 21 7.14.10 FEB 20 8.7.11 JAN 18 7.14.11...
Page 25: Table Of Contents
Section 1 General Pilot's Operating Handbook Section 1 General Table of contents General ..........1.1.1 Three view drawing .
Page 26: General
Section 1 General Pilot's Operating Handbook Intentionally left blank 1.0.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 27 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 28 Section 1 General Pilot's Operating Handbook Intentionally left blank Page 1.1.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 29: 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 1 - January 15, 2018 Page 1.2.1 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 30 Section 1 General Pilot's Operating Handbook Figure 1.2.1 (2/2) - Three view drawing Page 1.2.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 31: 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 32: 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 33: 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 34: 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 35: 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 36: 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 37: 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 38: 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 39 Section 1 General Pilot's Operating Handbook : Engine Indication System EMER : Emergency ESHP : Estimated shaft horsepower : Electronic Stability Protection ESS. BUS TIE : Essential BUS tie EXT. LIGHTS : Exterior lightings ° F : Fahrenheit degree : Fuel control unit : Flight level : Fuel On Board : Flight Plan...
Page 40 Section 1 General Pilot's Operating Handbook : Interturbine temperature : Kilogram : Knot (1 nautical mile/hr - 1852 m/hr) : Kilowatt : Litre L or L.H. : Left : Litre / hour lb or lbs : Pound(s) L / D : Lift-to-drag : Landing LDG GR...
Page 41 Section 1 General Pilot's Operating Handbook : Millimetre : Maximum Landing Weight : Maximum Ramp Weight : Message MTOW : Maximum Takeoff Weight MXCL : Maximum Climb MXCR : Maximum Cruise MZFW : Maximum Zero Fuel Weight : Nautical mile NOCR : Normal cruise (recommended) NORM...
Page 42: Radio-Navigation Abbreviations
Section 1 General Pilot's Operating Handbook STALL HTR : Stall warning heater : Standard STPD : Standard Temperature Pressure Dry T° : Temperature TEMP : Temperature : Takeoff TURN COORD : Turn coordinator : Gallon U.S : Under Speed Protection : Volt or Voltage WARN : Warning...
Page 43 Section 1 General Pilot's Operating Handbook GNSS : Global Navigation Satellite System : Global Positioning System : High Frequency : Instrument Flight Rules : Instrument Landing System : Instrument Meteorological Conditions L NAV : Lateral NAVigation : Localizer Precision Vertical : Marker Radio Beacon : Navigation Indicators or Receivers P RNAV...
Page 44 Section 1 General Pilot's Operating Handbook : World Geodetic System : Weather surveillance radar XPDR : Transponder Page 1.4.10 Edition 1 - January 15, 2018 Rev. 5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 45: 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 46 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 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 47 Section 1 General Pilot's Operating Handbook 1000 Figure 1.5.3 - Inches versus millimetres Edition 1 - January 15, 2018 Page 1.5.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 48 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 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 49: 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 50: 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 51 Section 2 Pilot's Operating Handbook Limitations EASA Approved Section 2 Limitations Table of contents General ..........2.1.1 Airspeed limitations .
Page 52 Section 2 Limitations Pilot's Operating Handbook EASA Approved Miscellaneous limits ........2.7.1 Seating limits C.G.
Page 53: General
EASA Approved - General TBM 930 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 54 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.1.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 55: 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 56 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.2.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 57: 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 58: 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 59: 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 60: 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 61: 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 62 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.4.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 63: 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 64: 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 65: 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 66: 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 67 Section 2 Limitations Pilot's Operating Handbook EASA Approved >> All is installed in this airplane in accordance with AC 20-138A. is, as installed in this airplane, approved for navigation using GPS and GPS/SBAS (within the coverage of a SBAS complying with ICAO Annex 10) for IFR enroute, terminal area, and RNP APCH operations (to LNAV, LNAV/VNAV and LPV minima).
Page 68 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/ En-route, RNP 4 GNSS FDE availability Additional com- Oceanic must be verified prior to...
Page 69 Section 2 Limitations Pilot's Operating Handbook EASA Approved ICAO Flight Plan Code Approved Approved Reference Reference Phase of flight Phase of flight Operational limitations Operational limitations Notes Notes Item Item Documents Documents Capability Capability Code PBN/ Approach At a minimum, the flight EASA Includes non-...
Page 70 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 71: Gnss (Gps/Sbas) Navigation System Limitations
Section 2 Limitations Pilot's Operating Handbook EASA Approved Note 1 FDE/RAIM availability worldwide can be determined using the WFDE Prediction program, part number 006-A0154- -01 or later approved version with GARMIN GA36 and GA37 antennas selected, or : - Within the United States, using the FAA's en- -route and terminal RAIM prediction website : www.raimprediction.net, or by contacting a Flight Service Station.
Page 72 Section 2 Limitations EASA Approved Pilot's Operating Handbook Discrepancies that invalidate a procedure must be reported to Garmin International. The affected procedure is prohibited from being flown using data from the Navigation database until a new Navigation database is installed in the airplane and verified that the discrepancy has been corrected.
Page 73 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 74: 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 75: Flap Operating Envelope
Section 2 Limitations Pilot's Operating Handbook EASA Approved Since the autopilot, when operating, may mask tactile cues that indicate adverse changes in handling characteristics, use of the autopilot is prohibited when any of the visual cues specified above exist, or when unusual lateral trim requirements or autopilot trim warnings are encountered while the airplane is in icing conditions.
Page 76: Equipment Required Depending On Type Of Operation
Section 2 Limitations EASA Approved Pilot's Operating Handbook Equipment required depending on type of operation The airplane is approved for day & night VFR and day & night IFR operations when appropriate equipment is installed and operating correctly. The type certification for each use requires the following equipment. The equipment must be installed and operate perfectly according to the indicated type of use.
Page 77 Section 2 Limitations Pilot's Operating Handbook EASA Approved Day VFR Pilot instruments Airspeed indicator Sensitive and adjustable altimeter Magnetic compass with built-in compensator CAS warning and caution messages Oil pressure Low fuel pressure Fuel selector OFF Fuel auxiliary pump ON L.H.
Page 78 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 79 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 80 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 81: 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 82: 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 83: 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 84 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.6.20 Edition 1 - January 15, 2018 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 85: 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 86: Cargo Net Installation Limits
Section 2 Limitations EASA Approved Pilot's Operating Handbook Cargo net installation limits Small cargo net : maximum loading height = 28 in (710 mm) Large cargo net : maximum loading height = 22 in (565 mm) in cabin, out of baggage compartment.
Page 87: 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 figure 2.8.1. KIAS Marking Significance (Value or range) Red strip Below 65 White strip 65 - 122 Full flap operating range...
Page 88: 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 89: Placards
Section 2 Limitations Pilot's Operating Handbook EASA Approved - Placards Under L.H. front side window Calibration chart on compass and on windshield post Steer Steer DATE : RADIO ON On pressurized baggage compartment partition wall 100 kg - - 220 lbs MAXIMUM IT IS THE PILOT’S RESPONSIBILITY TO CHECK THAT ALL THE BAGGAGES ARE PROPERLY SECURED...
Page 90 Section 2 Limitations EASA Approved Pilot's Operating Handbook (3)a For the small cargo net, on frame C13bis or on the right lower upholstery panel (3)b For the large cargo net, on R.H. side upholstery panel, in the rear baggage compartment (3)c On FWD baggage compartment door frame (non pressurized) 50 kg - - 110 lbs MAXIMUM...
Page 91 Section 2 Limitations Pilot's Operating Handbook EASA Approved On pedestal console On fuel selector Near fuel tank caps Edition 1 - January 15, 2018 Page 2.9.3 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 92 Section 2 Limitations EASA Approved Pilot's Operating Handbook On internal face of L.H. engine cowling Oil system capacity 12 l 12.7 qt On landing gear emergency control access door LDG GEAR EMERGENCY ACCESS PULL Under window, at L.H. Intermediate seat (10) On rear passenger's table casing TABLE MUST BE STOWED DURING TAKEOFF AND LANDING...
Page 93 Section 2 Limitations Pilot's Operating Handbook EASA Approved (11) Under R.H. control wheel (12) On nose gear door (13) On nose gear leg NOSE LANDING GEAR TIRE PRESSURE : 6,5 bar 94 psi Edition 1 - January 15, 2018 Page 2.9.5 Rev.
Page 94 Section 2 Limitations EASA Approved Pilot's Operating Handbook (14) On main gear leg MAIN LANDING GEAR TIRE PRESSURE : 8,96 bar 130 psi (15) On engine cowling, in front of compartment door EXTERNAL POWER 28 VOLTS D.C. NOMINAL 800 AMP STARTING CAPACITY MIN DO NOT EXCEED 1000 AMP (16)
Page 95 Section 2 Limitations Pilot's Operating Handbook EASA Approved (17) On access door - External side (18) On outer fuselage skin aft of access door and in the cabin forward of access door (19) On access door - Internal side Edition 1 - January 15, 2018 Page 2.9.7 Rev.
Page 96 Section 2 Limitations EASA Approved Pilot's Operating Handbook (20) On pilot door - Internal side, if installed (21) On emergency exit handle Marking on cover Marking on handle Page 2.9.8 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 97 Section 2 Limitations Pilot's Operating Handbook EASA Approved (22) On last step of stairs STAIRS MAX LOAD : ONE PERSON (23) On R.H. access door jamb (24) On R.H. side at front seat level and on the first rear passengers masks container (R.H.
Page 98 Section 2 Limitations EASA Approved Pilot's Operating Handbook (26) On internal face of the oxygen cylinder service door (27) On the oxygen service door (28) On emergency locator transmitter inspection door (29) On the potty seat curtain, if installed, on pilot's side CURTAIN MUST BE STOWED FOR TAKE- -OFF AND LANDING Page 2.9.10 Edition 1 - January 15, 2018...
Page 99 Section 2 Limitations Pilot's Operating Handbook EASA Approved >> Airplane equipped with coat hanger (Post-MOD70-0557-25B) (30) On the L.H. rear cargo compartment panel upper edge >> Airplane equipped with coat hanger (Post-MOD70-0557-25C) (31) On the L.H. rear cargo compartment panel upper edge Edition 1 - January 15, 2018 Page 2.9.11 Rev.
Page 100 Section 2 Limitations EASA Approved Pilot's Operating Handbook Intentionally left blank Page 2.9.12 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 101 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 ........3.12.23 AP ON YD OFF .
Page 102 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook FUEL IMBALANCE ........3.8.6 FUEL LOW L .
Page 103 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook STALL HEAT ON ........7.13.3 STALL NO HEAT .
Page 104 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.A.4 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 105 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Section 3 Emergency procedures Table of contents General ..........3.1.1 Procedure format .
Page 106 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Fire and smoke ......... 3.5.1 Engine fire on ground .
Page 107 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Electrical system ........3.9.1 .
Page 108 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 3.11 Deicing system ......... 3.11.1 Leading edges deicing failure .
Page 109 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook APR DWNGRADE ........3.12.24 in A/P vertical mode during FD approach with vertical guidance...
Page 110 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.0.6 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 111: 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 112 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 113: 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 114 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 115: 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 116: 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 117: 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 118 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Engine failure after rotation ► Continuing FUEL TANK SELECTOR ......Before touch down : FLAPS lever .
Page 119: 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 120 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 121: 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. ► Fly the airplane ◄ If circumstances and obtained minimum power allow : CAUTION ▲...
Page 122 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Engine regulation discrepancy, power loss, throttle control loss ► Continuing CAUTION ▲ ▲ When MAN OVRD control is used, the available power may not be sufficient to ensure a go-around in landing configuration, particularly if the weight is near the maximum weight.
Page 123 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Engine regulation discrepancy, power loss, throttle control loss ► Continuing When runway is assured : 17 - THROTTLE ........CUT OFF 18 - FLAPS lever...
Page 124: 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 125: 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 126: Itt
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook During engine start : Starting procedure ........Abort Refer to procedure Engine start, chapter 4.4 Cancel the flight.
Page 127: 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 128: Oil Temp
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook OIL TEMP Indicates that oil temperature is below 0°C or above 104°C (possibly with OIL PRESS Oil temperature indicator ........Check If the indicated temperature is in the green sector : ►...
Page 129: 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 130: Air Start Procedures
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Air start procedures Oxygen masks ..........CAUTION ▲...
Page 131 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 132 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.4.4 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 133: 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 134: Cabin Fire On Ground
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Cabin fire on ground THROTTLE ..........CUT OFF Brakes .
Page 135: 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 136: Cabin Electrical Fire Or Smoke During Flight
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Cabin electrical fire or smoke during flight ► Fly the airplane ◄ Oxygen masks and goggles ........If the origin is known : Defective equipment breaker .
Page 137: Smoke Elimination
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Smoke elimination Oxygen masks and goggles ........BLEED switch .
Page 138 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.5.6 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 139: Emergency Descents
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved - Emergency descents Emergency descents profiles Edition 1 - January 15, 2018 Page 3.6.1 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 140: Maximum Rate Descent
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Maximum rate descent THROTTLE ..........Flight IDLE Oxygen masks .
Page 141: Maximum Range Descent
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Maximum range descent Oxygen masks ..........THROTTLE .
Page 142 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Maximum range descent ► Continuing If icing conditions : 20 - PITOT L HTR switch ....... . 21 - WINDSHIELD switch .
Page 143: 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 144: 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 145: 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 146: 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 147: 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 148: 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 149: 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 150 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 151 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 152: 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 153 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Landing with unlocked main landing gear ► Continuing If landing gear drags during landing : 11 - THROTTLE ........CUT OFF 12 - Crash lever...
Page 154: 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 155: 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 156: Ditching
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Ditching ▲ CAUTION ▲ In heavy swell with light wind, land parallel to the swell (rollers). In heavy wind, land facing wind. ▲ LANDING GEAR lever ......... . . FLAPS lever .
Page 157: Landing Without Elevator Control
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Landing without elevator control LANDING GEAR lever ......... . FLAPS lever .
Page 158 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.7.16 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 159: 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 160: Fuel Press
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 161: Aux Boost Pmp On
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 162: 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 163: 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 164: 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 165: 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 166 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.8.8 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 167 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. ▲...
Page 168 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 169 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved LOW VOLTAGE Normal functioning with GENERATOR selector on MAIN. Voltmeter voltages ......... .
Page 170 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 171 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved MAIN GEN LOW VOLTAGE ► Continuing GENERATOR selector ......If altitude is >...
Page 172 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook MAIN GEN LOW VOLTAGE ► Continuing PITOT R & STALL HTR ....OFF/LDG/TAXI light .
Page 173 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 174 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 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 175 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Bus bar NOTE : BREAKERS ON C13 BIS FRAME Figure 3.9.1 (2/3) - Electrical distribution of bus bars Edition 1 - January 15, 2018 Page 3.9.9 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 176 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 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 177 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Total loss of electrical power Maintain airplane control. Use the MD302 for attitude, airspeed and/or altitude ► Fly the airplane ◄ ► Land as soon as possible ◄ ● NOTE ● Airplane power is provided to the MD302 display for normal operation.
Page 178 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.9.12 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 179 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 180 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook PRESSU OFF ► Continuing If on ground : BLEED switch ......... . . Taxi back to apron.
Page 181 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 182 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 1 - January 15, 2018 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 183 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 184 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 185 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved >> Without the EDM evolution patch (Pre-MOD70-0657-34) and prior to GDU v20.92 GARMIN software version (Pre-MOD70-0549-00E or F) CABIN ALTITUDE USE OXYGEN MASK ● NOTE ● CABIN ALTITUDE is followed by USE OXYGEN MASK and the “Use oxygen mask / Use oxygen mask”...
Page 186 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook >> With the EDM evolution patch (Post-MOD70-0657-34) or after GDU v20.92 GARMIN software version (Post-MOD70-0549-00E or F) ● NOTE ● may come on 45 seconds after CABIN ALTITUDE USE OXYGEN MASK EDM performs a 90°...
Page 187 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved CABIN DIFF PRESS Indicates a cabin pressure differential over 6.4 PSI ± 0.2 PSI. Pressurization indicator ........Check If ΔP >...
Page 188 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Cabin not depressurized after landing If ΔP cabin remains > 0 : DUMP switch ......... Actuate BLEED switch .
Page 189 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 190 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook DOOR Indicates that one of the door latches of the door(s) is not correctly locked. On ground : Check the correct locking, as well as the latches position of the door(s). DOOR is still ON : Do not take off.
Page 191 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved VACUUM LOW Low vacuum may lead to malfunctioning of leading edge deicing and pressurization. Monitor the normal functioning of leading edge deicing and pressurization. If necessary : Altitude ........Below 10000 ft Return to VMC conditions as soon as possible.
Page 192 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Defog malfunction If moisture starts to quickly cover the inside of the windscreen with the HOT AIR FLOW distributor already turned to the left : HOT AIR FLOW distributor ......Set to around a 10 o’clock position If moisture continues :...
Page 193: Deicing System
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 3.11 - Deicing system Leading edges deicing failure Symptoms : failure on one of the two pneumatic deicing pulses : ice on wing outboard sections, or, ice on wing inboard sections and stabilizers, one of the two cycling green lights is not lit.
Page 194: Prop Deice Fail
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook PROP DEICE FAIL Symptoms : propeller deicing green light is not lit, propeller vibrations............Reduce ►...
Page 195: 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 196: Windshield Deicing Failure
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Windshield deicing failure Symptoms : windshield being covered uniformly by ice, no perception of heat when touching deiced section, windshield deicing green light is not lit. If symptoms result from overheat : WINDSHIELD switch .
Page 197: 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 198: Pitot No Ht L-R
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook PITOT NO HT L-R Indicates that : - corresponding pitot tube heating has failed or - PITOT L HTR switch or PITOT R & STALL HTR switch is not ON while the engine is running.
Page 199: Stall No Heat
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved STALL NO HEAT Indicates that : - stall warning vane heating has failed or - PITOT R & STALL HTR switch is not ON while the engine is running. Correct operation of the aural stall warning may be altered by severe or prolonged icing.
Page 200 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 3.11.8 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 201: Miscellaneous
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 3.12 - Miscellaneous Trim Runaway ► Fly the airplane ◄ AP / TRIM DISC push-button ......Press and hold The three trim tabs are disconnected and runaway stops.
Page 202: Crack In Cockpit Window Or Window Panel
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Crack in cockpit window or window panel ► Fly the airplane ◄ Descend slowly. Cabin ∆P ..........Reduce By setting Landing Field Elevation to 10000 ft End of procedure.
Page 203: Emergency Exit Use
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Emergency exit use Check that the anti-theft safety pin has been removed. 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 204: Emergency Beacon (Elt) Use
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Emergency beacon (ELT) use Before a forced landing : If possible : Transmit a MAY DAY signal on COM VHF 121.5 MHz or on a known ATC frequency. After landing : ELT remote control switch .
Page 205: Inadvertent Spins
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Inadvertent spins WARNING ▲ ▲ Voluntary spins are prohibited. ▲ AP / TRIM DISC push-button ... . Press and Hold until recovery Control wheel .
Page 206: Ap Off, Stall Warning
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 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 207: Aural Wrn Fail
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 208: Aural Wrn 1 Chnl
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook AURAL WRN 1 CHNL ● NOTE ● System switches automatically on the remaining valid aural channel. ● End of procedure. Page 3.12.8 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 209: Esp Fail
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved ESP FAIL Indicates pitch, roll, high speed and AoA protections are inoperative. ► Fly the airplane ◄ Maintain the airplane inside the flight envelope. Flaps UP 105 < KIAS < 266 Flaps TO 100 <...
Page 210: Esp Degraded - Ias
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook ESP DEGRADED - IAS Indicates high speed protection is inoperative. ► Fly the airplane ◄ Maintain IAS below 266 KIAS. Continue flight. Inform maintenance department. End of procedure. Page 3.12.10 Edition 1 - January 15, 2018 Rev.
Page 211: Esp Degraded - Aoa
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 212: Oxygen Use
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Oxygen use With or without USE OXYGEN MASK WARNING ▲ ▲ Smoking is strictly prohibited when the oxygen system is in use. Before using oxygen, remove any trace of oil, grease, soap and other fatty substances (including lipstick, make-up, etc...).
Page 213 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Oxygen use ► Continuing If possible : 12 - Perform an emergency descent ....To an altitude below 10000 ft For intermediate and rear seats :...
Page 214: Airspeed Indicating System Failure
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook Airspeed indicating system failure Symptoms : erroneous indication in flight. PITOT L HTR switch ........Check ON PITOT R &...
Page 215: Flight Into Severe Icing Conditions
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 216: Cargo Door
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 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 217: Gpu Door
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 218: Ignition
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook IGNITION Indicates that ignition exciter is running. IGNITION switch ........Check position If weather permits : IGNITION switch...
Page 219: Ap On Yd Off
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 220: Autopilot Or Electric Pitch Trim Malfunction
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 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 221 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 222: Dual Gps/Sbas Failure Dr Or Loi Annunciation On Hsi)
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 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 223: Abort Apr
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved ABORT APR Indicates a loss of GPS navigation. ► Perform a go-around◄ End of procedure. Edition 1 - January 15, 2018 Page 3.12.23 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 224: Apr Dwngrade
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 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 225: Pit In Ap Vertical Mode During Fd Approach With Vertical Guidance
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 226: Vdi Vdi
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 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 227: Left Pfd Failure
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved Left PFD failure ► Fly the airplane ◄ At takeoff : Fly the airplane manually ... . . Using stand-by instruments AP / TRIM DISC push-button .
Page 228: Ahrs Failure
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook AHRS failure Symptoms : Autopilot is disconnected On PFD(s) : Comparator window and/or and/or annunciation(s) On PFD(s) : Reversionary sensor window BOTH ON AHRS1 BOTH ON AHRS2 annunciation Lost systems : AHRS1 or AHRS2 Autopilot (AP) Systems still operative :...
Page 229 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved AHRS failure ► Continuing and/or and/or If all annunciations go off, refer to following condition. BOTH ON AHRS1 BOTH ON AHRS2 annunciation not associated to and/or and/or annunciation(s) : PFD1 and PFD2 SENSOR softkeys .
Page 230: Adc Failure
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook ADC failure Symptoms : On PFD(s) : Comparator window and/or annunciation(s) On PFD(s) : Reversionary sensor window BOTH ON ADC1 BOTH ON ADC2 annunciation Lost systems : ADC1 or ADC2 Actions : Autopilot is still operative.
Page 231: Mfd Failure
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 232: Xpdr1 Fail Xpdr2 Fail
Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook XPDR1 FAIL XPDR2 FAIL Indicates transponder 1 [or transponder 2] is inoperative. ► Fly the airplane ◄ If transponder 2 [or transponder 1] is available : Set transponder 2 [or transponder 1] as active. Continue flight.
Page 233: Xpdr1 Ads-B Fail Xpdr2 Ads-B Fail
Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 234 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 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 235 Section 3 Emergency procedures Pilot's Operating Handbook EASA Approved 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 236 Section 3 Emergency procedures EASA Approved Pilot's Operating Handbook 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 237 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 238 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before taxiing ......... . . 4.4.37 Taxiing .
Page 239: 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 240 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 4.1.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 241: 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 242 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Intentionally left blank Page 4.2.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 243: 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 244 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Inside inspection ► Continuing 21 - INERT SEP ........... 22 - PARK BRAKE .
Page 245: Before Starting Engine
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before starting engine Crash lever ........... . ATIS .
Page 246: 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 247: 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 248: After Engine Start With Gpu
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook After engine start with GPU SOURCE ........... . BATT .
Page 249: Before Taxiing
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before taxiing Stand-by instruments ......... Check DE ICE SYSTEM .
Page 250: Before Line Up
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before line up LDG lights ............
Page 251: Normal Takeoff
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Normal takeoff ADI, HSI, headings ......... . . Check PROP RPM .
Page 252: Short Takeoff
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Short takeoff ADI, HSI, headings ......... . . Check PROP RPM .
Page 253: After Takeoff
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved After takeoff LANDING GEAR ......... Check UP FLAPS .
Page 254: Climb
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Climb ALT SEL ........... Check Altimeters setting .
Page 255: Cruise
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Cruise Altimeters setting ..........Check Autopilot .
Page 256: Before Descent
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before descent Briefing before approach ........Completed Altimeters setting .
Page 257: Approach
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Approach Altimeters setting (QNH) ........Set / Check Minimums .
Page 258: Final Approach (In Gs) Or Downwind Leg (Vmc)
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Final approach (in GS) or downwind leg (VMC) LDG lights ........... . . LANDING GEAR .
Page 259: Short Final (≈ 500 Ft)
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Short final (≈ 500 ft) LANDING GEAR ..........Check DN and 3 green FLAPS...
Page 260: Runway Clear
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Runway clear TAXI light ............
Page 261: Shutdown
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Shutdown 1 - PARK BRAKE ..........Set / ON 2 - EXT LIGHTS .
Page 262 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Shutdown ► Continuing 20 - Oxygen cylinder (right wing fairing) ......Close 21 - Install air inlet and static port plugs, and exhaust and pitot covers.
Page 263: 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 264 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 265 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 3/16 ► Continuing Initial inside inspection Cockpit CAUTION ▲ ▲ When engine is shut down, do not set the PROP DE ICE switch to ON for more than 10 seconds, damage to the propeller blades could result. ▲...
Page 266 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 4/16 ► Continuing CAUTION ▲ ▲ When the engine is shut down, the throttle must not be moved into the reverse area as a lack of hydraulic pressure prevents movement into reverse range.
Page 267 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 5/16 ► Continuing ENGINE START panel 25 - IGNITION switch ....... . . AUTO or OFF ●...
Page 268 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 6/16 ► Continuing 38 - LANDING GEAR lever ......... . . 39 - SOURCE selector .
Page 269 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 7/16 ► Continuing DE ICE SYSTEM panel 46 - All switches ..........47 - ICE LIGHT switch .
Page 270 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 8/16 ► Continuing 57 - PITOT R & STALL HTR switch ......●...
Page 271 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 9/16 ► Continuing 68 - Baggage compartment ....... . Straps in place >>...
Page 272 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 10/16 ► Continuing L.H. wing III 73 - Flap ..........Condition / Play Also inspect the lower surface, as well as flap fairing, where pebbles (and even ice in case of slush on the runway) may have accumulated.
Page 273 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 11/16 ► Continuing 80 - Left pitot ..........Condition 81 - Wing lower surface...
Page 274 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 12/16 ► Continuing ● NOTE ● If airplane has been used from muddy airfields or in snow, check wheel wells to make sure they are clean and not obstructed. Check frequently all landing gear retraction mechanism components, shock-absorbers, tires and brakes.
Page 275 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 13/16 ► Continuing ● NOTE ● Inspect if possible pressure port located inside exhaust stub. A missing port or a cracked port may hinder correct operation of continuous heating of air inlet lip. ●...
Page 276 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 14/16 ► Continuing 103 - Propeller and spinner ..No nicks, cracks or oil leaks / Attachment ● NOTE ● In case of operation from contaminated runways, it is necessary to carefully examine propeller blades, where traces of abrasion may be found.
Page 277 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Preflight inspection 15/16 ► Continuing R.H. main LANDING GEAR 110 - Shock absorber ........Check 111 - Doors .
Page 278 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Preflight inspection 16/16 ► Continuing 129 - ELT door ......... . . Closed / Locked ●...
Page 279: 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 280 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Inside inspection ► Continuing 10 - PASSENGER OXYGEN switch ....... . . STBY 11 - OXYGEN switch...
Page 281 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Inside inspection ► Continuing 22 - IGNITION switch ..........AUTO ●...
Page 282 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. ▲ 38 - MAN OVRD control ......Full backward (notched) CAUTION ▲...
Page 283: 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 284 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 285 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before starting engine ► Continuing 27 - PARK BRAKE ......... . Check ON ●...
Page 286: Engine Start
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Engine start STROBE switch ..........G3000 .
Page 287 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 288 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Engine start ► Continuing When Ng > 50 % and, 1 minute max : CAUTION ▲ ▲ If the starter does not go off automatically, disengage it using the ABORT position of the STARTER switch. ▲...
Page 289: 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 290 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 291 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Motoring ► Continuing 23 - STARTER switch ........ABORT Then OFF 24 -...
Page 292: 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 293 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Motoring followed by an engine start ► Continuing 13 - Motor ..........For 30 sec.
Page 294 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Motoring followed by an engine start ► Continuing Electric power 26 - MAIN GEN ........Check OFF Reset if necessary ●...
Page 295: 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 296: 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 297 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 298: In-Flight Available Oxygen Quantity
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook In-flight available oxygen quantity (Crew oxygen masks in NORMAL mode) Oxygen pressure ..........Read Outside air temperature (OAT) .
Page 299: Before Taxiing
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before taxiing Stand-by instruments ......... Check Check de-ice system ●...
Page 300 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before taxiing ► Continuing ......... . . Increase >...
Page 301 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before taxiing ► Continuing 15 - Pitch trim ..........UP / DN 16 - Pitch trim...
Page 302 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before taxiing ► Continuing CAUTION ▲ ▲ During feathering test, keep the spent time with the propeller RPM in the caution (yellow) range at a minimum. ▲ 31 - THROTTLE ......... FEATHER twice Flight IDLE to LO-IDLE then Flight IDLE, twice 32 -...
Page 303: 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 304: 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 305 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before line up ► Continuing Adjust trims for takeoff 17 - Pitch ........... . Adjust inside green index sector, depending on the current balance condition 18 -...
Page 306 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before line up ► Continuing 29 - CAS display ..........Check All messages OFF, PARK BRAKE...
Page 307 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Before line up ► Continuing 41 - Rotation airspeed (V ........Check 42 - Pilot's / Passengers' belts...
Page 308: Normal Takeoff
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Normal takeoff When lined up, on brakes : CAUTION ▲ ▲ If heavy precipitation, turn IGNITION and INERT SEP switches to ON. If icing conditions are foreseen, refer to chapter 4.5, paragraph Flight into known icing conditions.
Page 309 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Normal takeoff ► Continuing 11 - Rotation airspeed 12 - Attitude ........... . 10°...
Page 310: 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 311 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Short takeoff ► Continuing 10 - Brakes ........... . Release ●...
Page 312 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Short takeoff ► Continuing In case of initial climb at Vx : WARNING ▲ ▲ It is recommended not to retract FLAPS to UP before 500 ft AGL. ▲ 17 - Airspeed .
Page 313: After Takeoff
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved After takeoff LANDING GEAR lever ........Check UP FLAPS lever .
Page 314: Climb
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Climb ALT SEL ........... Check Altimeters setting .
Page 315 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Climb ► Continuing A/C panel 10 - TEMP selector ..........Adjust 11 - FUEL gages...
Page 316: Cruise
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Cruise Altimeters setting ..........Check Autopilot .
Page 317 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Cruise ► Continuing CAUTION ▲ ▲ If heavy precipitation, turn IGNITION and INERT SEP switches to ON. ▲ 12 - DE ICE SYSTEM panel ......As required Refer to chapter 4.5 13 -...
Page 318: Before Descent
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Before descent Briefing before approach ........Completed Altimeters settings .
Page 319: Approach
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Approach Altimeters settings (QNH) ....... . . Set / Check Minimums .
Page 320: 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 321: 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 322: 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 323: 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 324 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 325: 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 326: Touch And Go
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Touch and go Before wheels touch : WARNING ▲ ▲ Reduce power smoothly. Quickly reducing the power to idle during the flare may induce a pronounced deceleration which may lead to a drop down of the airplane.
Page 327 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Touch and go ► Continuing WARNING ▲ ▲ Confirm that flaps have reached the TO position before increasing power. Do not increase power with full flaps, as airplane may lift off prematurely at low speed. ▲...
Page 328: 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 329: Shutdown
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Shutdown PARK BRAKE ..........Set ON PARK BRAKE .
Page 330 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 to be heard to confirm that the AUX BP is functional.
Page 331 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 1 - January 15, 2018 Page 4.4.69 Rev.
Page 332: Outside Check After Shutdown
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Outside check after shutdown Oxygen cylinder (right wing fairing) ......Close Install air inlet and static port plugs, and exhaust and pitot covers.
Page 333: 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 334 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 335 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Flight into known icing conditions ► Continuing INERT SEP ON ........Check ON AIRFRAME DE ICE switch .
Page 336 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Flight into known icing conditions ► Continuing 12 - WINDSHIELD switch ........●...
Page 337 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Flight into known icing conditions ► Continuing Ice accumulation effects When ice has accumulated on the unprotected surfaces of the airplane, aerodynamic characteristics may be changed. Particularly stall airspeeds may increase by up to : FLAPS UP 20 KIAS FLAPS TO...
Page 338: Flight Into Severe Icing Conditions
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Flight into severe icing conditions The following weather conditions may be conducive to severe in-flight icing : Visible rain at temperatures below 0°C ambient air temperature, Droplets that splash or splatter on impact at temperatures below 0°C ambient air temperature.
Page 339: Flight Under Heavy Precipitations
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Flight under heavy precipitations IGNITION switch ..........●...
Page 340: Utilization On Runways Covered With Melting Or Not Tamped Snow
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization on runways covered with melting or not tamped snow If required : Refer to paragraph Utilization by cold weather and very cold weather. CAUTION ▲ ▲ When engine is shut down, do not set the PROP DE ICE switch to ON for more than 10 seconds, damage to the propeller blades could result.
Page 341 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization on runways covered with melting or not tamped snow ► Continuing Rotation airspeed ..... Increased by 5 KIAS ●...
Page 342 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization on runways covered with melting or not tamped snow ► Continuing Touch and Go : WARNING ▲ ▲ Touch and Go is prohibited. ▲ On the ramp, after landing or taxiing : 18 - Do not use the parking brake to prevent brake lock.
Page 343: Utilization On Icy Or Covered With Tamped Snow Runways 1/2
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization on icy or covered with tamped snow runways 1/2 If required : Refer to paragraph Utilization by cold weather and very cold weather. CAUTION ▲ ▲ When engine is shut down, do not set the PROP DE ICE switch to ON for more than 10 seconds, damage to the propeller blades could result.
Page 344 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization on icy or covered with tamped snow runways 2/2 ► Continuing Takeoff : 11 - After takeoff, normally retract the landing gear, then perform a complete cycle (extension / retraction) at IAS < 150 KIAS. Before landing : 12 - IGNITION switch...
Page 345: Utilization By Cold Weather (0°C To - 25°C) And Very Cold Weather (- 25°C To - 40°C)
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) ● NOTE ● The procedure hereafter supplements the normal procedures for the airplane use when operating under temperatures between 0°...
Page 346: Utilization By Cold Weather (- 40°C) To - 25°C) And Very Cold Weather (- 25°C To - 440°C)) - Envelope
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 1 ● NOTE ● The procedure hereafter supplements the normal procedures for the airplane use when operating in the Envelope 1 defined in figure 4.5.1.
Page 347: 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 1 ► Continuing 12 - PITOT L HTR switch ....... . 13 - PITOT R &...
Page 348 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 1 ► Continuing 22 - PARK BRAKE ........Check OFF ●...
Page 349: Utilization By Cold Weather (- 0°C To - 25°C) And Very Cold Weather (- 25°C To - 40°C) - Envelope 3
Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 2 ● 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 350 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 2 ► Continuing 11 - IGNITION switch ......ON during 30 seconds 12 - IGNITION...
Page 351 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 2 ► Continuing ▲ CAUTION ▲ When the engine is shut down, the THROTTLE must not be moved into the reverse area.
Page 352 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 2 ► Continuing When Ng > 50% : CAUTION ▲ ▲ If the starter does not go off automatically, disengage it using the ABORT position of the STARTER switch.
Page 353 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 2 ► Continuing After engine start : As soon as the current flow is lower than 100 A : A/C panel 46 - A/C switch...
Page 354 Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 3 ● NOTE ● The procedures defined for the Envelope 2 are also applicable for the Envelope 3.
Page 355 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization by cold weather (- 0°C to - 25°C) and very cold weather (- 25°C to - 40°C) - Envelope 3 ► Continuing Landing / After landing / Shutdown / 10 - Perform procedures defined for Envelope 1.
Page 356: Landing Procedure With Strong Headwind Or Crosswind 1/2
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Landing procedure with strong headwind or crosswind 1/2 If landing must be performed with strong headwind or crosswind : Increase approach airspeed by the greatest of these 2 following values : ( headwind 10 ) −...
Page 357 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Landing procedure with strong headwind or crosswind 2/2 ► Continuing Before touch-down : Generate a slideslip with the rudder in order to align fuselage with the runway (ie left crosswind, left wing low). Immediately after landing : CAUTION ▲...
Page 358: Utilization On Grass Runway
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook Utilization on grass runway ▲ CAUTION ▲ The small wheels of the airplane and its weight may lead it to sink in soaked or soft ground. ▲ Before planning the landing, ensure that the field is hard, smooth and dry enough. Landing and moreover takeoff shall not begin if any doubt exists about the condition of such a runway.
Page 359 Section 4 Normal procedures Pilot's Operating Handbook EASA Approved Utilization on grass runway ► Continuing ● NOTE ● Under 40 KIAS, using the reverse makes a cloud of solid particles (dusts, sand, gravels, cut grass, ...) appear around the front face of the airplane. This will damage the propeller and, after ingestion, the engine internal components (compressor and turbine blades).
Page 360: Gps Navigation
Section 4 Normal procedures EASA Approved Pilot's Operating Handbook GPS navigation Set up conditions Verify if the data base is current. Verify that altitude data is valid for the GPS prior to flight. Check the systems availability requirements in the table 2.6.1 in section 2 / GNSS (GPS/SBAS) navigation equipment approvals, depending on the planned navigation performance.
Page 361 Section 5 Performance Pilot's Operating Handbook Section 5 Performance Table of contents General ..........5.1.1 Noise level .
Page 362 Section 5 Performance Pilot's Operating Handbook 5.10 Climb performance ........5.10.1 MXCL - Speeds (IAS = 124 KIAS) .
Page 363 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 1 - January 15, 2018 Page 5.1.1 Rev.
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Page 365: Noise Level
Section 5 Performance Pilot's Operating Handbook EASA Approved - Noise level Maximum noise level Demonstrated noise permitted level FAR PART 36, 88 dB(A) 76.4 dB(A) Appendix G - Amdt 28 ICAO, Annex 16, Vol. 1, 6th edition, Amdt 8 85 dB(A) 76.4 dB(A) Chapter 10, Appendix 6 Approved noise levels for TBM airplane are stated in EASA.A.010 Type Certificate...
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Page 367: 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 368 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 1 - January 15, 2018...
Page 369: 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.
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Page 371: Sat - Oat Conversions
Section 5 Performance Pilot's Operating Handbook - SAT - OAT conversions ● NOTE ● These indicated temperatures are available for stabilized cruise at normal operating power. ● ISA - 20°C ISA - 10°C ISA + 10°C ISA + 20°C Pressure altitude (feet) - 05...
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Page 373: 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)
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Page 375: 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 1 - January 15, 2018 Page 5.7.1 Rev.
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Page 377: 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 378 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.
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Page 380 Section 5 Performance Pilot's Operating Handbook Maximum climb power (FL < 200) - 124 KIAS Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 381 Section 5 Performance Pilot's Operating Handbook Maximum climb power (FL > 200) - 124 KIAS Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 382: Maximum Climb Power (Fl < 200) - 170 Kias / M 0.40
Section 5 Performance Pilot's Operating Handbook Maximum climb power (FL < 200) - 170 KIAS / M 0.40 Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 383: Maximum Climb Power (Fl >200) - 170 Kias / M 0.40
Section 5 Performance Pilot's Operating Handbook Maximum climb power (FL > 200) - 170 KIAS / M 0.40 Conditions : If BLEED HI msg ON, reduce TRQ by 5 % ● NOTE ● : Add 0.5 % of TRQ for each additional 10 KIAS on climb airspeed. Table not valid if INERT SEP ON and/or BLEED HI msg ON.
Page 384: 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 385: 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 386 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 387 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°...
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Page 389: 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 390: 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 391: 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 392: 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 393: 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 394 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 395: 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 396 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 397 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 398: 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 ●NOTE ●...
Page 399 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 ●NOTE ●...
Page 400 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 ●NOTE ●...
Page 401: 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 402: 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 403: 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 1 - January 15, 2018 Page 5.11.1 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 404 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 405 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 406 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 407 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 408 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 409 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 410 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 411 Section 5 Performance Pilot's Operating Handbook Normal cruise (Recommended) 7100 lbs 6300 lbs Figure 5.11.9 - Cruise performance (Recommended cruise) Edition 1 - January 15, 2018 Page 5.11.9 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 412 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 413 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 414 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 415 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 416: Normal Cruise (Recommended)
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 417 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 418 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 419: Long Range Cruise (5500 Lbs - 2495 Kg)
Section 5 Performance Pilot's Operating Handbook Long range cruise (5500 lbs - 2495 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure altitude...
Page 420 Section 5 Performance Pilot's Operating Handbook Long range cruise (5500 lbs - 2495 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure altitude...
Page 421: Long Range Cruise (6300 Lbs - 2858 Kg)
Section 5 Performance Pilot's Operating Handbook Long range cruise (6300 lbs - 2858 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure altitude...
Page 422 Section 5 Performance Pilot's Operating Handbook Long range cruise (6300 lbs - 2858 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure altitude...
Page 423: Long Range Cruise (7100 Lbs - 3220 Kg)
Section 5 Performance Pilot's Operating Handbook Long range cruise (7100 lbs - 3220 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure altitude...
Page 424 Section 5 Performance Pilot's Operating Handbook Long range cruise (7100 lbs - 3220 kg) Conditions : Landing gear and flaps UP BLEED switch on AUTO and BLEED HI msg OFF Legend : OAT : °C IAS : KIAS USG/h kg/h TAS : KTAS Pressure altitude...
Page 425: 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...
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Page 427: 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...
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Page 429: 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 430: 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 431: 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 432: 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 433 Section 6 Weight and balance Pilot's Operating Handbook Section 6 Weight and balance Table of contents General ..........6.1.1 Airplane weighing procedures .
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Page 435: 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 436 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.1.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 437 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.
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Page 439: 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 440 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 441 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.
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Page 443: 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 444: 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 to 6.4.6, appropriate to the chosen units.
Page 445 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 1 - January 15, 2018 Page 6.4.3 Rev.
Page 446: 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 >> Up to S/N 1159 Weight Moment Item (kg) (m.kg) (MAC %) (1a)
Page 447 Section 6 Weight and balance Pilot's Operating Handbook >> Up to S/N 1159 Weight Item (kg) (1a) Empty weight Baggage (2a) (< 50 kg) (2a) Front seats -17.5 kg per seat (2a) removed Inter. seats (2a) -24 kg per seat (2a) removed Rear...
Page 448 Section 6 Weight and balance Pilot's Operating Handbook ( Arm (m) 4.392 ) − CG (MAC %) = × 100 Moment = Weight x Arm 1.51 >> From S/N 1160 Weight Moment Item (kg) (m.kg) (MAC %) (1a) (1b) (1c) Empty weight (kg) Baggage...
Page 449 Section 6 Weight and balance Pilot's Operating Handbook >> From S/N 1160 Weight Item (kg) (1a) Empty weight Baggage (2a) (< 50 kg) (2a) Front seats -15 kg per seat (2a) removed * Inter. seats (2a) -20.5 kg per seat (2a) removed * Rear...
Page 450: 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 6.4.8 Edition 1 - January 15, 2018...
Page 451 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 1 - January 15, 2018 Page 6.4.9 Rev.
Page 452: 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 >> Up to S/N 1159 Weight Moment Item (kg)
Page 453 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.3 - Weight and balance diagram Edition 1 - January 15, 2018 Page 6.4.11 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 454 Section 6 Weight and balance Pilot's Operating Handbook ( Arm (m) 4.392 ) − CG (MAC %) = × 100 Moment = Weight x Arm 1.51 >> From S/N 1160 Weight Moment Item (kg) (m.kg) (MAC %) Empty weight (kg) Baggage (<...
Page 455 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.4 - Weight and balance diagram Edition 1 - January 15, 2018 Page 6.4.13 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 456: 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 >> Up to S/N 1159 Weight Moment Item (lbs)
Page 457 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.5 - Weight and balance diagram Edition 1 - January 15, 2018 Page 6.4.15 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 458 Section 6 Weight and balance Pilot's Operating Handbook ( Arm (in) 172.93 ) − CG (MAC %) = × 100 Moment = Weight x Arm 59.45 >> From S/N 1160 Weight Moment Item (lbs) (in) (in.lbs) (MAC %) Empty weight (lbs) Baggage (<...
Page 459 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.6 - Weight and balance diagram Edition 1 - January 15, 2018 Page 6.4.17 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 460 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.4.18 Edition 1 - January 15, 2018 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 461: Weight And Balance Samples (M, Kg)
Section 6 Weight and balance Pilot's Operating Handbook Weight and balance samples (m, kg) >> Up to S/N 1159 CAUTION ▲ ▲ Loading samples - see figure 6.4.7 or 6.4.8 - are only given as an example ; for calculation concerning your airplane, refer to the diagram corresponding to its validity.
Page 462 Section 6 Weight and balance Pilot's Operating Handbook ( Arm (m) 4.392 ) − CG (MAC %) = × 100 Moment = Weight x Arm 1.51 >> Up to S/N 1159 Weight Moment Item (kg) (m.kg) (MAC %) Empty weight (kg) 2 126 4.738...
Page 463 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.7 - Loading sample (in kg and m) Edition 1 - January 15, 2018 Page 6.4.21 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 464 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.4.22 Edition 1 - January 15, 2018 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 465: Weight And Balance Samples (In, Lbs)
Section 6 Weight and balance Pilot's Operating Handbook Weight and balance samples (in, lbs) >> From S/N 1160 CAUTION ▲ ▲ Loading samples - see figure 6.4.7 or 6.4.8 - are only given as an example ; for calculation concerning your airplane, refer to the diagram corresponding to its validity.
Page 466 Section 6 Weight and balance Pilot's Operating Handbook ( Arm (in) 172.93 ) − CG (MAC %) = × 100 Moment = Weight x Arm 59.45 >> From S/N 1160 Weight Moment Item (lbs) (in) (in.lbs) (MAC %) Empty weight (lbs) 4 638 186.3...
Page 467 Section 6 Weight and balance Pilot's Operating Handbook Figure 6.4.8 - Loading samples (in lbs and in) Edition 1 - January 15, 2018 Page 6.4.25 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 468: 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 469 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 470 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) R.H. low + top pilot case support 9.70 203.74 (4.400) (5.175) 0557-25A - Upholstery Version 2017, of which : Neglig.
Page 471 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) - RH. intermediate seat (back to or in flight 38.58 224.80 direction) - Up to S/N 1159 (17.50) (5.710) 0553-25A...
Page 472 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.4.30 Edition 1 - January 15, 2018 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 473: 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 6, 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 474 Section 6 Weight and balance Pilot's Operating Handbook Intentionally left blank Page 6.5.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 475 Section 7 Description Pilot's Operating Handbook Section 7 Description Table of contents General ..........7.1.1 Airframe .
Page 476 Section 7 Description Pilot's Operating Handbook Powerplant ..........7.6.1 Turboprop engine operation .
Page 477 Section 7 Description Pilot's Operating Handbook 7.10 Emergency oxygen system ....... 7.10.1 Flight above 15000 ft with possible emergency descent .
Page 478 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.0.4 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 479: 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 Integrated Flight Deck Pilot's Guide.
Page 480 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.1.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 481: 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 482 Section 7 Description Pilot's Operating Handbook Figure 7.2.1 - Cabin arrangement 6-seat accommodation Page 7.2.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 483 Section 7 Description Pilot's Operating Handbook Figure 7.2.1A - Cabin arrangement 4-seat accommodation with large securing net Edition 1 - January 15, 2018 Page 7.2.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 484 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 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 485: 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 486 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 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 487 Section 7 Description Pilot's Operating Handbook Figure 7.2.2 (2/2) - Wing flaps Edition 1 - January 15, 2018 Page 7.2.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 488 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.2.8 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 489: 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 490 Section 7 Description Pilot's Operating Handbook >> Before digital hourmeter installation (Pre-MOD70-0533-31A) An hourmeter is located above circuit breakers panel. >> All 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.
Page 491 Section 7 Description Pilot's Operating Handbook the airspeed indicator, the landing gear control unit, the flap geared motor, the idle position sensor. 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...
Page 492 Section 7 Description Pilot's Operating Handbook Figure 7.3.1 - Instrument panel assembly (Typical arrangement) Page 7.3.4 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 493 Section 7 Description Pilot's Operating Handbook Intentionally left blank Edition 1 - January 15, 2018 Page 7.3.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 494 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 7.6.4 ELECTRIC POWER switches - see figure 7.8.5 INT LIGHTS internal lighting switches - see figure 7.8.7...
Page 495 Section 7 Description Pilot's Operating Handbook Figure 7.3.2 (2/2) - Upper panel and cockpit overhead panel Edition 1 - January 15, 2018 Page 7.3.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 496 Section 7 Description Pilot's Operating Handbook DISPLAY BACKUP, A/C CONTROL and SEATS HTRS MASTER (Post-MOD70-0588-25) panels - see figure 7.9.3 General alarm red and amber indicators PFD 1 MD302 Landing gear configuration and control panel - see figure 7.5.1 Parking brake control - see figure 7.5.6 Left station control wheel tube Deicing control and check panel - see figure 7.13.1 L.H.
Page 497 Section 7 Description Pilot's Operating Handbook Figure 7.3.3 (2/2) - Left instrument panel (Typical arrangement) Edition 1 - January 15, 2018 Page 7.3.9 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 498 Section 7 Description Pilot's Operating Handbook Stand-by compass BARO knobs Registration AFCS control unit Touchscreen controllers PRESSURIZATION panel - see figure 7.9.1 Micro LDR LVL push-button Figure 7.3.4 (1/2) - Central instrument panel Page 7.3.10 Edition 1 - January 15, 2018 Rev.
Page 499 Section 7 Description Pilot's Operating Handbook Figure 7.3.4 (2/2) - Central instrument panel (Typical arrangement) Edition 1 - January 15, 2018 Page 7.3.11 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 500 Section 7 Description Pilot's Operating Handbook >> Up to S/N 1159 PFD 2 DISPLAY BACKUP push-button Right station control wheel tube Crew music Adjustable air outlet Right station reception-micro jacks Hourmeter R. H. station rudder pedals adjusting handle Circuit breakers panel postlight Cigar lighter and two USB servicing plugs Cabin emergency air control (EMERGENCY RAM AIR control knob) Static source selector...
Page 501 Section 7 Description Pilot's Operating Handbook Figure 7.3.5 (2/2) - Right instrument panel (Typical arrangement) - Up to S/N1159 Edition 1 - January 15, 2018 Page 7.3.13 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 502 Section 7 Description Pilot's Operating Handbook >> From S/N 1160 PFD 2 DISPLAY BACKUP push-button Right station control wheel tube Crew music Adjustable air outlet Right station reception-micro jacks R. H. station rudder pedals adjusting handle Circuit breakers panel postlight USB servicing plugs Cabin emergency air control (EMERGENCY RAM AIR control knob) Static source selector...
Page 503 Section 7 Description Pilot's Operating Handbook Figure 7.3.5A (2/2) - Right instrument panel (Typical arrangement) - From S/N 1160 Edition 1 - January 15, 2018 Page 7.3.15 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 504 Section 7 Description Pilot's Operating Handbook >> All THROTTLE FLAPS lever THROTTLE friction adjustment Manual FUEL TANK SELECTOR - see figure 7.7.2 Roll trim tab control MAN OVRD emergency fuel regulation lever Pitch trim tab control Lock for access door to landing gear emergency pump - see figure 7.5.2 Figure 7.3.6 (1/2) - Pedestal console Page 7.3.16 Edition 1 - January 15, 2018...
Page 505 Section 7 Description Pilot's Operating Handbook Figure 7.3.6 (2/2) - Pedestal console (Typical arrangement) Edition 1 - January 15, 2018 Page 7.3.17 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 506 Section 7 Description Pilot's Operating Handbook Figure 7.3.7 - Circuit breakers panel Page 7.3.18 Edition 1 - January 15, 2018 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 507 Section 7 Description Pilot's Operating Handbook Figure 7.3.8 - General alarms warning lights Edition 1 - January 15, 2018 Page 7.3.19 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 508: Doors, Windows And Emergency Exit
Section 7 Description Pilot's Operating Handbook Doors, windows and emergency exit Cabin access door - see figure 7.3.9 The cabin one-piece access door, located on the left side of fuselage aft of the wings, opens outside. The retractable stairs and hand rail make boarding easier. To open the door from outside the airplane (make sure the door is not locked), press on front end of the handle embedded in door (this pressure disengages the handle from its recess), then turn the handle upwards.
Page 509 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 510 Section 7 Description Pilot's Operating Handbook Figure 7.3.9 - Cabin access door Page 7.3.22 Edition 1 - January 15, 2018 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 511 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 512 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 513 Section 7 Description Pilot's Operating Handbook Figure 7.3.9A - Cockpit access door (pilot door) Edition 1 - January 15, 2018 Page 7.3.25 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 514 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 515 Section 7 Description Pilot's Operating Handbook Figure 7.3.10 - Emergency exit Edition 1 - January 15, 2018 Page 7.3.27 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 516: Seats, Belts And Harnesses
Section 7 Description Pilot's Operating Handbook Seats, belts and harnesses >> Airplane with seat heaters (Post-MOD70-0588-25) Heated seats - see figure 7.3.11 Cockpit and cabin seats are equipped with a heating system for the comfort of 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,...
Page 517 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 1 - January 15, 2018 Page 7.3.29 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 518 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 519 Section 7 Description Pilot's Operating Handbook >> All 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 520 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 521 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 522: 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 523 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 524 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 525: 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 526 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 527 Section 7 Description Pilot's Operating Handbook Figure 7.3.12 (2/2) - Seats Edition 1 - January 15, 2018 Page 7.3.39 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 528 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 529 Section 7 Description Pilot's Operating Handbook Figure 7.3.12A (2/2) - Seats Edition 1 - January 15, 2018 Page 7.3.41 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 530 Section 7 Description Pilot's Operating Handbook >> All Figure 7.3.13 - Front and rear seat belts,with movable straps, and harnesses Page 7.3.42 Edition 1 - January 15, 2018 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 531: 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 532 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 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 533 Section 7 Description Pilot's Operating Handbook Figure 7.4.1 (2/2) - Roll Edition 1 - January 15, 2018 Page 7.4.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 534 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 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 535 Section 7 Description Pilot's Operating Handbook Figure 7.4.2 (2/2) - Lateral trim Edition 1 - January 15, 2018 Page 7.4.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 536: 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 537 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 1 - January 15, 2018 Page 7.4.7 Rev.
Page 538 Section 7 Description Pilot's Operating Handbook Figure 7.4.3 (2/2) - Elevator Page 7.4.8 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 539 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 1 - January 15, 2018 Page 7.4.9 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 540 Section 7 Description Pilot's Operating Handbook Figure 7.4.4 (2/2) - Pitch trim Page 7.4.10 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 541: 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 542 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 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 543 Section 7 Description Pilot's Operating Handbook Figure 7.4.5 (2/2) - Rudder Edition 1 - January 15, 2018 Page 7.4.13 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 544 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 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 545 Section 7 Description Pilot's Operating Handbook Figure 7.4.6 (2/2) - Rudder trim Edition 1 - January 15, 2018 Page 7.4.15 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 546 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.4.16 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 547: 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 548: 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 displayed 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 549 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 1 - January 15, 2018 Page 7.5.3 Rev.
Page 550: 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 551 Section 7 Description Pilot's Operating Handbook Figure 7.5.2 - Emergency landing gear extension control Edition 1 - January 15, 2018 Page 7.5.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 552: 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 553 Section 7 Description Pilot's Operating Handbook Figure 7.5.3 - Minimum turn diameter (Full rudder pedals travel without using differential braking) Edition 1 - January 15, 2018 Page 7.5.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 554 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 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 555: Brake System
Section 7 Description Pilot's Operating Handbook Brake system - see figure 7.5.5 The airplane is equipped with a hydraulically actuated disc braking system installed on the main landing gear wheels. Each toe brake at pilot and front passenger stations is equipped with a master cylinder which sends hydraulic pressure to the corresponding disc brake : left pedals, left-side brake ;...
Page 556 Section 7 Description Pilot's Operating Handbook Reservoir Vent R.H. station master cylinders PARK BRAKE control knob PARK BRAKE valve Drain Pilot's station master cylinders L.H. brake assembly R.H. brake assembly Figure 7.5.5 (1/2) - Brake system Page 7.5.10 Edition 1 - January 15, 2018 Rev.
Page 557 Section 7 Description Pilot's Operating Handbook Figure 7.5.5 (2/2) - Brake system Edition 1 - January 15, 2018 Page 7.5.11 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 558 Section 7 Description Pilot's Operating Handbook Figure 7.5.6 - Brake system Page 7.5.12 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 559: 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 560 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 561 Section 7 Description Pilot's Operating Handbook Figure 7.6.1 (2/2) - Powerplant Edition 1 - January 15, 2018 Page 7.6.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 562: Engine Control Levers
Section 7 Description Pilot's Operating Handbook Engine control levers - see figure 7.6.2 Engine operation requires use of two levers located on pedestal console in cabin : THROTTLE (Item 1), and its detent for reverse (Item 4) MAN OVRD control for emergency fuel regulation (Item 3). ●...
Page 563 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 564 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 565: Engine Instruments
Section 7 Description Pilot's Operating Handbook Engine instruments Engine indicating consists of : engine torque expressed in percent (%), TRQ propeller speed in RPM, PROP RPM generator rotation speed expressed in percent (%), Ng ITT expressed in °C, oil pressure expressed in PSI. oil temperature expressed in °C.
Page 566: Engine Starting
Section 7 Description Pilot's Operating Handbook Engine starting - see figure 7.6.4 Ignition function Ignition system consists of an ignition unit and two spark igniter plugs in powerplant, a three-position IGNITION switch OFF - AUTO - ON located on ENGINE START panel at upper panel.
Page 567 Section 7 Description Pilot's Operating Handbook Figure 7.6.4 - Engine starting Edition 1 - January 15, 2018 Page 7.6.9 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 568: 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 569 Section 7 Description Pilot's Operating Handbook Compressor turbine tacho-generator (Ng) Compressor turbine tacho-generator (Ng) is attached on accessory gearbox. It supplies a voltage which is transmitted to the GARMIN system for display on the MFD, under normal display conditions. Power turbine tacho-generator (Np) Power turbine tacho-generator is attached on the right side of the reduction gearbox.
Page 570: Propeller
Section 7 Description Pilot's Operating Handbook Propeller Airplane is equipped with a composite five-bladed, constant-speed and full-feathering propeller. Regulation Propeller governor located on engine maintains rotation speed to the nominal value of 2000 RPM. Regulation is obtained through propeller blade pitch variation : counterweights drive propeller blades toward high pitch (low RPM) whereas oil pressure delivered by governor drives back blades toward low pitch (high RPM).
Page 571: Fuel System
Section 7 Description Pilot's Operating Handbook - Fuel system - see figure 7.7.1 The fuel system comprises fuel tanks, fuel unit, selectors, manual and automatic, electric and mechanical boost pumps, engine fuel system, gaging installation, monitoring installation and drains. Fuel tanks Fuel tanks are formed by sealed casings in each wing.
Page 572 Section 7 Description Pilot's Operating Handbook Flow divider Fuel unit Flowmeter Filter drain Collector tank Fuel return pipe Fuel regulator Filling port High pressure pump (HP) NACA scoop Oil to fuel heater Tank vent valve Low pressure switch Fuel level gages Fuel jet Tank drain valve Main mechanical boost pump...
Page 573 Section 7 Description Pilot's Operating Handbook Figure 7.7.1 (2/2) - Fuel system Edition 1 - January 15, 2018 Page 7.7.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 574: Automatic Tank Selector
Section 7 Description Pilot's Operating Handbook Automatic tank selector - see figures 7.7.2 and 7.7.3 Automatic tank selection allows, without pilot's intervention, feeding the engine from one tank or the other in predetermined sequences. These sequences depend on airplane configuration (ground, in-flight, fuel low level CAS messages appearance). Automatic tank selection system comprises an electronic sequencer, an actuator attached on the fuel unit, FUEL SEL two-position selector (AUTO, MAN) and SHIFT push-knob located on FUEL panel.
Page 575: 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 576 Section 7 Description Pilot's Operating Handbook Figure 7.7.2 - Manual selector of fuel tanks Page 7.7.6 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 577 Section 7 Description Pilot's Operating Handbook AUX BP switch FUEL SEL switch SHIFT push-button Figure 7.7.3 - Fuel control panel Edition 1 - January 15, 2018 Page 7.7.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 578: 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 579: Fuel System Draining And Clogging Indicator
Section 7 Description Pilot's Operating Handbook Fuel system draining and clogging indicator - see figure 7.7.4 The fuel system comprises five drain points, a drain on the filter bowl, two drain valves on each tank, located on wing lower surface, one at wing root and the other past main landing gear well.
Page 580 Section 7 Description Pilot's Operating Handbook Lighting switch Mirror door Clogging indicator Central access door Filter drain Tank drain Drain bowl Figure 7.7.4 - Fuel system draining points and clogging indicator Page 7.7.10 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 581: Electrical System
Section 7 Description Pilot's Operating Handbook - Electrical system - see figures 7.8.1, 7.8.2 and 7.8.5 The airplane is fitted with a 28-volt direct-current electrical system. Electrical supply is obtained from various power supplies : a starter generator a stand-by generator a battery a ground power unit, via a plug, located on L.H.
Page 582: 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 583: 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 584: 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 585 Section 7 Description Pilot's Operating Handbook Figure 7.8.1 - Electrical diagram Edition 1 - January 15, 2018 Page 7.8.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 586 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 587 Section 7 Description Pilot's Operating Handbook Figure 7.8.3 - (1/3) - Electrical distribution of bus bars Edition 1 - January 15, 2018 Page 7.8.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 588 Section 7 Description Pilot's Operating Handbook NOTE : BREAKERS ON C13 BIS FRAME Figure 7.8.3 (2/3) - Electrical distribution of bus bars Page 7.8.8 Edition 1 - January 15, 2018 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 589 Section 7 Description Pilot's Operating Handbook Figure 7.8.3 (3/3) - Electrical distribution of bus bars Edition 1 - January 15, 2018 Page 7.8.9 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 590 Section 7 Description Pilot's Operating Handbook Essential bus NORM & EMER switch ESS BUS TIE 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 591 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 STORM Stormscope protection, if installed AIRFRAME DE ICE...
Page 592 Section 7 Description Pilot's Operating Handbook BUS 2 (Cont'd) SATCOM SATCOM protection, if installed SATCOM HEATER SATCOM heater protection, if installed 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...
Page 593 Section 7 Description Pilot's Operating Handbook >> Up to S/N 1159 Figure 7.8.4 (4/5) - Breaker panel (Typical arrangement) Edition 1 - January 15, 2018 Page 7.8.13 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 594 Section 7 Description Pilot's Operating Handbook >> From S/N 1160 Figure 7.8.4 (5/5) - Breaker panel (Typical arrangement) Page 7.8.14 Edition 1 - January 15, 2018 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 595: Indicating
Section 7 Description Pilot's Operating Handbook >> All 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...
Page 596 Section 7 Description Pilot's Operating Handbook MAIN reset knob ST-BY reset knob Crash lever SOURCE selector GENERATOR selector Figure 7.8.5 - Electrical control Page 7.8.16 Edition 1 - January 15, 2018 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 597: Exterior Lighting
Section 7 Description Pilot's Operating Handbook Exterior lighting - see figure 7.8.6 The airplane is equipped with three strobe and navigation lights, two landing lights, two taxi lights, two recognition lights and a wing leading edge icing inspection light. Landing lights The landing lights are embedded in the winglets' leading edge.
Page 598 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 599 Section 7 Description Pilot's Operating Handbook Taxi and landing light switch Pulselite system switch Navigation lights switch Strobe lights switch Figure 7.8.6 - External lighting controls Edition 1 - January 15, 2018 Page 7.8.19 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 600: Interior Lighting
Section 7 Description Pilot's Operating Handbook Interior lighting - see Figure 7.8.7 Interior lighting consists of access, cabin, instrument panel, instruments, baggage compartment and emergency lighting. Access lighting Access lighting consists of two floodlights located on the ceiling upholstering (one at the level of the access door, the other at the level of the storage cabinet) and the L.H.
Page 601 Section 7 Description Pilot's Operating Handbook Instrument panel lighting switch (rheostat) DIMMER switch Cabin lighting switch (rear seats reading light) Access door, baggage compartment and FWD dome light (delayed breaker) push-button Emergency lighting switch Breaker panel lighting switch Figure 7.8.7 (1/2) - Internal lighting controls Edition 1 - January 15, 2018 Page 7.8.21 Rev.
Page 602 Section 7 Description Pilot's Operating Handbook Figure 7.8.7 (2/2) - Internal lighting controls Page 7.8.22 Edition 1 - January 15, 2018 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 603: Air Conditioning And Pressurization
Section 7 Description Pilot's Operating Handbook - Air conditioning and pressurization ● NOTE ● A list of abbreviations used in this chapter is given in figure 7.9.2. ● The airplane is equipped with a Global Air System (GAS), which ensures air conditioning and pressurization control - see figure 7.9.2.
Page 604: 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 605: Cabin Pressurization Control System
Section 7 Description Pilot's Operating Handbook System operation See figure 7.9.3. The BLEED switch allows selection of the engine bleed air system, provided that the engine is running. The Ground Fan (GF) operates until takeoff, when BLEED switch is set to AUTO, and MAIN GEN is OFF.
Page 606 Section 7 Description Pilot's Operating Handbook Cabin altitude management To maximize comfort during all phases of flight, the cabin altitude is automatically computed by the GASC using flight parameters (such as airplane altitude, altitude rate of change) provided by the avionics. During descent, the GASC uses the Landing Field Elevation (LFE) to manage the optimal cabin altitude rate of change so that the airplane lands with a cabin altitude equal to LFE minus 200 ft.
Page 607 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 the 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 608: Dual-Zone Environmental Control System
Section 7 Description Pilot's Operating Handbook Dual-zone Environmental Control System (ECS) The ECS controls both the cockpit and cabin heating and cooling functions. The ECS consists of two independent air circuits : Heating circuit, controlled by the Temperature Conditioning System (TCS) Cooling circuit, controlled by the Vapor Cycle Cooling System (VCCS) Heating circuit The TCS regulates hot air coming from the bleed air system (also used for...
Page 609 Section 7 Description Pilot's Operating Handbook into the cabin by passing through : the overhead duct equipped with swiveling and adjustable air outlets, ports located on the floor between the cabinets and the intermediate passenger seats. System operation See figure 7.9.3 and the paragraph : Air temperature management. A/C control panel selection : If the A/C switch is set to OFF : >>...
Page 610 Section 7 Description Pilot's Operating Handbook >> After the GASC software update(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 611 Section 7 Description Pilot's Operating Handbook System protection Power for the ECS is supplied by the BUS 2 bar and is protected by the AIR COND breaker. Four fans are supplied by BUS 4 bar and protected respectively by following breakers : COND FAN, CABIN FAN, COCKPIT FAN and GND FAN.
Page 612 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 613 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 the 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 614 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 adjust the air to the desired temperature.
Page 615 Section 7 Description Pilot's Operating Handbook Cabin override Setting the switch to the 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 616 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 adjust the air to the desired temperature.
Page 617 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 618 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.9.16 Edition 1 - January 15, 2018 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 619 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 620 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 621 Section 7 Description Pilot's Operating Handbook Figure 7.9.2 (3/3) -- GAS Edition 1 - January 15, 2018 Page 7.9.19 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 622 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 7.9.3 (1/2) - GAS controls Page 7.9.20 Edition 1 - January 15, 2018 Rev.
Page 623 Section 7 Description Pilot's Operating Handbook Figure 7.9.3 (2/2) - GAS controls Edition 1 - January 15, 2018 Page 7.9.21 Rev. 5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 624 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.9.22 Edition 1 - January 15, 2018 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 625: Emergency Oxygen System
Section 7 Description Pilot's Operating Handbook 7.10 - Emergency oxygen system - see figure 7.10.1 The gaseous oxygen system is to be used by the crew and the passengers when the cabin altitude is greater than 10000 ft following a loss of pressurization, or if there is smoke or fumes in the cabin.
Page 626 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 four passenger masks, when the OXYGEN switch is set to ON.
Page 627 Section 7 Description Pilot's Operating Handbook a regulator equipped with : a two-position N-100% control tab that selects between a mix of cabin air and oxygen (NORMAL mode) and 100% oxygen (100% mode), an EMERGENCY rotating knob with a PRESS TO TEST function. ●...
Page 628 Section 7 Description Pilot's Operating Handbook MICRO/MASK switch OXYGEN switch PASSENGER OXYGEN switch Figure 7.10.1 - Emergency oxygen system Page 7.10.4 Edition 1 - January 15, 2018 Rev. 5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 629 Section 7 Description Pilot's Operating Handbook Harness inflation side vanes N (Normal) – 100% regulator control tab EMERGENCY control knob PRESS TO TEST function Vent valve Figure 7.10.2 - Crew oxygen masks - Regulator controls Edition 1 - January 15, 2018 Page 7.10.5 Rev.
Page 630 Section 7 Description Pilot's Operating Handbook >> Airplane equipped with MC10 Smart Mike oxygen masks Figure 7.10.3 - Crew oxygen masks - Noise reduction switch Page 7.10.6 Edition 1 - January 15, 2018 Rev. 5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 631: Flight Above 15000 Ft With Possible Emergency Descent
Section 7 Description Pilot's Operating Handbook >> All Flight above 15000 ft with possible emergency descent Minimum oxygen pressure (PSIG) for following conditions : Crew oxygen masks in NORMAL mode. 4 minutes of utilization by each pilot and passenger from 31000 ft to 15000 ft. Plus 30 minutes of utilization by each pilot and passenger at 15000 ft.
Page 632: 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 : Crew oxygen masks in NORMAL mode. Flight above 15000 ft. All equipment in use. 1 hour of utilization by each pilot and passenger.
Page 633: 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 : Crew oxygen masks in NORMAL mode. Flight under 15000 ft. 90 minutes of utilization by each pilot and one passenger. Plus 30 minutes of utilization by each pilot at 10000 ft.
Page 634 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.10.10 Edition 1 - January 15, 2018 Rev. 5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 635: Air Data System And Instruments
Section 7 Description Pilot's Operating Handbook 7.11 - Air data system and instruments - see figure 7.11.1 The airplane air data system consists of : Primary systems : two separate static pressure systems, two separate dynamic pressure systems. An alternate static pressure system. Static pressure systems Primary systems Two dual static ports (one on each side of the fuselage tail section) supply a dual...
Page 636: Dynamic Pressure System
Section 7 Description Pilot's Operating Handbook Dynamic pressure systems Dynamic pressure is provided by two heated pitot probes, one installed under each wing. The left probe supplies ADC 1 and the standby instrument. The right probe supplies ADC 2. Each line has a drain plug located in the root of the wing. Pitot heating Pitot heating is controlled by PITOT L HTR and PITOT R &...
Page 637 Section 7 Description Pilot's Operating Handbook Intentionally left blank Edition 1 - January 15, 2018 Page 7.11.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 638 Section 7 Description Pilot's Operating Handbook Pitot L Dynamic system drain Standby instrument ADC 1 ADC 2 Forward pressure bulkhead Static system drain Static system drain Static system drain Alternate static system drain Static source switching valve (Normal / Alternate) Instrument panel Dynamic system drain Pitot R...
Page 639 Section 7 Description Pilot's Operating Handbook Figure 7.11.1 (2/2) - Air data system Edition 1 - January 15, 2018 Page 7.11.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 640 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.11.6 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 641: Vacuum System And Instruments
Section 7 Description Pilot's Operating Handbook 7.12 - Vacuum system and instruments - see figure 7.12.1 The airplane is fitted with a vacuum system providing the suction necessary to operate the cabin pressurization and the leading edge deicing. Vacuum system includes : A pressure regulator An ejector A regulating and relief valve...
Page 642 Section 7 Description Pilot's Operating Handbook Pressure regulator Ejector Valve Regulating and relief valve Pressure switch Failure CAS message Figure 7.12.1 (1/2) - Vacuum system Page 7.12.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 643 Section 7 Description Pilot's Operating Handbook Figure 7.12.1 (2/2) - Vacuum system Edition 1 - January 15, 2018 Page 7.12.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 644 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.12.4 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 645: Ice Protection Equipment
Section 7 Description Pilot's Operating Handbook 7.13 - Ice protection equipment - see figure 7.13.1 Ice protection equipment is as follows : Pneumatic deice system for inboard, central and outboard wing and for stabilizers : AIRFRAME DE ICE Propeller electrical deice system : PROP DE ICE Windshield electrical deice system : WINDSHIELD Electrical heating system for both pitots and for the stall warning sensor : PITOT L HTR and PITOT R &...
Page 646: Propeller Deicing
Section 7 Description Pilot's Operating Handbook Propeller deicing Propeller deicing is accomplished through electrical heating of blade roots. This system operates cyclically and alternately on the inboard and outboard zones of all blades. Each cycle is 180 seconds long. The system operation is correct when green warning light located above PROP DE ICE switch illuminates.
Page 647: Heating Of Pitots And Stall Warning Sensor (Pitot L Htr And Pitot R & Stall Htr)
Section 7 Description Pilot's Operating Handbook Heating of pitots and stall warning sensor (PITOT L HTR and PITOT R & STALL HTR) The two pitots, which supply ADCs, the airspeed indicator and the stall warning sensor are electrically heated. This deice equipment must be used even during flight into non-icing conditions.
Page 648 Section 7 Description Pilot's Operating Handbook Figure 7.13.1 - Deicing control and check panel Page 7.13.4 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 649: Miscellaneous Equipment
Section 7 Description Pilot's Operating Handbook 7.14 - Miscellaneous equipment Stall warning system The airplane is equipped with an electrically deiced stall sensor in the leading edge of the right wing. This sensor fitted with a vane is electrically connected to an audible warning.
Page 650: Static Dischargers
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 651: Weather Radar Gwx 70
Section 7 Description Pilot's Operating Handbook Weather radar GWX 70 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 652 Section 7 Description Pilot's Operating Handbook Radar mode Area of weather display Antenna stabilization status Touchscreen controllers Scale for weather display Figure 7.14.1 (1/2) - GWX 70 Weather radar display and controls Page 7.14.4 Edition 1 - January 15, 2018 Rev.
Page 653 Section 7 Description Pilot's Operating Handbook Figure 7.14.1 (2/2) - GWX 70 Weather radar display and controls Edition 1 - January 15, 2018 Page 7.14.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 654: 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 655: 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 656: 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 657: Data Collection And Transmission System (Fastbox), If Installed
Section 7 Description Pilot's Operating Handbook Data collection and transmission system (FASTBOX), if installed 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 658 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 659 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 660 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 661 Section 7 Description Pilot's Operating Handbook Under certain circumstances when the GNSS integrity requirement is not met, the approach may be aborted. This is annunciated through ABORT APR , while the service level annunciation is no longer displayed on 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 662 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 663: Optional Equipment
Section 7 Description Pilot's Operating Handbook Optional equipment For optional equipment such as stormscope, SVS or TAWS, refer to section 9 Supplements. Other optional equipment such as radio altimeter or chartview system or TAS are described in the GARMIN Pilot's Guide. ●...
Page 664 Section 7 Description Pilot's Operating Handbook Intentionally left blank Page 7.14.16 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 665 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 666 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook 8.10 Utilization by cold weather (- 0°C to - 25°C) or very cold weather (- 25°C to - 40°C) ..... 8.10.1 Page 8.0.2 Edition 1 - January 15, 2018...
Page 667: 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 668 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.1.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 669: 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 670 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.2.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 671: 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 672 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.3.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 673: 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 674 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.4.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 675: 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 676 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.5.2 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 677: 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 678: 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 679 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Figure 8.6.1 - Turning angle limits Edition 1 - January 15, 2018 Page 8.6.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 680: 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 681 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Figure 8.6.2 - Control lock device Edition 1 - January 15, 2018 Page 8.6.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 682 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.6.6 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 683: 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 684: 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 685 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 686 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 687 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 688 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 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 689: 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 690: Oxygen
Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Oxygen The oxygen replenishment device is installed directly on the oxygen cylinder head. It consists of a charging valve and a pressure gauge graduated from 0 to 2000 PSIG. A chart - see figure 8.7.4, located on the inside of the cylinder service door, gives the maximum cylinder charge pressure for the ambient temperature.
Page 691 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 692 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook If the pressure on the oxygen cylinder gauge is lower than the maximum for the cylinder temperature : Fill the oxygen cylinder. The minimum pressure for the oxygen cylinder is 217 PSIG (15 bars). CAUTION ▲...
Page 693 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 694 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 695 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 696 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Page 8.7.14 Edition 1 - January 15, 2018 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 697: 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 698: 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 699: 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 ▲ ▲ For all cabin layouts, make sure that access to emergency exit is free at all times. ▲ CAUTION ▲ ▲ Removed equipment items must be stored in a manner that ensures their integrity.
Page 700 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. >>...
Page 701 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook D - Removal of intermediate seats - see figures 8.9.2 and 8.9.3 To remove intermediate seats, perform the following operations Install protective covers. Pull backrest bottom upholstery (25) to remove it. >>...
Page 702 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook E - Removal of a cabinet ● NOTE ● This operation must be carried out by a service center. ● F - Cabin comfort - see figure 8.9.3 Blank off the hot air outlet, located forward the large door, with blanking device assy (33) stored in storage bag - see figure 8.9.3 detail A.
Page 703 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Position the seat and put lock (22) near the color mark (37) made on rail bottom on aisle side. ● NOTE ● The color mark (37) in the rail is aligned with red marks (36). ●...
Page 704 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Conversion of 4-seat accommodation into 6-seat accommodation - see 2 -- figures 8.9.1, 8.9.2, 8.9.3 and 8.9.4 A - Tools and consumable materials Seat protective covers B - Preparation Make sure the SOURCE selector is set to OFF and the crash lever is down.
Page 705 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook E - Installation of intermediate seats Install intermediate seats – refer to paragraph 1 G. If removed, install the baggage compartment partition net. If removed, install cabin central carpet. F - Installation of rear seats - see figure 8.9.1 Make sure the work area is clean and free from debris.
Page 706 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Additional configurations 3 -- WARNING ▲ ▲ Removed seats can only be reinstalled at their original locations. Rear seats (L.H. or R.H.) are the only ones that can be installed in the rear seat zone along the cabin axis on both central rails.
Page 707 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Intentionally left blank Edition 1 - January 15, 2018 Page 8.9.9 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 708 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Seat tilting handle Ring Lock Rail Backrest tilting handle Quick link Knob Strap Seats heaters connector, if installed Figure 8.9.1 (1/2) - Removal / installation of rear seat Page 8.9.10 Edition 1 - January 15, 2018 Rev.
Page 709 Section 8 Handling, servicing and maintenance Pilot's Operating Handbook Figure 8.9.1 (2/2) - Removal / installation of rear seat Edition 1 - January 15, 2018 Page 8.9.11 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 710 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 (if installed) Figure 8.9.2 - Removal / installation of intermediate seat Page 8.9.12 Edition 1 - January 15, 2018 Rev.
Page 711 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 1 - January 15, 2018 Page 8.9.13 Rev.
Page 712 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 8.9.14 Edition 1 - January 15, 2018 Rev. 4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 713 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 714 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 715 With MOD70-0549-00 List of equipment Report reference NAV No. 34/90-RJ-App 6 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 716 List of equipment Pilot's Operating Handbook List of effective pages and validities Edition 1 of January 15, 2018 Airplane equipped with MOD70-0549-00 Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date Title JUN 20 JUN 20 JUN 20 JUN 20 JUN 20 JUN 20 JUN 20 JAN 18...
Page 717 List of equipment Pilot's Operating Handbook Page Edit./Rev. Rev. Date Page Edit./Rev. Rev. Date JUN 20 JUN 20 JUN 20 JUN 20 JUN 20 JUN 20 JUN 20 Page 0B Edition 1 - January 15, 2018 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 718 List of equipment Pilot's Operating Handbook List of amendments Revision 0 dated January 15, 2018 Pages Description All pages Creation Edition 1 - January 15, 2018 Page 0C Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 719 List of amendments Revision 1 dated April 3, 2018 Pages Description Title Change of legal entity name from SOCATA SAS to DAHER AEROSPACE List of effective pages and validities List of amendments Revision 1 4 thru 42 Removal of equipment manufacturer name...
Page 720 List of equipment Pilot's Operating Handbook List of amendments Revision 2 dated April 8, 2019 Pages Description Title Updating of the date on the copyright List of effective pages and validities 0E and 0F List of amendments Revision 2 Terminology Edition 1 - January 15, 2018 Page 0E Rev.
Page 721 List of equipment Pilot's Operating Handbook List of amendments Revision 3 dated June 15, 2020 Pages Description Title Updating of the date on the copyright 0A, 0B List of effective pages and validities 0F thru 0H List of amendments Revision 3 Update of page numbers Addition of equipment part numbers for airplanes up to S/N 1215 Correction of flow control shut-off valve part number...
Page 722 List of equipment Pilot's Operating Handbook List of amendments Revision 3 dated June 15, 2020 (Cont'd) Pages Description Correction of weight for GDUs Update of MOD number for GEA 71B, GIA 64W, GMA 36B, Surface Watch Addition of Stormscope data (34056F) Addition of ressourcing radome Deletion of GRA 55 transceiver part number Addition of TAS system data (MOD70-0258-00G)
Page 723 List of equipment Pilot's Operating Handbook Intentionally left blank Page 0H Edition 1 - January 15, 2018 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 724 List of equipment Pilot's Operating Handbook Table of contents Page ATA 01 - Specific optional equipment ........ATA 21 - Environmental system .
Page 725 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 726 List of equipment Pilot's Operating Handbook List of critical RVSM equipment Equipment listed hereafter, or later approved versions, is required for RVSM operation. >> Up to S/N 1215 Equipment Barometric altimeter : - GDC74B (Air data computer) P/N 011-01110-01 - GDU1200W (Display) P/N 011-02333-00 Autopilot Altitude Hold function : - GMC710 (AFCS mode controller)
Page 727: 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 1 - January 15, 2018 Rev.
Page 728: Environmental System
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 21 - Environmental system 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 729 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 730 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 731: 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 732: 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 DSC 740049 (Qty : 2) Neglig.
Page 733 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 734 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) 0563-23A Dual audio system with integrated Marker Beacon 2.80 148.90 Receiver # 2 GMA 36B (1.27) (3.782) 0564-31A G3000 COM # 1 system...
Page 735: 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 736: 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 25-11 - Furnishing - Flight compartment 25032 Front seats ease covers 2.756 183.78 (1.250)
Page 737 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) 0374-25B Servicing plugs unit, of which : 3.75 (1.700) - 12 VDC servicing plugs unit (Qty : 2 - one in the 3.31 195.28 cockpit, one in the cabin), of which :...
Page 738 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 739 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) 0568-25A Airbag capability 1.43 166.85 (0.647) (4.238) Seats Pilot's seat T700C2500002 55.12 183.90 (25.00) (4.671) 0553-25A Pilot's seat T700J2500005 48.90 185.86...
Page 740: 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 741: 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 (equipped assy T7002710018) (0.700) (5.400) 27-20 - Yaw control...
Page 742 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) 27-50 - Wing flaps (control) Flap control including : 15.520 218.50 (7.040) (5.550) - Flap motor 6157-1 2.866 216.54 (1.300)
Page 743: 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 744: 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 745 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) 30-60 - Propeller deicing Timer 3E2311-4 0.44 200.79 (0.200) (5.100) Page 22 Edition 1 - January 15, 2018 Rev.
Page 746: Indicating/Recording Systems
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 31 - Indicating/recording systems 31-20 - Independent instruments 31002A Hourmeter 56457-3 (engine running time) 0.551 156.30 (0.250) (3.970) Hourmeter 56457-3 (flying time)
Page 747 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 Avionics processing Unit # 2 GIA 64W 7.50 147.8 (3.40) (3.753) 0578-31A Data collection and transmission system 3.62 125.2 (FASTBOX)
Page 748: 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 749 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 Brake assembly 030-19100 14.991 204.33 (6.800) (5.190) 0606-32 Brake assembly 30-311 14.991 204.33 (6.800)
Page 750: 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 751 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 752: 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 753 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) 0544-34B Air Data Computer # 2 GDC 72B 1.83 148.11 (0.83) (3.762) 34-21 - Heading reference system 0476-00A Attitude and Heading Reference System # 1 GRS 77 3.46...
Page 754 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) 0476-00A Integrated Flight Deck System G3000 composed of : . PFD1 GDU 1200W 8.29 154.88 (3.76) (3.934) .
Page 755 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) 0549-00A Integrated Flight Deck System G3000 composed of : - PFD1 GDU 1250W 5.49 154.88 (2.49) (3.934) - PFD2 GDU 1250W 5.49...
Page 756 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) 34-31 - Marker MARKER antenna DM N27-3 0.750 129.92 (0.340) (3.300) 0541-23A MARKER antenna 6216-82-00 0.990 121.00 (0.450) (3.065)
Page 757 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 0451-34B GRA 55 radar altimeter, of which : 4.127 220.47 (1.872) (5.600) - Transceiver 3.527 228.82 (1.600)
Page 758 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) 0258-00G TAS system GTS 820, G3000 coupled, of which: 22.53 177.68 (10.220) (4.513) - Processor GTS 820 9.92 143.11 (4.500)
Page 759 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 34-53 - Transponder 0475-34A Transponder # 1 GTX 33D - Mode S with antenna 3.39 147.68 diversity and extended squitter (1.54) (3.751)
Page 760 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) 0542-34C 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 761 List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 34-54 - Automatic Direction Finder (ADF) 0507-34A ADF RA 3500 system (European countries only), of 7.61 216.48 which : (3.45)
Page 762: 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 0597-35A MC10 Smartmike oxygen mask (pilot and front 1.290 188.98 passenger) (0.585) (4.800) 0207-00 Gaseous oxygen system with oxygen masks 22.73...
Page 763: 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 764: Information Systems
List of equipment Pilot's Operating Handbook Item Weight OPT70 Required (R) or Standard (S) or Optional (A or O) per unit equipment MOD70 (kg) 46 - Information systems 0459-46C Flight stream transceiver FS210 0.264 151.18 (0.120) (3.840) 0459-46D Flight stream transceiver FS210 0.264 151.18 (0.120)
Page 765: 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 766: 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 1.764 158.27 ( 0.800) (4.020) Edition 1 - January 15, 2018 Page 43 Rev.
Page 767: 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 - 7.716 200.00 ( - 3.500) (5.080) Page 44 Edition 1 - January 15, 2018...
Page 768: 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 769: 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 770: Engine 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) 76 - Engine controls 0558-76 Single lever power control modification Neglig. auto-throttle capability - Version A: Single lever power control capability - Version B: Non auto-throttle knob Edition 1 - January 15, 2018 Page 47...
Page 771: 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 772: 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 773 List of equipment Pilot's Operating Handbook Intentionally left blank Page 50 Edition 1 - January 15, 2018 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 774 Supplement A Section 9 Pilot's Operating Handbook List of supplements and validities Airplane type * Sup. Edit. Description List of supplements From S/N 1000, plus S/N 687 WX-500 stormscope OPT70-34-056 From S/N 1000, plus S/N 687 Engine fire detection system OPT70-26-002G OPT70-26-002H MOD70-0496-26A...
Page 775 Supplement A Section 9 Pilot's Operating Handbook Airplane type * Sup. Sup. Edit. Edit. Description Description GARMIN GSR56 weather datalink and satellite phone MOD70-0331-23 From S/N 1000, plus S/N 687 Public transportation French-registered airplanes MOD70-0352-11 From S/N 1000, plus S/N 687 with MOD70-0176-00 Five-bladed propeller MOD70-0345-61...
Page 776 Supplement A Section 9 Pilot's Operating Handbook Airplane type * Sup. Sup. Edit. Edit. Description Description Lavatory compartment MOD70-0505-25 From S/N 1000, plus S/N 687 Stick Shaker MOD70-0510-27 Version C From S/N 1000 to S/N 1049, plus S/N 687 GARMIN G1000 NXi retrofit MOD70-0539-00 From S/N 1000 to S/N 1169 Data collection and transmission...
Page 777 Supplement A Section 9 Pilot's Operating Handbook Airplane type * Sup. Sup. Edit. Edit. Description Description Extended large storage cabinet MOD70-0684-25 From S/N 1270 GDR66 COM3 VHF communication MOD70-0722-23 From S/N 1272 900 E0 From S/N 1000 to S/N 1049, plus S/N 687 900 E1 From S/N 1050 910 E0...
Page 778 Supplement 6 WX-500 stormscope Pilot's Operating Handbook SUPPLEMENT WX-500 stormscope Table of contents Page General ..........9.6.2 Limitations .
Page 779 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 780 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 781 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 782 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 783: 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 784: 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 785 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. ▲...
Page 786: 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 787: 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 788: 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 789 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 790 Supplement 45 Mexico specifics Pilot's Operating Handbook SUPPLEMENT Mexico specifics Table of contents Page General ..........9.45.2 Limitations .
Page 791 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 792 Supplement 45 Mexico specifics Pilot's Operating Handbook For the small cargo net, on frame C13bis For the large cargo net, on R.H. Side upholstery panel, in the rear baggage compartment Non pressurized FWD baggage compartment On baggage compartment door frame MÁXIMO 50 kg - (110 lbs) PARA INSTRUCCIONES DE CARGA REFIERASE A LOS ”DATOS DE PESO Y BALANCE”...
Page 793 Supplement 45 Mexico specifics Pilot's Operating Handbook On R.H. side at front seat level and on the first rear passengers masks container (R.H. side on the ceiling) On rear passengers masks containers (on R.H. side on the ceiling and left side) On rear passenger's table casing LA MESA DEBE ESTAR GUARDADA DURANTE EL DESPEGUE Y ATERRIZAJE.
Page 794 Supplement 45 Mexico specifics Pilot's Operating Handbook Door internal side On access door On pilot door, if installed On emergency exit handle Edition 2 - April 29, 2016 Page 9.45.5 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 795 Supplement 45 Mexico specifics Pilot's Operating Handbook On landing gear emergency control access door At the upper corner of the window on each side of the cockpit 10 - On cabinet drawer (optional) >> Airplane equipped with coat hanger (Post-MOD70-0557-25) 11 - On the upper edge of the L.H.
Page 796 Supplement 45 Mexico specifics Pilot's Operating Handbook >> Airplane equipped with lavatory compartment (Post-MOD70-0505-25) 12 - On fixed panel, cabin side 13 - On fixed panel, toilet side Edition 2 - April 29, 2016 Page 9.45.7 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 797 Supplement 45 Mexico specifics Pilot's Operating Handbook 14 - On access door, cabin side and toilet side 15 - Behind access door, cabin side and toilet side Page 9.45.8 Edition 2 - April 29, 2016 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 798 Supplement 45 Mexico specifics Pilot's Operating Handbook 16 - Front face of lavatory compartment, near opening / closing switches 17 - On the magazine rack Edition 2 - April 29, 2016 Page 9.45.9 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 799 Supplement 45 Mexico specifics Pilot's Operating Handbook >> All External placards 18 - Under engine cowling and under each wing 19 - Near fuel tank caps Page 9.45.10 Edition 2 - April 29, 2016 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 800 Supplement 45 Mexico specifics Pilot's Operating Handbook 20 - Above brakes hydraulic fluid reservoir against firewall 21 - On langing gear hydraulic fluid reservoir 22 - On fuse box in engine cowling Edition 2 - April 29, 2016 Page 9.45.11 Rev.
Page 801 Supplement 45 Mexico specifics Pilot's Operating Handbook 23 - On internal face of L.H. engine cowling 24 - On front lower portion of firewall L.H. side Page 9.45.12 Edition 2 - April 29, 2016 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 802 Supplement 45 Mexico specifics Pilot's Operating Handbook 25 - On engine cowling, in front of compartment door 26 - On nose gear door 27 - On nose gear leg Edition 2 - April 29, 2016 Page 9.45.13 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 803 Supplement 45 Mexico specifics Pilot's Operating Handbook 28 - On main gear leg 29 - On internal face of the oxygen cylinder service door 30 - On the oxygen service door Page 9.45.14 Edition 2 - April 29, 2016 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 804 Supplement 45 Mexico specifics Pilot's Operating Handbook 31 - Near air data system port 32 - On external side of emergency locator transmitter inspection door 33 - On emergency exit external side Edition 2 - April 29, 2016 Page 9.45.15 Rev.
Page 805 Supplement 45 Mexico specifics Pilot's Operating Handbook 34 - Door external side On pilot door On access door On outer fuselage skin aft of access door and in the cabin forward of access door Page 9.45.16 Edition 2 - April 29, 2016 Rev.
Page 806 Supplement 45 Mexico specifics Pilot's Operating Handbook 35 - On last step of stairs CARGA MÁXIMA SOBRE LA ESCALERA : UNA PERSONA 36 - On R.H. access door jamb Edition 2 - April 29, 2016 Page 9.45.17 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 807 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 808 Supplement 45 Mexico specifics Pilot's Operating Handbook SECTION 7 Description No specifics SECTION 8 Handling, servicing and maintenance No specifics Edition 2 - April 29, 2016 Page 9.45.19 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 809 Supplement 45 Mexico specifics Pilot's Operating Handbook Intentionally left blank Page 9.45.20 Edition 2 - April 29, 2016 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 810 Supplement 49 GARMIN TAWS system Pilot's Operating Handbook SUPPLEMENT GARMIN TAWS system Table of contents Page General ..........9.49.2 Limitations .
Page 811 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 812 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 813 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 814 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 815 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 816 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 817 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 818 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 819 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 820 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 821 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 822 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 823 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 824 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 825: General
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 826: Emergency Procedures
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 827: Normal Procedures
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 828: Performance
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 829: Handling, Servicing And Maintenance
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 830 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 831: 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 832 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 833: 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 834 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 835 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 836: 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 837: 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 838: Handling, Servicing And Maintenance
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 839 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 840 Supplement 59 Brazil specifics Pilot's Operating Handbook SUPPLEMENT Brazil specifics Table of contents Page General ..........9.59.2 Limitations .
Page 841: Pilot's Operating Handbook
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 842 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 843 Supplement 59 Brazil specifics Pilot's Operating Handbook For the small cargo net, on frame C13bis For the large cargo net, on R.H. side upholstery panel, in the rear baggage compartment On FWD baggage compartment door frame, non pressurized 50 kg MÁXIMO PARA INSTRUÇÓES DE CARREGAMENTO CONSULTAR A SEÇÃO DE PESO E BALANCEAMENTO DO MANUAL DE VÔO...
Page 844 Supplement 59 Brazil specifics Pilot's Operating Handbook Near fuel tank caps On internal face of L.H. engine cowling Capacidade de óleo 12 l 12,7 qt On rear passenger's table casing A MESA DEVERÁ ESTAR RECOLHIDA PARA DECOLAGEM E POUSO Edition 1 - December 31, 2015 Page 9.59.5 Rev.
Page 845 Supplement 59 Brazil specifics Pilot's Operating Handbook On nose gear door On engine cowling, in front of compartment door - - TOMADA EXTERNA - - 28 VOLTS D.C. NOMINAL - - 800 AMPS CAPACIDADE MÍNIMA PARA PARTIDA - - NÃO EXCEDA 1000 AMPS On pilot door - External side, if installed Page 9.59.6 Edition 1 - December 31, 2015...
Page 846 Supplement 59 Brazil specifics Pilot's Operating Handbook On access door - External side On outer fuselage skin aft of access door and in the cabin forward of access door On access door - Internal side Edition 1 - December 31, 2015 Page 9.59.7 Rev.
Page 847 Supplement 59 Brazil specifics Pilot's Operating Handbook On pilot door - Internal side, if installed On emergency exit handle Marking on cover Marking on handle On last step of stairs MAX. UMA PESSOA NA ESCADA Page 9.59.8 Edition 1 - December 31, 2015 Rev.
Page 848 Supplement 59 Brazil specifics Pilot's Operating Handbook On R.H. access door jamb On R.H. side at front seat level and on the first rear passengers masks container (R.H. side on the ceiling) On rear passengers masks containers Edition 1 - December 31, 2015 Page 9.59.9 Rev.
Page 849 Supplement 59 Brazil specifics Pilot's Operating Handbook On the oxygen service door >> Airplanes equipped with Lavatory compartment (Post-MOD70-0505-25) On fixed panel, cabin side On fixed panel, toilet side Page 9.59.10 Edition 1 - December 31, 2015 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 850 Supplement 59 Brazil specifics Pilot's Operating Handbook On access door, cabin side and toilet side Behind access door, cabin side and toilet side Edition 1 - December 31, 2015 Page 9.59.11 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 851 Supplement 59 Brazil specifics Pilot's Operating Handbook Front face of lavatory compartment, near opening / closing switches On the magazine rack and on side wall of storage volume >> Airplanes equipped with Coat hanger (Post-MOD70-0557-25) On the upper edge of the L.H. Passenger access door panel Page 9.59.12 Edition 1 - December 31, 2015 Rev.
Page 852: Emergency Procedures
Supplement 59 Brazil specifics Pilot's Operating Handbook SECTION 3 Emergency procedures No specifics SECTION 4 Normal procedures No specifics SECTION 5 Performance No specifics SECTION 6 Weight and balance The weight and balance hereafter supplement or replace those of the standard airplane described in section 6 Weight and balance of the basic POH.
Page 853: Description
Supplement 59 Brazil specifics Pilot's Operating Handbook SECTION 7 Description No specifics SECTION 8 Handling, servicing and maintenance No specifics Page 9.59.14 Edition 1 - December 31, 2015 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 854: Supplement
Supplement 63 Lavatory compartment Pilot's Operating Handbook SUPPLEMENT Lavatory compartment Table of contents Page General ..........9.63.2 Limitations .
Page 855 Supplement 63 Lavatory compartment Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and operations necessary for operation when the TBM airplane is equipped with the option lavatory compartment. SECTION 2 Limitations The limitations hereafter supplement or replace those of the standard airplane described in section 2 Limitations of the basic POH when the TBM airplane is...
Page 856 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 857 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 858 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 859 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 860 Supplement 63 Lavatory compartment Pilot's Operating Handbook On the magazine rack SECTION 3 Emergency procedures The emergency procedures hereafter supplement those of the standard airplane described in section 3 Emergency procedures of the basic POH. 3.10 - Pressurization and air conditioning >>...
Page 861 Supplement 63 Lavatory compartment Pilot's Operating Handbook SECTION 4 Normal procedures The normal procedures hereafter supplement or replace those of the standard airplane described in section 4 Normal procedures of the basic POH when the TBM airplane is equipped with the option lavatory compartment. BRIEFING to passengers to be performed before entering the airplane Normal and Emergency stowing operations of the divider.
Page 862 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 863 Supplement 63 Lavatory compartment Pilot's Operating Handbook >> From S/N 1000 to S/N 1159 ( Arm (m) 4.392 ) − Moment = Weight x Arm CG (MAC %) = × 100 1.51 Weight Moment Item (kg) (m.kg) (MAC %) Empty Weight (kg) (1a) (1b) (1c)
Page 864 Supplement 63 Lavatory compartment Pilot's Operating Handbook >> From S/N 1160 ( Arm (m) 4.392 ) − Moment = Weight x Arm CG (MAC %) = × 100 1.51 Weight Moment Item (kg) (m.kg) (MAC %) Empty Weight (kg) (1a) (1b) (1c) Weight and moment variation after lavatory...
Page 865 Supplement 63 Lavatory compartment Pilot's Operating Handbook Using the weight and balance form CAUTION ▲ ▲ Empty weight, arm and CG % position to be considered are the ones from the last weight and balance report issued after the lavatory compartment option installation.
Page 866 Supplement 63 Lavatory compartment Pilot's Operating Handbook Weight and balance form and diagram (m, kg) - only applicable if lavatory compartment is installed >> From S/N 1000 to S/N 1159 ( Arm (m) 4.392 ) − Moment = Weight x Arm CG (MAC %) = ×...
Page 867 Supplement 63 Lavatory compartment Pilot's Operating Handbook >> From S/N 1160 ( Arm (m) 4.392 ) − Moment = Weight x Arm CG (MAC %) = × 100 1.51 Weight Moment Item (kg) (m.kg) (MAC %) Empty Weight (kg) Baggage FWD (<...
Page 868 Supplement 63 Lavatory compartment Pilot's Operating Handbook Figure 9.63.1 -- Weight and Balance diagram Edition 1 - November 16, 2016 Page 9.63.15 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 869 Supplement 63 Lavatory compartment Pilot's Operating Handbook Weight and balance form and diagram (in, lbs) - only applicable if lavatory compartment is installed >> From S/N 1000 to S/N 1159 ( Arm (in) 172.93 ) − Moment = Weight x Arm CG (MAC %) = ×...
Page 870 Supplement 63 Lavatory compartment Pilot's Operating Handbook >> From S/N 1160 ( Arm (in) 172.93 ) − Moment = Weight x Arm CG (MAC %) = × 100 59.45 Weight Moment Item (lbs) (in) (in.lbs) (MAC %) Empty Weight (lbs) Baggage FWD (<...
Page 871 Supplement 63 Lavatory compartment Pilot's Operating Handbook Figure 9.63.2 -- Weight and Balance diagram Page 9.63.18 Edition 1 - November 16, 2016 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 872 Supplement 63 Lavatory compartment Pilot's Operating Handbook SECTION 7 Description Information hereafter supplement or replace those of the standard airplane described in section 7 Description of the basic POH when the airplane is equipped with the option Lavatory compartment. For operation, refer to equipment User's Guide. The lavatory compartment is installed against right interior upholstery panel, facing large door.
Page 873 Supplement 63 Lavatory compartment Pilot's Operating Handbook Electric connection of the system is performed via a power plug : >> Without optional 12V power plugs (Pre-MOD70-0174-25) 28 volts >> With optional 12V power plugs (Post-MOD70-0174-25) 12 volts >> All The power plug is located on the right hand side upholstery panel. Connection is only accessible when the lavatory compartment structure is unscrewed from the floor and moved slightly aside to access the plug.
Page 874 Supplement 63 Lavatory compartment Pilot's Operating Handbook Figure 9.63.3 (1/2) -- Lavatory compartment Edition 1 - November 16, 2016 Page 9.63.21 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 875 Supplement 63 Lavatory compartment Pilot's Operating Handbook Figure 9.63.3 (2/2) -- Lavatory compartment Page 9.63.22 Edition 1 - November 16, 2016 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 876 Supplement 63 Lavatory compartment Pilot's Operating Handbook SECTION 8 Handling, servicing and maintenance Installation and operation of Lavatory compartment do not change the basic handling, servicing and maintenance procedures of the airplane described in section 8 Handling, servicing and maintenance of the basic POH. Edition 1 - November 16, 2016 Page 9.63.23 Rev.
Page 877 Supplement 63 Lavatory compartment Pilot's Operating Handbook Intentionally left blank Page 9.63.24 Edition 1 - November 16, 2016 Rev. 3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

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