Daher TBM 960 Pilot's Information Manual
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Daher TBM 960 Pilot's Information Manual

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Pilot's Information Manual
P/N DMMPIPYEE0EN - Edition 0 - Revision 2
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 intended for operation of the airplane.
The list of effective pages in this manual corresponds to that of the basic
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 the Copyright.
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 960
CAUTION
Pilot's Operating Handbook.
maintained.
© 2022 - DAHER AEROSPACE
All rights reserved
Printed in FRANCE

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Summary of Contents for Daher TBM 960

  • 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 JAN 2022 2.9.1 to 2.9.11 MAR 2022 3.A.1 to 3.A.3 APR 2022 3.0.1 to 3.0.3 APR 2022 3.1.1 to 3.1.4 JAN 2022 POH TBM 960 - Edition 0 Page 0.19 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 3 JAN 2022 5.3.1 to 5.3.2 JAN 2022 5.4.1 to 5.4.1 MAR 2022 5.5.1 to 5.5.1 JAN 2022 5.6.1 to 5.6.1 JAN 2022 POH TBM 960 - Edition 0 Page 0.20 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 4 JAN 2022 8.5.1 to 8.5.1 JAN 2022 8.6.1 to 8.6.5 MAR 2022 8.7.1 to 8.7.15 JAN 2022 8.8.1 to 8.8.2 JAN 2022 POH TBM 960 - Edition 0 Page 0.21 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 5 Section 0 Pilot's Operating Handbook Page No. Rev. No. Rev. Date 8.9.1 to 8.9.15 MAR 2022 8.10.1 to 8.10.2 JAN 2022 POH TBM 960 - Edition 0 Page 0.22 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 6 Pilot's Information Manual Table of Contents Section General Limitations Emergency Procedures Abnormal Procedures Normal Procedures Performance Weight and Balance Description Handling, Servicing and Maintenance PIM TBM 960 - Edition 0 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 7: Table Of Contents

    1.4.8 - Conversion Factors ..............1.5.1 - Pressure and Standard Atmosphere ......... 1.6.1 Standard Atmosphere ............1.6.1 Pressure Conversion Table ..........1.6.2 PIM TBM 960 - Edition 0 Page 1.0.1 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 8 Section 1 General Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 1.0.2 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 9: General

    The electrical load shedding procedure provided in Section 3 of this POH must be followed to meet requirements of paragraph 14 CFR 135.163(f)(2). PIM TBM 960 - Edition 0 Page 1.1.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 10 Section 1 General Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 1.1.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 11: Three View Drawing

    35.22 ft 2.914 m 9.56 ft 3.874 m 12.71 ft (*) Airplane on a level surface with fully extended FWD shock absorber PIM TBM 960 - Edition 0 Page 1.2.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 12 Section 1 General Pilot's Information Manual Figure 1.2.2 - Three View Drawing (2/2) 12.833 m 42.1 ft 4.988 m 16.36 ft PIM TBM 960 - Edition 0 Page 1.2.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 13: Descriptive Data

    The electro-hydro-mechanical Propeller Control Unit (PCU) modulates the blade angle. Fuel Total capacity: 301 USG (1,140 liters) Total capacity, each tank: 150.5 USG (570 liters) PIM TBM 960 - Edition 0 Page 1.3.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 14: Engine Oil

    Usable capacity: 6 qt (5.7 liters) Maximum oil consumption in a 10-hour period: 0.14 qt/h (0.13 l/h) [0.3 lb/h (136 cc/h)] Specification PIM TBM 960 - Edition 0 Page 1.3.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 15: Maximum Certificated Weights

    Maximum cabin height: 4 ft (1.22 m) Number of cabin entries: 1 (standard) + 1 pilot door (if installed) Entry width (standard): 3.54 ft (1.08 m) PIM TBM 960 - Edition 0 Page 1.3.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 16: Specific Loadings

    Pilot entry mean height: 3.18 ft (0.97 m) Specific Loadings Wing loading: 39.3 lbs/ft (191.9 kg/m Power loading: 8.5 lbs/SHP (3.86 kg/SHP) PIM TBM 960 - Edition 0 Page 1.3.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 17: Abbreviations And Terminology

    Maximum Landing Gear Operating Speed: the maximum speed at which the landing gear can be safely extended or retracted. PIM TBM 960 - Edition 0 Page 1.4.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 18: Power Terminology

    Airplane Performance and Flight Planning Terminology Climb gradient The ratio of the change in height during a portion of climb to the horizontal distance traversed during the same time interval. PIM TBM 960 - Edition 0 Page 1.4.2 Rev. 00...

  • Page 19: Weight And Balance Terminology

    The maximum weight approved at the beginning of the takeoff Takeoff Weight run. Maximum The maximum weight approved for landing touchdown. Landing Weight General Abbreviations Ampere Air Conditioning Air Data Computer PIM TBM 960 - Edition 0 Page 1.4.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 20 Electronic Stability Protection ESS BUS TIE Essential Bus Tie EXT LIGHTS External Lights °F Degrees Fahrenheit FADEC Full Authority Digital Engine Control PIM TBM 960 - Edition 0 Page 1.4.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 21 Instrument INT LIGHTS Interior Lights Interturbine Temperature Kilogram kg/h Kilogram per Hour kg/m Kilograms per Square Meter kg/SHP Kilogram per Shaft Horsepower PIM TBM 960 - Edition 0 Page 1.4.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 22 Mach Number Mean Aerodynamic Chord MAIN GEN Main Generator Manual MAX RPM Maximum Revolutions per Minute Millibar Multifunction Display Minute Minimum m.kg Kilogram-meters PIM TBM 960 - Edition 0 Page 1.4.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 23 Single Engine Indicator Selector Signalization Sea Level Serial Number SPKR Speaker STALL HTR Stall Warning Heater ST-BY Standby Standard STPD Standard Temperature Pressure Dry PIM TBM 960 - Edition 0 Page 1.4.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 24: Radio Navigation Abbreviations

    Dead Reckoning Emergency Locator Transmitter Final Approach Fix Flight Director Fault Detection and Exclusion Flight Management System GNSS Global Navigation Satellite System PIM TBM 960 - Edition 0 Page 1.4.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 25 VNAV Vertical NAVigation VHF Omnidirectional Range VOR/LOC VHF Omnidirectional Range LOCalizer WFDE WAAS Fault Detection and Exclusion World Geodetic System XPDR Transponder PIM TBM 960 - Edition 0 Page 1.4.9 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 26 Section 1 General Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 1.4.10 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 27: Conversion Factors

    0.3048 meters meters 3.2808 feet inches 25.4 0.03937 inches Imp.Gal 4.546 liters liters 0.220 Imp.Gal 3.785 liters liters 0.264 0.45359 2.2046 PIM TBM 960 - Edition 0 Page 1.5.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 28 Section 1 General Pilot's Information Manual Figure 1.5.1 - Feet to Meters feet 31,000 30,000 20,000 10,000 meters 2,500 5,000 7,500 10,000 PIM TBM 960 - Edition 0 Page 1.5.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 29 Section 1 General Pilot's Information Manual Figure 1.5.2 - Inches to Millimeters 1,000 PIM TBM 960 - Edition 0 Page 1.5.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 30 Section 1 General Pilot's Information Manual Figure 1.5.3 - Pounds to Kilograms 8,000 6,000 4,000 2,000 1,000 2,000 3,000 4,000 PIM TBM 960 - Edition 0 Page 1.5.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 31: Pressure And Standard Atmosphere

    - 36.5 - 33.6 28,000 329.3 - 40.4 - 40.7 30,000 300.8 - 44.4 - 47.8 31,000 287.4 - 46.4 - 51.6 PIM TBM 960 - Edition 0 Page 1.6.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 32: Pressure Conversion Table

    30.65 30.68 1,040 1,041 1,042 1,043 1,044 1,045 1,046 1,047 1,048 1,049 30.71 30.74 30.77 30.80 30.83 30.86 30.89 30.92 30.95 30.98 PIM TBM 960 - Edition 0 Page 1.6.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 33 Reverse Utilization ..............2.6.10 Weather Radar ..............2.6.10 Equipment Required Depending on Type of Operation ..2.6.10 Altitude Operating Limits ............2.6.14 PIM TBM 960 - Edition 0 Page 2.0.1 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 34 Airspeed Indicator on PFD(s) and on Standby Airspeed Indicator ................2.8.1 Pressurization ............... 2.8.1 Engine Instruments ............... 2.8.2 - Placards ..................2.9.1 PIM TBM 960 - Edition 0 Page 2.0.2 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 35: General

    Pilot's Information Manual - General TBM 960 is the trade name of the TBM 700 N variant 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 36 Section 2 Limitations Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 2.1.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 37: Airspeed Limitations

    Retraction Emergency extension Maximum landing gear Do not exceed this speed extended speed with landing gear extended PIM TBM 960 - Edition 0 Page 2.2.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 38 Section 2 Limitations Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 2.2.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 39: Powerplant Limitations

    900 °C < ITT ≤ 1,000 °C acceptable for maximum 5 seconds. CAUTION Do not mix different viscosities or specifications of oil as their different chemical structure can make them incompatible. PIM TBM 960 - Edition 0 Page 2.3.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 40: Fuel

    DIEGME) shall be between a minimum of 0.06% and a maximum of 0.15% by volume. Refer to Paragraph Fuel in Subsection 8.7. for additional information. PIM TBM 960 - Edition 0 Page 2.3.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 41: Propeller

    Maximum reverse: - 9.3° Full Authority Digital Engine Control (FADEC) NO DISPATCH Takeoff is not allowed when is displayed in the CAS window. PIM TBM 960 - Edition 0 Page 2.3.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 42 The full duration of the flight after which first appeared must be counted when calculating the 50-flight-hour time period. Calculating the 50-flight-hour time period is the pilot's responsibility. PIM TBM 960 - Edition 0 Page 2.3.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 43: Starter Operation Limits

    Between 1st and 2nd sequence: wait for 1 minute. Between 2nd and 3rd sequence: wait for 5 minutes. Between 3rd and 4th sequence: wait for 30 minutes. PIM TBM 960 - Edition 0 Page 2.4.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 44 Section 2 Limitations Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 2.4.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 45: Weight And C.g. Limits

    >> With 4-seat accommodation in rear part of pressurized cabin: 396 lbs (180 kg), with small or large net – Figure 2.5.1 PIM TBM 960 - Edition 0 Page 2.5.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 46: C.g. Limits

    193.7 in (4.921 m) aft of datum at 7,394 lbs (3,354 kg) (35% of MAC) 194.0 in (4.928 m) aft of datum at 6,986 lbs (3,169 kg) (35.5% of MAC) PIM TBM 960 - Edition 0 Page 2.5.2 Rev. 00...
  • Page 47 Figure 2.5.2 - C.G. Limits (MAC %) Max Ramp Weight (MRW) Max Takeoff Weight (MTOW) (MAC %) 22 24 32 34 PIM TBM 960 - Edition 0 Page 2.5.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 48 Max Zero Fuel Weight (MZFW) Zero Fuel Weight Empty Weight (MAC %) 14 16 18 20 22 24 26 28 30 32 34 36 PIM TBM 960 - Edition 0 Page 2.5.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 49: Operation Limits

    Weight above 6,579 lbs (2,984 kg): -1.5 < n < +3.5 g Flaps Down -0 < n < +2.0 g CAUTION Intentional negative load factors are prohibited. PIM TBM 960 - Edition 0 Page 2.6.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 50: Generator Limits

    The autothrottle must be disengaged before 200 ft (60 m) AGL. HomeSafe Emergency Function HomeSafe must be activated only when the pilot is incapacitated. PIM TBM 960 - Edition 0 Page 2.6.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 51: Gnss (Gps/Sbas) Navigation Equipment Approvals

    Depending on the area of navigation, an operational approval may be required to use the navigation performance that are detailed in the table hereafter. The pilot is responsible to ensure compliance with current operational requirements. PIM TBM 960 - Edition 0 Page 2.6.3 Rev. 00...
  • Page 52 RF Legs) and utilized when procedures. This includes conducting procedures procedures with Radius-to- containing RF Legs. Fix Legs (RF Legs). Continue ► PIM TBM 960 - Edition 0 Page 2.6.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 53 (with conducting procedures or the final leg of the missed and without containing RF Legs. approach procedure only. RF Legs) PIM TBM 960 - Edition 0 Page 2.6.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 54: Gnss (Gps/Sbas) Navigation System Limitations

    Navigation database or verifies each waypoint for accuracy by reference to current approved data. PIM TBM 960 - Edition 0 Page 2.6.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 55 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 PIM TBM 960 - Edition 0 Page 2.6.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 56: Icing Conditions

    The wing and tail leading edge pneumatic deicing boot system may be deactivated only after leaving icing conditions and after the airplane is determined to be clear of ice. PIM TBM 960 - Edition 0 Page 2.6.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 57: Severe Icing Conditions

    This supersedes any relief provided by the Master Minimum Equipment List (MMEL). Refer to Paragraph Equipment Required Depending on Type of Operation PIM TBM 960 - Edition 0 Page 2.6.9 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 58: Flap Operating Envelope

    It is the pilot's responsibility to check that the following equipment lists are in accordance with the specific national operation rules of the airplane registration country depending on the type of operation. PIM TBM 960 - Edition 0 Page 2.6.10 Rev. 00...
  • Page 59 Ground power unit connected Inertial separator Starter Ignition Flaps Landing gears and doors Aural warning warning Landing gear warning Stall warning Engine instruments Torquemeter PIM TBM 960 - Edition 0 Page 2.6.11 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 60 Battery Miscellaneous Seats (each occupant) Belts (each occupant) Straps (each occupant) Pilot's Operating Handbook Night VFR All equipment required for day VFR PIM TBM 960 - Edition 0 Page 2.6.12 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 61 Airframe, stabilizer and elevator horn deicing Wing leading edge inspection light, if night flight Stall warning deicing Inertial separator Garmin annunciation “Airspeed” PIM TBM 960 - Edition 0 Page 2.6.13 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 62: Altitude Operating Limits

    RVSM approval. The standby altimeter is not approved for RVSM operations. PIM TBM 960 - Edition 0 Page 2.6.14 Rev. 00...

  • Page 63: In-Flight Breaker Use Limits

    Selected altitude Barometric pressure setting Chartview System Operating Limitations The geographic-referenced airplane symbol on some charts must not be used for navigation. PIM TBM 960 - Edition 0 Page 2.6.15 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 64 Database currency must be verified prior to use via database effectivity page. The flight crew is responsible for verifying availability of charts for the planned flight. PIM TBM 960 - Edition 0 Page 2.6.16 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 65: Miscellaneous Limits

    Flight with an open or ajar door is prohibited. Cargo Net Installation Limits Small cargo net: maximum loading height = 28 in (710 mm) PIM TBM 960 - Edition 0 Page 2.7.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 66 Large cargo net: maximum loading height = 22 in (565 mm) in cabin, out of baggage compartment. CAUTION No item may extend forward of the cargo net system to protect door from obstruction. PIM TBM 960 - Edition 0 Page 2.7.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 67: Markings

    266 KIAS = V Above 266 pole strip Pressurization Table 2.8.2 - Pressurization Marking Marking Value Significance Red line 6.2 psi Cabin differential pressure limit PIM TBM 960 - Edition 0 Page 2.8.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 68: Engine Instruments

    Propeller RPM (Np) is not presented in the above table as the information is only presented as a digital indicator – refer to Paragraph Digit Colors PIM TBM 960 - Edition 0 Page 2.8.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 69 > 5 seconds Yellow and Ng > 72% 135 < psi ≤ 175 ≤ 20 seconds < 40 psi None Continue ► PIM TBM 960 - Edition 0 Page 2.8.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 70 1,905 ≤ Np ≤ 1,955 None Green 2,030 < Np < 2,100 None Yellow > 2,030 ≥ 20 seconds ≥ 2,100 None PIM TBM 960 - Edition 0 Page 2.8.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 71 103% < TRQ ≤ 118% < 5 seconds 103% < TRQ ≤ 118% ≥ 5 seconds Yellow > 103% ≥ 20 seconds > 118% None PIM TBM 960 - Edition 0 Page 2.8.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 72 Section 2 Limitations Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 2.8.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 73: Placards

    FOR LOADING INSTRUCTIONS REFER TO WEIGHT AND BALANCE SECTION OF PILOT'S OPERATING HANDBOOK For the large cargo net, on right side upholstery panel, in the rear baggage compartment PIM TBM 960 - Edition 0 Page 2.9.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 74 IN PILOT'S OPERATING HANDBOOK On the pedestal console GND FEATHER NOSE DOWN NOSE IDLE IDLE AILERON TRIM FLAPS On the fuel selector PIM TBM 960 - Edition 0 Page 2.9.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 75 FUELS QUANTITY AND TYPE OF ADDITIVE U. S. GALLONS On internal face of left-side engine cowling 10. On the landing gear emergency control access door PIM TBM 960 - Edition 0 Page 2.9.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 76 12. Above the passenger's table TABLE MUST BE STOWED DURING TAKE-OFF AND LANDING 13. Under the right control wheel 14. On the nose gear door PIM TBM 960 - Edition 0 Page 2.9.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 77 28 VOLTS D.C. NOMINAL 800 AMPS STARTING CAPACITY MIN DO NOT EXCEED 1000 AMPS 18. On the pilot door - External side, if installed PIM TBM 960 - Edition 0 Page 2.9.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 78 Pilot's Information Manual 19. On the access door - External side 20. On the outer fuselage skin aft of the access door PIM TBM 960 - Edition 0 Page 2.9.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 79 23. On the pilot door - Internal side, if installed 24. On the emergency exit handle Marking on cover and marking on handle. PIM TBM 960 - Edition 0 Page 2.9.7 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 80 Section 2 Limitations Pilot's Information Manual 25. Above the emergency exit door 26. On the last step of stairs PIM TBM 960 - Edition 0 Page 2.9.8 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 81 1250 1350 1450 1550 1650 1750 1850 1950 2050 2150 1150 2250 CHARGE PRESSURE (PSI G) 29. On the oxygen service door PIM TBM 960 - Edition 0 Page 2.9.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 82 31. On each coat and headset hanger 32. Above the AFCS control unit USE OF HOMESAFE FUNCTION RESTRICTED TO SITUATIONS PILOT INCAPACITATION PIM TBM 960 - Edition 0 Page 2.9.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 83 Section 2 Limitations Pilot's Information Manual 33. On both sides of each buckle positioner SEAT BUCKLE POSITIONER ONLY PIM TBM 960 - Edition 0 Page 2.9.11 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 84 Section 2 Limitations Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 2.9.12 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 85 ENG PROT ACTIVE ..............3A.3.3 ESP DEGRADED AOA ............3A.12.3 ESP DEGRADED IAS .............. 3A.12.2 ESP FAIL .................. 3A.12.1 EXCEEDANCE ............... 3A.12.22 PIM TBM 960 - Edition 0 Page 3.A.1 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 86 LOW LVL FAIL L-R ..............3A.8.4 LOW VOLTAGE ................3A.9.4 MAIN GEN .................. 3A.9.3 MAIN GEN and LOW VOLTAGE ..........3A.9.5 NG ....................3.3.15 PIM TBM 960 - Edition 0 Page 3.A.2 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 87 USP ACTIVE ................3.12.4 VACUUM LOW ................. 3A.10.4 XPDR1 ADS-B FAIL and XPDR2 ADS-B FAIL ..... 3A.12.18 XPDR1 FAIL and XPDR2 FAIL ..........3A.12.17 PIM TBM 960 - Edition 0 Page 3.A.3 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 88 Section 3 Emergency Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3.A.4 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 89 Cabin Electrical Fire or Smoke During Flight ......3.5.4 Smoke Elimination ..............3.5.6 - Emergency Descents ..............3.6.1 Emergency Descents Profiles ..........3.6.1 PIM TBM 960 - Edition 0 Page 3.0.1 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 90 HS CONFIG MODE ............. 3.12.11 3.13 - Miscellaneous ................3.13.1 Crack in Cockpit Window or Window Panel ......3.13.1 Emergency Exit Use ............. 3.13.2 PIM TBM 960 - Edition 0 Page 3.0.2 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 91 3.13.4 AP Off, Stall Warning ............3.13.5 Oxygen Use ................3.13.6 Flight into Severe Icing Conditions ........3.13.9 NO DISPATCH ..............3.13.10 PIM TBM 960 - Edition 0 Page 3.0.3 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 92 Section 3 Emergency Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3.0.4 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 93: General

    Red or amber failure warnings are coupled with the lighting of: a flashing red indicator/pushbutton PIM TBM 960 - Edition 0 Page 3.1.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 94: Procedure Format

    Through self-training, simulator, initial and recurrent training, the pilot must perfectly know these items in order to take appropriate actions without using any Check-List as soon as the emergency situation occurs and is identified PIM TBM 960 - Edition 0 Page 3.1.2 Rev. 00...
  • Page 95 ► Land as soon as practicable ◄ means land for maintenance on the nearest suitable runway with convenient facilities. CAS MESSAGES Indicated as displayed in the CAS window: PIM TBM 960 - Edition 0 Page 3.1.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 96 ANNUNCIATIONS ON PFDs or MFD Indicated as displayed in the PFD or MFD with specifying “annunciation” next to the message: BOTH ON AHRS1 annunciation, HDG annunciation. PIM TBM 960 - Edition 0 Page 3.1.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 97: Rejected Takeoff

    If necessary: - Evacuate the airplane after coming to complete stop. Do not unfasten seat belts before complete stop End of procedure. PIM TBM 960 - Edition 0 Page 3.2.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 98: Rejected Takeoff For Any Other Reason

    If necessary: - Evacuate the airplane after coming to complete stop. Do not unfasten seat belts before complete stop End of procedure. PIM TBM 960 - Edition 0 Page 3.2.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 99: Engine Failures

    Engine Failure Before Rotation 1 / 1 - Perform procedure . Engine Failure at Takeoff Before Rotation in Subsection 3.2. End of procedure. PIM TBM 960 - Edition 0 Page 3.3.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 100: Engine Failure After Rotation

    - Evacuate the airplane after coming to complete stop. Do not unfasten seat belts before complete stop End of procedure ■ Continue ► PIM TBM 960 - Edition 0 Page 3.3.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 101 14 - Crash lever ................Pull down 15 - Evacuate the airplane after coming to complete stop. Do not unfasten seat belts before complete stop End of procedure. PIM TBM 960 - Edition 0 Page 3.3.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 102: Engine Failure In Flight

    DE ICE LIGHT COND PWR2 LIGHT DOORS CH.B DETEC FADEC CH.B DATA SATCOM PANEL CABIN CONT SATCOM LINK HEATER LIGHT Continue ► PIM TBM 960 - Edition 0 Page 3.3.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 103 NO DISPATCH is ON, will be displayed when on ground – refer to procedure NO DISPATCH in Subsection 3.13. End of procedure. PIM TBM 960 - Edition 0 Page 3.3.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 104: Oil Press Or Oil Press

    ENG OP DEGRADED may appear – refer to procedure ENG OP DEGRADED in Subsection 3A.3. Prepare for an engine stop shortly. Continue ► PIM TBM 960 - Edition 0 Page 3.3.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 105 - ENGINE MODE switch ..............OFF - FUEL TANK SELECTOR ............... OFF - Perform procedure ..Maximum Range Descent in Subsection 3.6. End of procedure. PIM TBM 960 - Edition 0 Page 3.3.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 106: Engine Regulation Discrepancy

    If engine power allows for level flight at 120 KIAS or above: CAUTION Avoid rapid THROTTLE movements. No faster than 10 seconds between IDLE and maximum power positions. Continue ► PIM TBM 960 - Edition 0 Page 3.3.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 107 NO DISPATCH will be displayed when on ground, refer to procedure DISPATCH in Subsection 3.13. End of procedure ■ Continue ► PIM TBM 960 - Edition 0 Page 3.3.9 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 108 By setting nose-up attitude 18 - INERT SEP switch ................ON If ITT > 850 °C: 19 - INERT SEP switch ............... OFF Continue ► PIM TBM 960 - Edition 0 Page 3.3.10 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 109 NO DISPATCH are displayed in flight, will be displayed when on ground, refer to procedure NO DISPATCH in Subsection 3.13. End of procedure. PIM TBM 960 - Edition 0 Page 3.3.11 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 110: Prop

    In that case, the go-around may damage the gear reduction box and the reverse efficiency might be lower than expected. Inform maintenance department. Repair before further flight. End of procedure. PIM TBM 960 - Edition 0 Page 3.3.12 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 111: Itt

    End of procedure ■ After engine start: On ground: - Cancel the flight. Inform maintenance department. End of procedure ■ Continue ► PIM TBM 960 - Edition 0 Page 3.3.13 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 112 - THROTTLE ..............Reduce To get ITT in green sector ► Land as soon as possible ◄ Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3.3.14 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 113 - THROTTLE ..................Reduce To get Ng below 104% ► Land as soon as possible ◄ Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3.3.15 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 114: Oil Temp Or Oil Temp

    - Oxygen masks ............... Use Refer to procedure Oxygen Use in Subsection 3.13. - THROTTLE ..................IDLE - ENGINE MODE switch ..............OFF Continue ► PIM TBM 960 - Edition 0 Page 3.3.16 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 115 2 / 2 ► Continuing - FUEL TANK SELECTOR ............... OFF - Perform procedure ..Maximum Range Descent in Subsection 3.6. End of procedure. PIM TBM 960 - Edition 0 Page 3.3.17 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 116: Feather

    Forced Landing or Ditching in Subsection 3.7. NOTE NO DISPATCH will be displayed when on ground, refer to procedure DISPATCH in Subsection 3.13. End of procedure. PIM TBM 960 - Edition 0 Page 3.3.18 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 117: Air Start

    Air start may be attempted outside of the envelope. However, above 20,000 ft or at lower speeds, ITT tends to increase during start and prudence is recommended. End of procedure. PIM TBM 960 - Edition 0 Page 3.4.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 118: Air Start Procedure

    13 - STARTER switch ..................ON 2 seconds, then release STARTER 14 - ..................Check ON IGNITION 15 - ..................Check ON Continue ► PIM TBM 960 - Edition 0 Page 3.4.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 119 23 - BLEED switch ..............As required 24 - Electrical equipment ............As required ► Land as soon as possible ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3.4.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 120 Section 3 Emergency Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3.4.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 121: Fire And Smoke

    If necessary: - Warn ground assistance. - Crash lever ..................Pull down ► Evacuate as soon as possible ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3.5.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 122: Cabin Fire On Ground

    - Crash lever ..................Pull down - Cabin fire extinguisher ..............As required ► Evacuate as soon as possible ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3.5.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 123: Engine Fire In Flight

    Maximum Rate Descent in Subsection 3.6. - Perform a forced landing. Refer to procedure Forced Landing or Ditching in Subsection 3.7. End of procedure. PIM TBM 960 - Edition 0 Page 3.5.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 124: Cabin Electrical Fire Or Smoke During Flight

    Check for possible fire or smoke while re-engaging necessary electrical equipment one after the other. 13 - SOURCE selector ................. BATT 14 - GENERATOR selector ..............MAIN Continue ► PIM TBM 960 - Edition 0 Page 3.5.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 125 19 - Perform an emergency descent. Refer to procedure Maximum Rate Descent in Subsection 3.6. ► Land as soon as possible ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3.5.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 126: Smoke Elimination

    End of procedure ■ If smoke increases: - EMERGENCY RAM AIR control knob ........... Push ► Land as soon as possible ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3.5.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 127: Emergency Descents

    15,000 10,000 Max Range Descent 5,000 IAS = 120 KIAS Ground distances (Nautical Miles) No wind - Smooth atmosphere End of procedure. PIM TBM 960 - Edition 0 Page 3.6.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 128 If rough air or in case of structure problem: - Airspeed ..............Below 178 KIAS - FLAPS lever ..................UP - LANDING GEAR lever ..............DN End of procedure. PIM TBM 960 - Edition 0 Page 3.6.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 129: Maximum Range Descent

    11 - Prepare for a forced landing. Refer to procedure Forced Landing or Ditching in Subsection 3.7. End of procedure ■ Continue ► PIM TBM 960 - Edition 0 Page 3.6.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 130 27 - All personal electrical devices ..........Disconnect 28 - Prepare for a forced landing. Refer to procedure Forced Landing or Ditching in Subsection 3.7. End of procedure. PIM TBM 960 - Edition 0 Page 3.6.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 131 13 - LANDING GEAR lever ........... Keep UP When chosen landing surface is assured: 14 - FLAPS lever ................... LDG 15 - Crash lever ................Pull down Continue ► PIM TBM 960 - Edition 0 Page 3.7.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 132 24 - Maintain attitude without flaring out until touchdown. 25 - Evacuate through EMERGENCY EXIT. Refer to procedure Emergency Exit Use in Subsection 3.13. End of procedure. PIM TBM 960 - Edition 0 Page 3.7.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 133: Tire Blowout During Landing

    - Stop the airplane to minimize damages. - Shut down the engine. Refer to procedure Shutdown in Subsection 4.4. End of procedure. PIM TBM 960 - Edition 0 Page 3.7.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 134: Flaps Asym

    IAS < 122 KIAS for deflections greater than TO position. At landing: - Perform procedure ..Landing with Flaps Malfunction in Subsection 3A.7. End of procedure. PIM TBM 960 - Edition 0 Page 3.7.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 135: Fuel System

    End of procedure ■ FUEL PRESS remains ON: - Fullest tank ..............Select - Avoid high power and rapid movements of the THROTTLE. Continue ► PIM TBM 960 - Edition 0 Page 3.8.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 136 2 / 2 ► Continuing 10 - Altitude ............Below 18,000 ft ► Land as soon as possible ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3.8.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 137: Fuel Low L-R

    ► Fly the airplane ◄ - Minimum fuel ................Check - Take decision. If necessary: ► Land as soon as practicable ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3.8.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 138: Fuel Clogging

    On ground: ► Do not take off ◄ Inform maintenance department. The airplane is grounded, repair before further flight. End of procedure. PIM TBM 960 - Edition 0 Page 3.8.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 139: Electrical System

    L WS DE ICE PITOT R & STALL TAXI LIGHT LH LDG LIGHT RADIO ALTI RH LDG LIGHT PULSE SYST FUEL SEL Continue ► PIM TBM 960 - Edition 0 Page 3.9.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 140 115 VAC PLUG HEATERS CMD NOTE Breakers located on Frame C13bis and Frame C15. Figure 3.9.3 - BUS 5 Bar NOT USED Continue ► PIM TBM 960 - Edition 0 Page 3.9.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 141 AHRS 1 BUS 2 LDG SIG CPCS PWR1 CAB BLEED IGNITION EMER LIGHT GND CLR ACCESS (driving geared motor) End of procedure. PIM TBM 960 - Edition 0 Page 3.9.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 142: Total Loss Of Electrical Power

    ON. If airplane power is lost, the internal battery will provide power to the MD302 for one hour. End of procedure. PIM TBM 960 - Edition 0 Page 3.9.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 143: 3.10 - Pressurization And Air Conditioning

    - CPCS PWR2 (BUS 2) breaker ........Check pushed If possible: - TRQ ................. Reduce ► Fly the airplane ◄ - BLEED switch ................AUTO Continue ► PIM TBM 960 - Edition 0 Page 3.10.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 144: Pressu Off

    10 - Taxi back to apron. 11 - Shut down the engine. Refer to procedure Shutdown in Subsection 4.4. Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3.10.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 145: Cabin Altitude And Use Oxygen Mask

    Subsection 3.6. - Limit flight altitude to maintain cabin altitude below 10,000 ft. Inform maintenance department before next flight. End of procedure. PIM TBM 960 - Edition 0 Page 3.10.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 146: Edm

    Subsection 3.6. - Limit flight altitude to maintain cabin altitude below 10,000 ft. Inform maintenance department before next flight. End of procedure. PIM TBM 960 - Edition 0 Page 3.10.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 147: Cabin Diff Press

    ► Fly the airplane ◄ If necessary: - Perform an emergency descent. Refer to procedure Maximum Rate Descent in Subsection 3.6. End of procedure. PIM TBM 960 - Edition 0 Page 3.10.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 148: 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. PIM TBM 960 - Edition 0 Page 3.10.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 149: Door

    - DUMP switch ............... Press - THROTTLE ................IDLE - Airspeed ................ 120 KIAS ► Land as soon as possible ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3.10.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 150 Section 3 Emergency Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3.10.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 151: Deicing System

    Section 3 Emergency Procedures Pilot's Information Manual 3.11 - Deicing System No Emergency Procedures Refer to Section 3A for Abnormal Procedures. PIM TBM 960 - Edition 0 Page 3.11.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 152 Section 3 Emergency Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3.11.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 153: 3.12 - Avionics Miscellaneous

    If unsuccessfull to disconnect AT: - AP SERVOS breaker ........... Pull AP is also inoperative Fly the airplane without AP End of procedure. PIM TBM 960 - Edition 0 Page 3.12.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 154: Trim Runaway

    The pitch trim may be used manually, the two other trim tabs may be used again electrically. End of procedure ■ Continue ► PIM TBM 960 - Edition 0 Page 3.12.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 155 According to the defective trim - AP/TRIMS switch ................ON The two other trim tabs may be used again electrically. End of procedure. PIM TBM 960 - Edition 0 Page 3.12.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 156: Usp Active

    - Do not disconnect AP. - Manage the flight. NOTE Stall warning may be triggered but AP will remain ON. End of procedure. PIM TBM 960 - Edition 0 Page 3.12.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 157: Aural Wrn Fail

    105 < KIAS < 266 Flaps TO 100 < KIAS < 178 Flaps LDG 85 < KIAS < 122 End of procedure. PIM TBM 960 - Edition 0 Page 3.12.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 158: Aural Wrn 1 Chl

    Pilot's Information Manual AURAL WRN 1 CHL 1 / 1 NOTE System switches automatically on the remaining valid aural channel. End of procedure. PIM TBM 960 - Edition 0 Page 3.12.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 159: Abort Apr

    Pilot's Information Manual ABORT APR 1 / 1 Indicates a loss of GPS navigation. ► Perform a go-around ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3.12.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 160: Homesafe Rqst

    AP / YD / AT also disengage NOTE Before reengaging AP / YD and/or AT, check that FD and AT modes are correct. End of procedure. PIM TBM 960 - Edition 0 Page 3.12.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 161: Homesafe Deactivation

    - Inform ATC that the pilot is back and flying the airplane, and ask for altimeter setting. Inform that the pilot must reenter the flight plan in the - Altimeter setting ................Re-adjust If necessary Continue ► PIM TBM 960 - Edition 0 Page 3.12.9 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 162 2 / 2 ► Continuing ACFT CONF MISM is ON: - Perform procedure ....ACFT CONF MISM in Subsection 3A.7. End of procedure. PIM TBM 960 - Edition 0 Page 3.12.10 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 163 Indicates that HomeSafe is still in configuration mode after a maintenance operation. HS CONFIG MODE appears only at avionics initialization. - Do not start the engine. Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3.12.11 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 164 Section 3 Emergency Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3.12.12 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 165 ► Fly the airplane ◄ - Descend slowly. - Cabin differential pressure ............. Reduce By setting Landing Field Elevation to 10,000 ft End of procedure. PIM TBM 960 - Edition 0 Page 3.13.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 166 - Put the emergency exit door inside fuselage or throw it away from the fuselage through the opening. - Evacuate airplane. End of procedure. PIM TBM 960 - Edition 0 Page 3.13.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 167: Emergency Beacon (Elt) Use

    - Transmit a MAY DAY signal on COM VHF 121.5 MHz or on a known ATC frequency. After landing: - ELT remote control switch ................. ON Maintain ON until aid arrives End of procedure. PIM TBM 960 - Edition 0 Page 3.13.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 168 When rotation is stopped: - Level the wings and ease out of the dive. ► Fly the airplane ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3.13.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 169: Ap Off, Stall Warning

    - Fly the airplane, wings levelled and nose down until stall warning stops. - TRQ ....................As required - Return to the desired flight path. End of procedure. PIM TBM 960 - Edition 0 Page 3.13.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 170: Oxygen Use

    Before using oxygen, remove any trace of oil, grease, soap and other fatty substances (including lipstick, make-up, etc.) on the user's face. Continue ► PIM TBM 960 - Edition 0 Page 3.13.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 171 12 - Perform an emergency descent ..To an altitude below 10,000 ft Refer to procedure Maximum Rate Descent in Subsection 3.6. Continue ► PIM TBM 960 - Edition 0 Page 3.13.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 172 15 - Pull on the lanyard cord to pull out the lanyard pin and flow the oxygen. 16 - Put the mask on the face. 17 - Check that the green bag inflates. End of procedure. PIM TBM 960 - Edition 0 Page 3.13.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 173: Flight Into Severe Icing Conditions

    - Perform procedure ..Flight into Severe Icing Conditions in Subsection 4.5. End of procedure. PIM TBM 960 - Edition 0 Page 3.13.9 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 174 ► Do not take off ◄ Inform maintenance department. The airplane is grounded, repair before further flight. End of procedure. PIM TBM 960 - Edition 0 Page 3.13.10 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 175 3A.7.6 Landing with Unlocked Main Landing Gear ......3A.7.9 Landing with Defective Nose Landing Gear (Down Unlocked or Not Down) ................ 3A.7.11 PIM TBM 960 - Edition 0 Page 3A.0.1 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 176 ..............3A.11.9 ICE DETECTION FAIL ............3A.11.10 3A.12 - Avionics Miscellaneous ............. 3A.12.1 ESP FAIL ................3A.12.1 ESP DEGRADED IAS ............3A.12.2 PIM TBM 960 - Edition 0 Page 3A.0.2 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 177 ..............3A.12.22 3A.13 - Miscellaneous ................3A.13.1 CARGO DOOR ..............3A.13.1 GPU DOOR ................. 3A.13.2 IGNITION ................3A.13.3 LMTD DISPATCH ..............3A.13.4 PIM TBM 960 - Edition 0 Page 3A.0.3 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 178 Section 3A Abnormal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3A.0.4 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 179 General. Refer to Subsection 3.1. General for further information about: Alarm system recall, Procedure format, which are also applicable to Abnormal Procedures. PIM TBM 960 - Edition 0 Page 3A.1.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 180 Section 3A Abnormal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3A.1.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 181 Section 3A Abnormal Procedures Pilot's Information Manual 3A.2 - Rejected Takeoff No Abnormal Procedures Refer to Section 3 for Emergency Procedures. PIM TBM 960 - Edition 0 Page 3A.2.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 182 Section 3A Abnormal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3A.2.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 183 Single engine indicator may switch to ITT or NG parameter depending on engine conditions. - AT ....................Disconnect - THROTTLE ..................Reduce To get ITT in green sector End of procedure. PIM TBM 960 - Edition 0 Page 3A.3.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 184 On ground: ► Do not take off ◄ Inform maintenance department. The airplane is grounded, repair before further flight. End of procedure. PIM TBM 960 - Edition 0 Page 3A.3.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 185 The single engine indicator may switch to NG parameter depending on engine conditions. If after 10 seconds exceedance is still: - THROTTLE ................Reduce To get parameter in green sector End of procedure. PIM TBM 960 - Edition 0 Page 3A.3.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 186 THROTTLE is out of IDLE position. - GND FEATHER switch ..............OFF Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3A.3.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 187 THROTTLE (including reverse range). - THROTTLE ..................... IDLE - Continue start procedure normally. End of procedure. PIM TBM 960 - Edition 0 Page 3A.3.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 188 ► Do not perform a go-around ◄ NOTE NO DISPATCH will be displayed when on ground, refer to procedure DISPATCH in Subsection 3.13. End of procedure. PIM TBM 960 - Edition 0 Page 3A.3.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 189 NOTE NO DISPATCH will be displayed when on ground, refer to procedure DISPATCH in Subsection 3.13. End of procedure. PIM TBM 960 - Edition 0 Page 3A.3.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 190 On ground: ► Do not take off ◄ Inform maintenance department. The airplane is grounded, repair before further flight. End of procedure. PIM TBM 960 - Edition 0 Page 3A.3.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 191 On ground: ► Do not take off ◄ Inform maintenance department. The airplane is grounded, repair before further flight. End of procedure. PIM TBM 960 - Edition 0 Page 3A.3.9 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 192 Section 3A Abnormal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3A.3.10 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 193 Section 3A Abnormal Procedures Pilot's Information Manual 3A.4 - Air Start No Abnormal Procedures Refer to Section 3 for Emergency Procedures. PIM TBM 960 - Edition 0 Page 3A.4.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 194 Section 3A Abnormal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3A.4.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 195 Section 3A Abnormal Procedures Pilot's Information Manual 3A.5 - Fire and Smoke No Abnormal Procedures Refer to Section 3 for Emergency Procedures. PIM TBM 960 - Edition 0 Page 3A.5.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 196 Section 3A Abnormal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3A.5.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 197 Section 3A Abnormal Procedures Pilot's Information Manual 3A.6 - Emergency Descents No Abnormal Procedures Refer to Section 3 for Emergency Procedures. PIM TBM 960 - Edition 0 Page 3A.6.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 198 Section 3A Abnormal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3A.6.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 199 NOTE Pressing the MASTER CAUTION pushbutton mutes the "Landing gear / Landing gear" voice alert above 800 ft AGL. End of procedure. PIM TBM 960 - Edition 0 Page 3A.7.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 200 IAS < 122 KIAS for deflections greater than TO position. At landing: - Perform procedure ........Landing with Flaps Malfunction End of procedure. PIM TBM 960 - Edition 0 Page 3A.7.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 201 Proceed as for a normal landing with 100 KIAS of approach airspeed. Provide for a landing distance increased by 50%. End of procedure. PIM TBM 960 - Edition 0 Page 3A.7.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 202 End of procedure ■ If not: - LDG GEAR breaker ............... Push - Perform procedure ........Emergency Gear Extension End of procedure. PIM TBM 960 - Edition 0 Page 3A.7.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 203 Symptoms have to be considered at the end of the sequence. - Airspeed .............. Maintain below 150 KIAS - Perform procedure ..........Emergency Gear Extension End of procedure. PIM TBM 960 - Edition 0 Page 3A.7.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 204 - Landing gear emergency pump handle ..........Actuate With maximum amplitude until pump hardening - MASTER WARNING pushbutton ............Press GEAR UNSAFE To reset the Continue ► PIM TBM 960 - Edition 0 Page 3A.7.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 205 (or more) green light(s) is(are) not ON and/or flickering while pressing the CHECK DOWN pushbutton: A gear unlock condition is confirmed. Continue ► PIM TBM 960 - Edition 0 Page 3A.7.7 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 206 If one main landing gear is not down, it is recommended to land with landing gear up – refer to procedure Landing with Gear Up End of procedure. PIM TBM 960 - Edition 0 Page 3A.7.8 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 207: Throttle

    13 - ENGINE MODE switch ............OFF 14 - FUEL TANK SELECTOR ............OFF 15 - Crash lever ..............Pull down Continue ► PIM TBM 960 - Edition 0 Page 3A.7.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 208 21 - FUEL TANK SELECTOR ............OFF 22 - Shut down the engine. Refer to procedure Shutdown in Subsection 4.4. 23 - Evacuate. End of procedure. PIM TBM 960 - Edition 0 Page 3A.7.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 209 13 - Crash lever ..................Pull down 14 - Evacuate the airplane after coming to complete stop. Do not unfasten seat belts before complete stop End of procedure. PIM TBM 960 - Edition 0 Page 3A.7.11 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 210 11 - Crash lever ..................Pull down 12 - Evacuate the airplane after coming to complete stop. Do not unfasten seat belts before complete stop End of procedure. PIM TBM 960 - Edition 0 Page 3A.7.12 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 211 - Adjust elevator by using the manual pitch trim wheel. When ground approaches: - Slope ................. Decrease progressively - TRQ ................Reduce progressively End of procedure. PIM TBM 960 - Edition 0 Page 3A.7.13 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 212: Acft Conf Mism

    178 KIAS Landing gear retraction 150 KIAS GEAR UNSAFE is ON: - Perform procedure ..... Landing Gear Extension Discrepancy End of procedure. PIM TBM 960 - Edition 0 Page 3A.7.14 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 213: Hs Abn Brakes

    When possible, and at the latest before 200 ft on final: - AP/TRIM DISC pushbutton ............Press twice AP / AT also disengage End of procedure. PIM TBM 960 - Edition 0 Page 3A.7.15 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 214 Section 3A Abnormal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3A.7.16 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 215: 3A.8 - Fuel System

    - AUX BP switch ................ ON - Avoid high power and rapid movements of the THROTTLE. ► Land as soon as possible ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3A.8.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 216: Auto Sel

    - FUEL SEL pushbutton ..............MAN Status light in green - Select tanks manually ............As required CAUTION Maximum fuel imbalance is 15 USG. End of procedure. PIM TBM 960 - Edition 0 Page 3A.8.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 217: Fuel Imbalance

    - Fullest tank .................. Select By shifting FUEL TANK SELECTOR manually ► Fly the airplane ◄ CAUTION Maximum fuel imbalance is 15 USG. End of procedure. PIM TBM 960 - Edition 0 Page 3A.8.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 218: Low Lvl Fail L-R

    If any doubt: ► Land as soon as practicable ◄ ► Fly the airplane ◄ On the ground: Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3A.8.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 219: Fuel Clogging

    On ground: ► Do not take off ◄ Inform maintenance department. The airplane is grounded, repair before further flight. End of procedure. PIM TBM 960 - Edition 0 Page 3A.8.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 220 Section 3A Abnormal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3A.8.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 221: 3A.9 - Electrical System

    If this indication remains steady at a high value: It may be due to a battery or generation system failure. End of procedure. PIM TBM 960 - Edition 0 Page 3A.9.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 222: Bat Off

    - SOURCE selector ................BATT If warning persists: ► Land as soon as possible ◄ - Airplane mains voltage ............... Monitor End of procedure. PIM TBM 960 - Edition 0 Page 3A.9.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 223: Main Gen

    - GENERATOR selector ..............ST-BY If necessary: - ST-BY GENERATOR RESET pushbutton ......Press - Maintain ST-BY loads below 100 A. End of procedure. PIM TBM 960 - Edition 0 Page 3A.9.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 224: Low Voltage

    - GENERATOR selector ..............ST-BY If necessary: - ST-BY GENERATOR RESET pushbutton ......Press - Maintain ST-BY loads below 100 A. End of procedure. PIM TBM 960 - Edition 0 Page 3A.9.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 225: Main Gen And Low Voltage

    Return to VMC conditions, if possible. - GENERATOR selector ............OFF If airplane altitude is > 10,000 ft: 10 - OXYGEN switch ............. ON Continue ► PIM TBM 960 - Edition 0 Page 3A.9.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 226 22 - AIRFRAME DE ICE ........OFF Status light in white 23 - PROP DE ICE ..........OFF Status light in white Continue ► PIM TBM 960 - Edition 0 Page 3A.9.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 227 > 95 KIAS If time permits: 37 - AIR COND breaker ............Pull ► Land as soon as possible ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3A.9.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 228 Section 3A Abnormal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3A.9.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 229: 3A.10 - Pressurization And Air Conditioning

    ECS DEGRADED 1 / 1 Indicates an ECS malfunction. - Shorten the flight. Inform maintenance department before next flight. End of procedure. PIM TBM 960 - Edition 0 Page 3A.10.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 230: Pressu Backup

    The pilot should take into account the airplane descent profile in order to avoid pressure annoyance. End of procedure. PIM TBM 960 - Edition 0 Page 3A.10.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 231: Cabin Not Depressurized After Landing

    If necessary: - EMERGENCY RAM AIR control knob ........Pull - Wait for complete cabin depressurization before opening any door. End of procedure. PIM TBM 960 - Edition 0 Page 3A.10.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 232: Vacuum Low

    ► Return to VMC conditions as soon as possible. ◄ ► Fly the airplane ◄ - BLEED switch ................ OFF/RST End of procedure. PIM TBM 960 - Edition 0 Page 3A.10.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 233: Defog Malfunction

    In flight, the cabin will quickly depressurize. Therefore, the cabin vertical speed indicator and altimeter indications will rapidly meet those of respectively the airplane VSI and altimeter. End of procedure. PIM TBM 960 - Edition 0 Page 3A.10.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 234 Section 3A Abnormal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 3A.10.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 235: 3A.11 - Deicing System

    - DE ICE SYSTEM mode switch ............... MAN All deicing systems turn on - AIRFRAME DE ICE pushbutton .............. OFF Status light in white End of procedure. PIM TBM 960 - Edition 0 Page 3A.11.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 236: Prop Deice Fail

    - DE ICE SYSTEM mode switch ............... MAN All deicing systems turn on - PROP DE ICE pushbutton ..............OFF Status light in white End of procedure. PIM TBM 960 - Edition 0 Page 3A.11.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 237: Inert Sep Fail

    INERT DE ICE breaker triggered. ► Leave icing conditions as soon as possible ◄ ► Fly the airplane ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3A.11.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 238: Windshield Deicing Failure

    The demisting function is automatically switched OFF 10 minutes after the DEFOG pushbutton has been set to ON. Before landing: - Wait for a sufficient visibility. End of procedure. PIM TBM 960 - Edition 0 Page 3A.11.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 239: Windshield Misting Or Internal Icing

    - Clean the left-side window. - Perform a sideslip approach with rudder pedals to the right. To get sufficient landing visual references Continue ► PIM TBM 960 - Edition 0 Page 3A.11.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 240 2 / 2 ► Continuing For landing: 10 - FLAPS lever ................... LDG 11 - Airspeed ............Maintain above 95 KIAS End of procedure. PIM TBM 960 - Edition 0 Page 3A.11.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 241: Pitot No Ht L-R

    ► Fly the airplane ◄ - Airspeed ............Monitor below 266 KIAS End of procedure. PIM TBM 960 - Edition 0 Page 3A.11.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 242: Stall No Heat

    - Airspeed ..................... Monitor Maintain minimum airspeed according to airplane configuration and icing conditions ► Fly the airplane ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3A.11.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 243: Ice Detected

    Icing conditions are no longer detected by the ice detector. - DE ICE SYSTEM mode switch ........... As required End of procedure. PIM TBM 960 - Edition 0 Page 3A.11.9 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 244: Ice Detection Fail

    AIRFRAME DE ICE / PROP DE ICE / WINDSHIELD systems will be forced to ON for the remainder of the flight. There is no time limitation to the use of deicing systems. End of procedure. PIM TBM 960 - Edition 0 Page 3A.11.10 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 245: 3A.12 - Avionics Miscellaneous

    100 < KIAS < 178 Flaps LDG 85 < KIAS < 122 - Continue the flight. Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 246 ► Fly the airplane ◄ - Airspeed .............. Maintain below 266 KIAS - Continue the flight. Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 247 100 < KIAS < 178 Flaps LDG 85 < KIAS < 122 - Continue the flight. Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 248 If symptoms persist, as well as on the electronic standby instrument on the left-side instrument panel: - Perform a precautionary approach maintaining an adequate airspeed. End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 249 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 ..............Correct End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 250: Autopilot Or Electric Pitch Trim Malfunction

    - AP/TRIMS switch ..................OFF - AP/TRIM DISC pushbutton ............... Release If necessary: - Control wheel ................Retrim End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 251: Dual Gps/Sbas Failure

    - Navigation ..Use the airplane symbol, magenta course line on the map display and the amber CDI for course information Continue ► PIM TBM 960 - Edition 0 Page 3A.12.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 252 The airplane symbol is removed from all maps. The map will remain centered at the last known position. NO GPS POSITION will be annunciated in the center of the map. End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 253: Apr Dwngrade

    For more details on the approach downgrading process, refer to Paragraph Garmin Integrated Flight Deck (GIFD) Approaches in Subsection 7.15. End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.9 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 254: Pit In Ap Vertical Mode During Fd Approach With Vertical

    ► Fly the airplane ◄ Actions: If automatic downgrade to LNAV: - Update minimums as appropriate. If not: ► Perform a go-around ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.10 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 255: Vdi Or Vdi On Approach

    VDI or VDI at bottom of VDI window. ► Fly the airplane ◄ If possible: - Use LNAV minimums. If not: ► Perform a go-around ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.11 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 256: Left Pfd Failure

    - L.H. DISPLAY BACKUP ..............Engage TAS system is lost. - XFR button (on AFCS) ....... Press / to right side then left side End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.12 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 257: Ahrs Failure

    - FD specific modes ........Engaged as desired HDG, NAV, ALT, etc - Fly the airplane manually to follow Command Bars. End of procedure ■ Continue ► PIM TBM 960 - Edition 0 Page 3A.12.13 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 258 - AHRS1 on PFD1 and/or AHRS2 on PFD2 ......Reset - BOTH ON AHRS1 or BOTH ON AHRS2 annunciation ..Check - FD ................Use normally As desired End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.14 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 259: Adc Failure

    - ADC1 on PFD1 and/or ADC2 on PFD2 ......Reset - BOTH ON ADC1 or BOTH ON ADC2 annunciation . Check OFF NOTE AT may be possibly disengaged. End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.15 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 260: Mfd Failure

    If PFD 2 is in full screen mode, it will be splitted a few seconds after MFD failure. Lost systems: MFD. Actions: - L.H. DISPLAY BACKUP button ............. Press - MFD breaker ................Check pushed End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.16 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 261: Xpdr1 Fail Or Xpdr2 Fail

    - Inform Air Traffic Control of the loss of the second transponder. - Leave controlled airspace. - Continue the flight. Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.17 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 262: Xpdr1 Ads-B Fail Or Xpdr2 Ads-B Fail

    If transponder 2 [or transponder 1] is unavailable: - Inform Air Traffic Control. - Leave ADS-B OUT airspace. - Continue the flight. Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.18 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 263: Gwx Fail

    - WXR breaker ................Check pushed - Continue the flight by using other weather data source, and adjust flight route. Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.19 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 264: Tcas Fail

    No active traffic available, but ADS-B IN traffic may still be displayed. ► Fly the airplane ◄ Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.20 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 265: Traffic Fail

    No active traffic available, but ADS-B IN traffic may still be displayed. ► Fly the airplane ◄ Inform maintenance department. End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.21 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 266: Exceedance

    (> V EXCEEDANCE is only displayed at engine shutdown. Inform maintenance department before next flight. End of procedure. PIM TBM 960 - Edition 0 Page 3A.12.22 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 267: 3A.13 - Miscellaneous

    ► Fly the airplane ◄ - Airspeed ..................Reduce To minimum available ► Land as soon as practicable ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3A.13.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 268: Gpu Door

    ► Fly the airplane ◄ - Airspeed ..................Reduce To minimum available ► Land as soon as practicable ◄ End of procedure. PIM TBM 960 - Edition 0 Page 3A.13.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 269: Ignition

    Status light in blue ► Fly the airplane ◄ NOTE IGNITION pushbutton may be left ON for a long period. End of procedure. PIM TBM 960 - Edition 0 Page 3A.13.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 270: Lmtd Dispatch

    50-flight-hour time period. Calculating the 50-flight-hour time period is the pilot's responsibility. Inform maintenance department to anticipate maintenance action. End of procedure. PIM TBM 960 - Edition 0 Page 3A.13.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 271 4.4.16 Before Starting Engine ............4.4.19 In-Flight Available Oxygen Quantity (Crew oxygen masks in NORMAL mode) ..............4.4.22 Engine Start ................4.4.23 PIM TBM 960 - Edition 0 Page 4.0.1 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 272 Weather (- 25 °C to - 40 °C) – Envelope 2 and 3 ....4.5.19 Landing Procedure with Strong Headwind or Crosswind ..4.5.25 PIM TBM 960 - Edition 0 Page 4.0.2 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 273 Section 4 Normal Procedures Pilot's Information Manual Utilization on Grass Runway ..........4.5.27 GPS Navigation ..............4.5.29 PIM TBM 960 - Edition 0 Page 4.0.3 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 274 Section 4 Normal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 4.0.4 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 275: General

    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. PIM TBM 960 - Edition 0 Page 4.1.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 276 Section 4 Normal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 4.1.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 277: Airspeeds For Normal Operation

    Approach airspeed Flaps LDG Maximum operating speed (V Landing gear and flaps UP Glide airspeed (maximum L/D ratio) Landing gear and flaps UP PIM TBM 960 - Edition 0 Page 4.2.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 278 Section 4 Normal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 4.2.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 279: Checklist Procedures

    21 - FAN ......................OFF 22 - THROTTLE ..................... IDLE 23 - FUEL TANK SELECTOR ............Open / L or R Continue ► PIM TBM 960 - Edition 0 Page 4.3.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 280 25 - EMERGENCY RAM AIR ............../ Pushed 26 - ESS BUS TIE ..............NORM / Guarded 27 - Breakers ..................All pushed End of procedure. PIM TBM 960 - Edition 0 Page 4.3.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 281: Before Starting Engine

    18 - VOLTS: BAT > 24.5 V / GPU ≈ 28 V ............ Check 19 - CAS ...................... Check 20 - FLAPS ....................... UP End of procedure. PIM TBM 960 - Edition 0 Page 4.3.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 282: Engine Start

    For all other cases, the airplane is grounded. Inform maintenance department. End of procedure ■ Continue ► PIM TBM 960 - Edition 0 Page 4.3.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 283 Pilot's Information Manual Engine Start 2 / 2 ► Continuing When Ng > 45%: 10 - Starter ..............Check OFF automatically End of procedure. PIM TBM 960 - Edition 0 Page 4.3.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 284: Manual Dry Motoring

    Maintain ON during the motoring sequence After 30 seconds maximum: - STARTER ....................OFF 10 - Engine crank mode ................. OFF End of procedure. PIM TBM 960 - Edition 0 Page 4.3.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 285: After Engine Start With Gpu

    When Np < 400 RPM: - GPU ....................Disconnect GPU DOOR ................Check OFF - GND FEATHER ..................OFF End of procedure. PIM TBM 960 - Edition 0 Page 4.3.7 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 286: After Engine Start

    11 - FAN ....................As required 12 - SEATS HTRS MASTER ............... As required 13 - BLEED ....................AUTO End of procedure. PIM TBM 960 - Edition 0 Page 4.3.8 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 287: Before Taxiing

    11 - WX radar ..................STBY 12 - EIS ......................Check 13 - CAS ...................... Check 14 - TAXI lights ....................ON End of procedure. PIM TBM 960 - Edition 0 Page 4.3.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 288: Before Line Up

    19 - Instruments departure setting ............... Check 20 - SID (PROC) ....................Set 21 - ALT SEL ....................Set 22 - XPDR squawk ................... Set Continue ► PIM TBM 960 - Edition 0 Page 4.3.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 289 Airspeed 6,500 7,000 (lbs) 6,579 7,394 (up to 7,615) Weight 2,984 3,354 (up to 3,454) (kg) 2,800 3,000 3,200 End of procedure. PIM TBM 960 - Edition 0 Page 4.3.11 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 290: Normal Takeoff

    - Brakes ....................Apply 10 - LANDING GEAR ..................UP When airspeed above 115 KIAS: 11 - FLAPS ....................... UP End of procedure. PIM TBM 960 - Edition 0 Page 4.3.12 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 291: Short Takeoff

    10 - Brakes ....................Apply 11 - LANDING GEAR ..................UP When airspeed above 115 KIAS: 12 - FLAPS ....................... UP End of procedure. PIM TBM 960 - Edition 0 Page 4.3.13 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 292: After Takeoff

    - EIS ......................Check - CAS ...................... Check - DE ICE SYSTEM ................. As required - INERT SEP .................. As required End of procedure. PIM TBM 960 - Edition 0 Page 4.3.14 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 293: Climb

    12 - DE ICE SYSTEM ................. As required 13 - INERT SEP .................. As required 14 - LDG lights ..................As required End of procedure. PIM TBM 960 - Edition 0 Page 4.3.15 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 294: Cruise

    11 - INERT SEP .................. As required 12 - LDG lights ..................As required 13 - Top of descent ................Computed End of procedure. PIM TBM 960 - Edition 0 Page 4.3.16 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 295: Before Descent

    - AMPS / VOLTS ..................Check - DE ICE SYSTEM mode .............. As required - INERT SEP .................. As required End of procedure. PIM TBM 960 - Edition 0 Page 4.3.17 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 296: Approach

    - DE ICE SYSTEM mode .............. As required - INERT SEP ....................ON When below FL 100: 10 - LDG lights ....................ON End of procedure. PIM TBM 960 - Edition 0 Page 4.3.18 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 297: Final Approach (In Gs) Or Downwind Leg (Vmc)

    1 / 1 - LDG lights ....................ON - LANDING GEAR ..................DN Check three green - FLAPS ....................... TO End of procedure. PIM TBM 960 - Edition 0 Page 4.3.19 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 298: Short Final (Around 500 Ft)

    - LANDING GEAR .................. Check DN and three green - FLAPS ..................... LDG - AP / YD / AT ................. Disconnect End of procedure. PIM TBM 960 - Edition 0 Page 4.3.20 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 299: Runway Clear

    - FLAPS ....................... UP - FAN ....................As required - XPDR ....................Check 10 - WX radar ................Check STANDBY End of procedure. PIM TBM 960 - Edition 0 Page 4.3.21 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 300: Shutdown

    After inertial separator retraction, about 40 seconds: 17 - SOURCE ....................OFF 18 - Crash lever ..................Pull down 19 - Standby instruments ................OFF End of procedure. PIM TBM 960 - Edition 0 Page 4.3.22 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 301: Outside Check After Shutdown

    - Install air inlet and static port plugs, and exhaust and pitot covers. NOTE Check oil level within 15 to 20 minutes following engine shutdown. End of procedure. PIM TBM 960 - Edition 0 Page 4.3.23 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 302 Section 4 Normal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 4.3.24 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 303: Amplified Procedures

    Remove tie-downs. For quantities, products and specifications of products and materials currently used, refer to Paragraph Maintenance in Subsection 8.7. Continue ► PIM TBM 960 - Edition 0 Page 4.4.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 304 Pilot's Information Manual Preflight Inspection 2 / 15 ► Continuing Figure 4.4.1 - Preflight Inspection Initial inside inspection Cockpit - I Continue ► PIM TBM 960 - Edition 0 Page 4.4.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 305 13 - Door ..................In place NOTE The bypass selector must be pushed at its maximum stop, so as to have the door in place. Continue ► PIM TBM 960 - Edition 0 Page 4.4.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 306 Overhead panel 28 - OXYGEN switch ................OFF 29 - PASSENGER OXYGEN switch ............ STBY 30 - Emergency lighting ..............Check Continue ► PIM TBM 960 - Edition 0 Page 4.4.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 307 GPU + battery. Make sure that a GPU is connected and powering the airplane. 36 - Voltage .............. Check ≈ 28 Volts Continue ► PIM TBM 960 - Edition 0 Page 4.4.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 308 44 - EXT LIGHTS panel ..............All OFF Instrument panel, MFD 45 - CAS display ................. Check 46 - Left and right fuel quantities ............Check Continue ► PIM TBM 960 - Edition 0 Page 4.4.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 309 55 - Crash lever ................Pull down Cabin - II 56 - Cabin fire extinguisher ..........Pressure / Attachment 57 - Seats / belts ..................Check Continue ► PIM TBM 960 - Edition 0 Page 4.4.7 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 310 When the airplane is stored for extended periods of time, a thorough preflight inspection is recommended. Particular attention should be paid to possible Continue ► PIM TBM 960 - Edition 0 Page 4.4.8 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 311 Air vent is not likely to be obstructed by ice or water, as it is located in a wing lower surface recess. 73 - Left-side pitot ................... Condition Continue ► PIM TBM 960 - Edition 0 Page 4.4.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 312 79 - Shock absorber ................Check 80 - Doors ................... Check 81 - Tire ....................Check 82 - Wheel well ................... Check Continue ► PIM TBM 960 - Edition 0 Page 4.4.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 313 87 - Filter contamination indicator (clogging indicator) ........ Check 88 - Left-side exhaust stub ..........Condition / No cracks Continue ► PIM TBM 960 - Edition 0 Page 4.4.11 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 314 (two rectangular grilles located forward of the circular grille). 96 - Propeller and spinner ... No nicks, cracks or oil leaks / Attachment Continue ► PIM TBM 960 - Edition 0 Page 4.4.12 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 315 Additional remarks are identical to those of left-side wing. 102 - Fuel tank drain (two on each wing) ............Drain Fuel free of water and contamination Continue ► PIM TBM 960 - Edition 0 Page 4.4.13 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 316 Check that outside handle of emergency exit is flush with door skin. 121 - ELT ....................ARM/OFF 122 - ELT door ................Closed / Locked Continue ► PIM TBM 960 - Edition 0 Page 4.4.14 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 317 131 - Static dischargers ................Condition 132 - Tail cone / nav. lights / strobe ............Condition 133 - Static pressure ports ................Clean End of procedure. PIM TBM 960 - Edition 0 Page 4.4.15 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 318: Inside Inspection

    - Pilot's and passengers' belts and harnesses ....Fasten Ensure correct positioning of front seat occupiers’ safety belt buckles by using the buckle positioners Continue ► PIM TBM 960 - Edition 0 Page 4.4.16 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 319 14 - INT LIGHTS panel ................All OFF 15 - CABIN switch ..................OFF 16 - ACCESS switch ..................OFF Continue ► PIM TBM 960 - Edition 0 Page 4.4.17 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 320 35 - EMERGENCY RAM AIR ............Closed / Pushed 36 - ESS BUS TIE switch ............NORM / Guarded 37 - Breakers ..................All pushed End of procedure. PIM TBM 960 - Edition 0 Page 4.4.18 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 321: Before Starting Engine

    If battery voltage < 24.5 V: 12 - Ask for a GPU and be ready to a GPU start. 13 - GENERATOR selector ................MAIN Continue ► PIM TBM 960 - Edition 0 Page 4.4.19 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 322 28 - FUEL SEL pushbutton ................MAN Status light in green 29 - MFD ....................Initialize 30 - Fuel on board ..................Check Check quantity Continue ► PIM TBM 960 - Edition 0 Page 4.4.20 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 323 For that, press on brake pedals before turning brake selector to the right. End of procedure. PIM TBM 960 - Edition 0 Page 4.4.21 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 324: In-Flight Available Oxygen Quantity (Crew Oxygen Masks In Normal Mode)

    4.4.2. Table 4.4.1 - Oxygen Duration Duration: Passengers, Duration: Passengers, Number of passengers plus 1 pilot plus 2 pilots End of procedure. PIM TBM 960 - Edition 0 Page 4.4.22 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 325 Starter operation is bound by limitations – refer to Subsection 2.4. Starter Operation Limits. 10 - STARTER switch ..................ON 2 seconds, then release Continue ► PIM TBM 960 - Edition 0 Page 4.4.23 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 326 – refer to procedure Manual Dry Motoring ABORTING START 16 - ............. Check ON AUX BP ON 17 - ............... Check OFF Continue ► PIM TBM 960 - Edition 0 Page 4.4.24 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 327 In ISA conditions at sea level, Ng ≈ 58.5%. Ng may vary between 55% and 63% depending on external conditions. End of procedure. PIM TBM 960 - Edition 0 Page 4.4.25 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 328: Manual Dry Motoring

    11 - STARTER switch ..................ON Maintain ON during the motoring sequence Simultaneously: 12 - Timer clock ....................Start STARTER 13 - ..................Check ON Continue ► PIM TBM 960 - Edition 0 Page 4.4.26 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 329 It is recommended to avoid more than two consecutive motoring between two engine starts, to minimize potential leakages of the bearing #1 lab seal. End of procedure. PIM TBM 960 - Edition 0 Page 4.4.27 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 330: After Engine Start With Gpu

    On EIS of MFD 14 - CAS display ..................Check 15 - FAN selector ................. As required 16 - BLEED switch ..................AUTO Continue ► PIM TBM 960 - Edition 0 Page 4.4.28 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 331 2 / 2 ► Continuing When ground personnel is cleared from propeller area: 17 - Perform procedure ............. After Engine Start End of procedure. PIM TBM 960 - Edition 0 Page 4.4.29 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 332: After Engine Start

    When MAIN LOAD < 80 A: 11 - GENERATOR selector ............ST-BY To perform test 12 - AMPS / VOLTS ..............Check Continue ► PIM TBM 960 - Edition 0 Page 4.4.30 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 333 NOTE The demisting function is automatically switched OFF 10 minutes after the DEFOG pushbutton has been set to ON. End of procedure. PIM TBM 960 - Edition 0 Page 4.4.31 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 334: Before Taxiing

    Keep ON while taxiing in order to avoid ingestion of particles by the engine - Flight controls ..................Check Proper operation from stop to stop, full deflection Continue ► PIM TBM 960 - Edition 0 Page 4.4.32 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 335 HOME, AIRCRAFT SYSTEMS, LFE and then MANUAL 20 - VHF / VOR / GPS .............. Adjust / Test Continue ► PIM TBM 960 - Edition 0 Page 4.4.33 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 336 30 - PARK BRAKE ..................OFF Make sure that chocks are removed, if used PARK BRAKE 31 - ................Check OFF End of procedure. PIM TBM 960 - Edition 0 Page 4.4.34 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 337: Taxiing

    Check navigation and communication systems before or during taxiing, check gyroscopic instruments on PFDs 1 / 2 and standby indicator during ground turns End of procedure. PIM TBM 960 - Edition 0 Page 4.4.35 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 338: Before Line Up

    Adjust inside green index sector, depending on the current balance condition 15 - Yaw ..................TO Adjust inside green index sector Continue ► PIM TBM 960 - Edition 0 Page 4.4.36 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 339 27 - Altimeters setting ................. Set / Check 28 - Instruments departure setting ............... Check 29 - SID (PROC) ....................Set 30 - ALT SEL ....................Set Continue ► PIM TBM 960 - Edition 0 Page 4.4.37 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 340 38 - INERT SEP switch ............... As required Depending on external conditions and takeoff performance 39 - Rotation airspeed (V ) ................. Check Continue ► PIM TBM 960 - Edition 0 Page 4.4.38 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 341 All engine parameters must be in green range, except propeller RPM 43 - PARK BRAKE ..................OFF PARK BRAKE 44 - ................Check OFF End of procedure. PIM TBM 960 - Edition 0 Page 4.4.39 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 342: Normal Takeoff

    - Brakes ....................Release 10 - THROTTLE .................. Full forward 11 - Max TRQ ....................Check Corresponding to takeoff performance tables Continue ► PIM TBM 960 - Edition 0 Page 4.4.40 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 343 Continue ► PIM TBM 960 - Edition 0 Page 4.4.41 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 344 It is recommended not to retract FLAPS to UP before 500 ft AGL. 17 - Airspeed ................. 100 KIAS When airspeed above 115 KIAS: 18 - FLAPS lever ....................UP End of procedure. PIM TBM 960 - Edition 0 Page 4.4.42 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 345: Short Takeoff

    - THROTTLE .................. Full forward 10 - Max TRQ ....................Check Corresponding to takeoff performance tables 11 - Brakes ....................Release Continue ► PIM TBM 960 - Edition 0 Page 4.4.43 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 346 GEAR UNSAFE 17 - GEAR UNSAFE red warning light and ..... Check OFF At the end of the sequence Continue ► PIM TBM 960 - Edition 0 Page 4.4.44 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 347 It is recommended not to retract FLAPS to UP before 500 ft AGL. 18 - Airspeed ................. 100 KIAS When airspeed above 115 KIAS: 19 - FLAPS lever ....................UP End of procedure. PIM TBM 960 - Edition 0 Page 4.4.45 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 348: After Takeoff

    - CAS display ..................Check - DE ICE SYSTEM panel ..............As required - INERT SEP switch ............... As required End of procedure. PIM TBM 960 - Edition 0 Page 4.4.46 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 349: Climb

    12 - Fuel gauges ..................Check Verify fuel quantity and imbalance, correct if necessary 13 - AMPS / VOLTS ..................Check Continue ► PIM TBM 960 - Edition 0 Page 4.4.47 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 350 Flight into Severe Icing Conditions in Subsection 4.5. 15 - INERT SEP switch ............... As required 16 - LDG lights ..................As required End of procedure. PIM TBM 960 - Edition 0 Page 4.4.48 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 351: Cruise

    Maximum imbalance 15 USG When the cruise parameters are stabilized, after 4 minutes minimum: 13 - AMPS / VOLTS ..................Check Continue ► PIM TBM 960 - Edition 0 Page 4.4.49 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 352 15 - INERT SEP switch ............... As required 16 - LDG lights ..................As required 17 - Top of descent ................Computed End of procedure. PIM TBM 960 - Edition 0 Page 4.4.50 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 353: Before Descent

    10 - Perform procedure .... Windshield Misting or Internal Icing in Subsection 3A.11. 11 - INERT SEP switch ............... As required End of procedure. PIM TBM 960 - Edition 0 Page 4.4.51 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 354: Approach

    11 - Perform procedure .... Windshield Misting or Internal Icing in Subsection 3A.11. 12 - INERT SEP switch ..................ON Continue ► PIM TBM 960 - Edition 0 Page 4.4.52 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 355 14 - Passenger's briefing ..............As required 15 - Seats, belts, harnesses ............... Locked 16 - Passenger's table ................Stowed End of procedure. PIM TBM 960 - Edition 0 Page 4.4.53 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 356: Final Approach (In Gs) Or Downwind Leg (Vmc)

    - GEAR UNSAFE red warning light ..........Check OFF GEAR UNSAFE ................Check OFF 10 - Amber light ................... Check OFF Continue ► PIM TBM 960 - Edition 0 Page 4.4.54 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 357 11 - FLAPS lever ....................TO Airspeed < 178 KIAS 12 - WX radar mode ..................STBY End of procedure. PIM TBM 960 - Edition 0 Page 4.4.55 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 358: Short Final (Around 500 Ft)

    Disconnect the yaw damper at DH/MDA. Otherwise, pilot will be pushing rudder pedals against the servo. This is particularly significant when landing in a crosswind. End of procedure. PIM TBM 960 - Edition 0 Page 4.4.56 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 359: Landing

    - Brakes ..................As required NOTE Wheels may lock if applying maximum braking at speeds higher than 40 KIAS. End of procedure. PIM TBM 960 - Edition 0 Page 4.4.57 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 360: Go-Around With Ap Off

    When airspeed is at or above 115 KIAS: - FLAPS lever ....................UP - Climb airspeed ................As required - TRQ ....................As required End of procedure. PIM TBM 960 - Edition 0 Page 4.4.58 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 361: Go-Around With Ap On

    When airspeed is at or above 115 KIAS: - FLAPS lever ....................UP - Climb airspeed ................As required - TRQ ....................As required End of procedure. PIM TBM 960 - Edition 0 Page 4.4.59 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 362: Touch And Go

    6,500 7,000 (lbs) 6,579 7,110 Weight 3,225 2,984 (kg) 2,800 3,000 3,200 After wheels touch: - FLAPS lever ....................TO Continue ► PIM TBM 960 - Edition 0 Page 4.4.60 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 363 The POH does not supply distances for touch and go. The pilot must decide whether the runway length is sufficient. NOTE Do not engage AT below 1,000 ft (300 m) AGL. End of procedure. PIM TBM 960 - Edition 0 Page 4.4.61 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 364: Runway Clear

    11 - XPDR ..................Check GND 12 - WX radar ................Check STANDBY The weather radar automatically sets to STANDBY upon touchdown End of procedure. PIM TBM 960 - Edition 0 Page 4.4.62 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 365: Shutdown

    After automatic dry motoring if any: 14 - FUEL TANK SELECTOR ................. OFF 15 - INERT SEP switch .................. OFF Continue ► PIM TBM 960 - Edition 0 Page 4.4.63 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 366 25 - Turn the control knob to select POWER OFF on the menu and press the control knob to turn the standby attitude module off. End of procedure. PIM TBM 960 - Edition 0 Page 4.4.64 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 367: Outside Check After Shutdown

    Check oil level within 15 to 20 minutes following engine shutdown. Refer to Paragraph Engine Oil in Subsection 8.7. End of procedure. PIM TBM 960 - Edition 0 Page 4.4.65 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 368 Section 4 Normal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 4.4.66 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 369: Particular Procedures

    The procedures and procedure elements given in this subsection Particular Procedures supplement the normal procedures or complete certain elements of the normal procedures described in Subsection(s) 4.3 and/or 4.4. PIM TBM 960 - Edition 0 Page 4.5.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 370: Flight Into Known Icing Conditions

    Propeller electrical deice system, Electrical heating system for both pitots and for the stall warning incidence sensor, Windshield electrical deice system, and Continue ► PIM TBM 960 - Edition 0 Page 4.5.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 371 – without manual adjustment of the THROTTLE. If not, adjust engine power manually. - All deicing systems ............... Check ON Continue ► PIM TBM 960 - Edition 0 Page 4.5.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 372 > 6,579 lbs (2,984 kg) Flaps UP 130 KIAS 135 KIAS Flaps TO 110 KIAS 115 KIAS Flaps LDG 90 KIAS 95 KIAS Continue ► PIM TBM 960 - Edition 0 Page 4.5.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 373 Because of the higher landing airspeed, landing distances will be increased. In the landing configuration, using 90 KIAS approach airspeed increases landing distance by 20% – refer to Subsection Landing Distances. End of procedure. PIM TBM 960 - Edition 0 Page 4.5.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 374: Flight Into Severe Icing Conditions

    If the flaps are extended: - Do not retract flaps until the airframe is clear of ice. End of procedure. PIM TBM 960 - Edition 0 Page 4.5.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 375: Flight Under Heavy Precipitations

    - INERT SEP switch ..................ON End of procedure. PIM TBM 960 - Edition 0 Page 4.5.7 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 376: Utilization On Runways Covered With Water

    If takeoff or landing must be performed on a runway covered with water: - IGNITION pushbutton ..............ON Status light in green - INERT SEP switch ................ON End of procedure. PIM TBM 960 - Edition 0 Page 4.5.8 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 377: Utilization On Runways Covered With Melting Or Not Tamped Snow

    If the runway is long enough: - FLAPS lever ................UP Takeoff distances increased by 15% - Rotation airspeed ........Increased by 5 KIAS Continue ► PIM TBM 960 - Edition 0 Page 4.5.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 378 17 - ................Check ON 18 - INERT SEP switch ................ON INERT SEP ON 19 - ..............Check ON Continue ► PIM TBM 960 - Edition 0 Page 4.5.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 379 20 - Do not use the parking brake to prevent brake lock. 21 - Use chocks and/or tie-down the airplane. End of procedure. PIM TBM 960 - Edition 0 Page 4.5.11 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 380: Utilization On Icy Or Covered With Tamped Snow Runways

    - Use brakes only at very low airspeed and progressively. Before line up: - IGNITION pushbutton ..............ON Status light in green IGNITION ................Check ON Continue ► PIM TBM 960 - Edition 0 Page 4.5.12 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 381 Make turns at a very low airspeed, engine torque tends to make the airplane turn to the left. 20 - Use brakes only at very low airspeed and progressively. Continue ► PIM TBM 960 - Edition 0 Page 4.5.13 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 382 21 - Do not use the parking brake to prevent brake lock. 22 - Use chocks and/or tie-down the airplane. End of procedure. PIM TBM 960 - Edition 0 Page 4.5.14 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 383: Utilization In Cold Weather (0 °C To -25 °C) And Very Cold Weather (-25 °C To -40°C)

    GPU starting Normal procedures ENVELOPE 1 Normal procedures BAT starting OAT (°C) - 30 - 40 - 20 - 10 End of procedure. PIM TBM 960 - Edition 0 Page 4.5.15 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 384: Utilization In Cold Weather (0 °C To -25 °C) And Very Cold Weather (-25 °C To -40 °C) - Envelope

    All deicing systems turn on 10 - INERT SEP switch ............Check ON INERT SEP ON 11 - ............Check ON Continue ► PIM TBM 960 - Edition 0 Page 4.5.16 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 385 21 - Perform normal procedures defined in Subsection(s) 4.3 and/or 4.4. 22 - Use chocks and/or tie-down the airplane using anchor points on ground. Continue ► PIM TBM 960 - Edition 0 Page 4.5.17 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 386 3 / 3 ► Continuing 23 - Install air inlet and static port plugs, and exhaust and pitot covers. End of procedure. PIM TBM 960 - Edition 0 Page 4.5.18 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 387: Utilization In Cold Weather (0 °C To - 25 °C) And Very Cold Weather (- 25 °C To - 40 °C) - Envelope 2 And

    - Remove chocks and/or release ties from the airplane. Continue ► PIM TBM 960 - Edition 0 Page 4.5.19 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 388 18 - Ground power unit ..............Connected 19 - SOURCE selector ................GPU GPU DOOR 20 - ................. Check ON Continue ► PIM TBM 960 - Edition 0 Page 4.5.20 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 389 35 - Engine parameters ..............Check NOTE Ng depends on external conditions. AUX BP ON 36 - ............... Check OFF Continue ► PIM TBM 960 - Edition 0 Page 4.5.21 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 390 51 - Allow the cabin to heat respecting defined time – see Figure 4.5.2. Before switching on the navigation and monitoring systems. This allows to respect Continue ► PIM TBM 960 - Edition 0 Page 4.5.22 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 391 Utilization in Cold Weather (0 °C to -25 °C) and Very Cold Weather (-25 °C to -40 °C) – Envelope 1 Continue ► PIM TBM 960 - Edition 0 Page 4.5.23 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 392 Subsection Utilization in Cold Weather (-0 °C to -25 °C) or Very Cold Weather (-25 °C to -40 °C). End of procedure. PIM TBM 960 - Edition 0 Page 4.5.24 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 393: Landing Procedure With Strong Headwind Or Crosswind

    - Generate a slideslip with the rudder in order to align fuselage with the runway (i.e left crosswind, left wing low). Continue ► PIM TBM 960 - Edition 0 Page 4.5.25 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 394 Maximum demonstrated crosswind for landing is 20 kt. The most restrictive situation is as follows: takeoff with wind coming from the left, wet runway, aft C.G. End of procedure. PIM TBM 960 - Edition 0 Page 4.5.26 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 395 - Reverse ..............Only if necessary CAUTION Do not maintain reverse at airspeeds below 40 KIAS to avoid ingestion of foreign matter. Continue ► PIM TBM 960 - Edition 0 Page 4.5.27 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 396 This will damage the propeller and, after ingestion, the engine internal components (compressor and turbine blades). End of procedure. PIM TBM 960 - Edition 0 Page 4.5.28 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 397 In the scope of these additions, the pilot must pay attention not to duplicate points. End of procedure. PIM TBM 960 - Edition 0 Page 4.5.29 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 398 Section 4 Normal Procedures Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 4.5.30 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 399 Climb Performance after Go-Around ........5.10.11 Climb Performance – Flaps TO ..........5.10.12 5.11 - Cruise Performance ..............5.11.1 Maximum Cruise ..............5.11.1 PIM TBM 960 - Edition 0 Page 5.0.1 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 400 5.14.1 Weight 7,110 lbs (3,225 kg) ..........5.14.2 Weight 6,250 lbs (2,835 kg) ..........5.14.3 Weight 5,071 lbs (2,300 kg) ..........5.14.4 PIM TBM 960 - Edition 0 Page 5.0.2 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 401: General

    INERT SEP is ON, and P2.5 HI message is ON. Supplements in Section 9 provide specific airplane performance associated with optional equipment and systems. PIM TBM 960 - Edition 0 Page 5.1.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 402 Section 5 Performance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 5.1.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 403: Noise Level

    No determination has been made by the Federal Aviation Administration that the noise levels of this airplane are or should be acceptable or unacceptable for operation at, into or out of any airport. PIM TBM 960 - Edition 0 Page 5.2.1 Rev. 00...
  • Page 404 Section 5 Performance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 5.2.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 405: Airspeed Calibration

    LDG GR DN LDG GR DN KIAS KCAS KIAS KCAS KIAS KCAS MPH IAS MPH CAS MPH IAS MPH CAS MPH IAS MPH CAS PIM TBM 960 - Edition 0 Page 5.3.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 406 LDG GR DN LDG GR DN KIAS KCAS KIAS KCAS KIAS KCAS MPH IAS MPH CAS MPH IAS MPH CAS MPH IAS MPH CAS PIM TBM 960 - Edition 0 Page 5.3.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 407: Cabin Pressurization Envelope

    Figure 5.4.1 - Cabin Pressurization Operating Envelope Cabin altitude (feet) 10,000 9,000 8,000 7,000 6,000 5,000 4,000 3,000 2,000 1,000 Flight Level (FL) PIM TBM 960 - Edition 0 Page 5.4.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 408 Section 5 Performance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 5.4.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 409: Sat - Oat Conversions

    - 24 31,000 - 67 - 66 - 57 - 56 - 47 - 46 - 37 - 36 - 27 - 26 PIM TBM 960 - Edition 0 Page 5.5.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 410 Section 5 Performance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 5.5.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 411: Stall Speeds

    7,394 to 7,615* (3,354 to 3,454*) * Stall speeds remain the same when increasing weight because C.G. changes at the same time. PIM TBM 960 - Edition 0 Page 5.6.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 412 Section 5 Performance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 5.6.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 413: Wind Components

    20 kts : Demonstrated crosswind 0° 20° 30° 40° 10° 50° 60° 70° 80° 90° 100° 110° 140° 160° 120° 180° Crosswind components - kts PIM TBM 960 - Edition 0 Page 5.7.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 414 Section 5 Performance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 5.7.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 415: Engine Operation

    TRQ setting = 82% for IAS = 124 KIAS – see Table 5.8.3. Maximum cruise power: TRQ setting = 94% – see Table 5.8.21. PIM TBM 960 - Edition 0 Page 5.8.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 416: Maximum Climb Power - 124 Kias

    Table 5.8.3 P2.5 HI or P3 Table 5.8.4 Table 5.8.5 P2.5 Table 5.8.6 Table 5.8.7 P2.5 HI or P3 Table 5.8.8 Table 5.8.9 PIM TBM 960 - Edition 0 Page 5.8.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 417 CAS message is OFF, and messages are OFF. Table 5.8.2 - MXCL Power (FL < 200) – 124 KIAS Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 418 Table 5.8.2 - MXCL Power (FL < 200) – 124 KIAS Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 419 CAS message is OFF, and messages are OFF. Table 5.8.3 - MXCL Power (FL > 200) – 124 KIAS Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 420 Table 5.8.3 - MXCL Power (FL > 200) – 124 KIAS Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 421 ON. Table 5.8.4 - MXCL Power (FL < 200) – 124 KIAS [P2.5 HI or P3] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.7 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 422 Table 5.8.4 - MXCL Power (FL < 200) – 124 KIAS [P2.5 HI or P3] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.8 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 423 ON. Table 5.8.5 - MXCL Power (FL > 200) – 124 KIAS [P2.5 HI or P3] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 424 Table 5.8.5 - MXCL Power (FL > 200) – 124 KIAS [P2.5 HI or P3] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 425 OFF. Table 5.8.6 - MXCL Power (FL < 200) – 124 KIAS [INERT SEP] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.11 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 426 Table 5.8.6 - MXCL Power (FL < 200) – 124 KIAS [INERT SEP] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.12 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 427 OFF. Table 5.8.7 - MXCL Power (FL > 200) – 124 KIAS [INERT SEP] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.13 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 428 Table 5.8.7 - MXCL Power (FL > 200) – 124 KIAS [INERT SEP] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.14 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 429 Table 5.8.8 - MXCL Power (FL < 200) – 124 KIAS [INERT SEP – P2.5 HI or P3] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.15 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 430 Table 5.8.8 - MXCL Power (FL < 200) – 124 KIAS [INERT SEP – P2.5 HI or P3] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.16 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 431 Table 5.8.9 - MXCL Power (FL > 200) – 124 KIAS [INERT SEP – P2.5 HI or P3] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.17 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 432 Table 5.8.9 - MXCL Power (FL > 200) – 124 KIAS [INERT SEP – P2.5 HI or P3] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.18 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 433: Maximum Climb Power - 170 Kias / M 0.40

    Table 5.8.12 P2.5 HI or P3 Table 5.8.13 Table 5.8.14 P2.5 Table 5.8.15 Table 5.8.16 P2.5 HI or P3 Table 5.8.17 Table 5.8.18 PIM TBM 960 - Edition 0 Page 5.8.19 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 434 OFF. Table 5.8.11 - MXCL Power (FL < 200) – 170 KIAS / M 0.40 Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.20 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 435 Table 5.8.11 - MXCL Power (FL < 200) – 170 KIAS / M 0.40 Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.21 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 436 OFF. Table 5.8.12 - MXCL Power (FL > 200) – 170 KIAS / M 0.40 Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.22 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 437 Table 5.8.12 - MXCL Power (FL > 200) – 170 KIAS / M 0.40 Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.23 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 438 Table 5.8.13 - MXCL Power (FL < 200) – 170 KIAS / M 0.40 [P2.5 HI or P3] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.24 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 439 Table 5.8.13 - MXCL Power (FL < 200) – 170 KIAS / M 0.40 [P2.5 HI or P3] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.25 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 440 Table 5.8.14 - MXCL Power (FL > 200) – 170 KIAS / M 0.40 [P2.5 HI or P3] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.26 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 441 Table 5.8.14 - MXCL Power (FL > 200) – 170 KIAS / M 0.40 [P2.5 HI or P3] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.27 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 442 Table 5.8.15 - MXCL Power (FL < 200) – 170 KIAS / M 0.40 [INERT SEP] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.28 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 443 Table 5.8.15 - MXCL Power (FL < 200) – 170 KIAS / M 0.40 [INERT SEP] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.29 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 444 Table 5.8.16 - MXCL Power (FL > 200) – 170 KIAS / M 0.40 [INERT SEP] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.30 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 445 Table 5.8.16 - MXCL Power (FL > 200) – 170 KIAS / M 0.40 [INERT SEP] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.31 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 446 Table 5.8.17 - MXCL Power (FL < 200) – 170 KIAS / M 0.40 [INERT SEP – P2.5 HI or P3] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.32 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 447 Table 5.8.17 - MXCL Power (FL < 200) – 170 KIAS / M 0.40 [INERT SEP – P2.5 HI or P3] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.33 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 448 Table 5.8.18 - MXCL Power (FL > 200) – 170 KIAS / M 0.40 [INERT SEP – P2.5 HI or P3] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.34 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 449 Table 5.8.18 - MXCL Power (FL > 200) – 170 KIAS / M 0.40 [INERT SEP – P2.5 HI or P3] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.35 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 450: Maximum Cruise Power

    Table 5.8.21 P2.5 HI or P3 Table 5.8.22 Table 5.8.23 P2.5 Table 5.8.24 Table 5.8.25 P2.5 HI or P3 Table 5.8.26 Table 5.8.27 PIM TBM 960 - Edition 0 Page 5.8.36 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 451 CAS message is OFF, and messages are OFF. Table 5.8.20 - MXCR Power (FL < 200) Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.37 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 452 Table 5.8.20 - MXCR Power (FL < 200) Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.38 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 453 CAS message is OFF, and messages are OFF. Table 5.8.21 - MXCR Power (FL > 200) Flight level (FL) OAT (° Continue ► PIM TBM 960 - Edition 0 Page 5.8.39 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 454 Table 5.8.21 - MXCR Power (FL > 200) Flight level (FL) OAT (° NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.40 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 455 CAS message is OFF, and message is ON. Table 5.8.22 - MXCR Power (FL < 200) [P2.5 HI or P3] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.41 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 456 Table 5.8.22 - MXCR Power (FL < 200) [P2.5 HI or P3] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.42 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 457 CAS message is OFF, and message is ON. Table 5.8.23 - MXCR Power (FL > 200) [P2.5 HI or P3] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.43 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 458 Table 5.8.23 - MXCR Power (FL > 200) [P2.5 HI or P3] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.44 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 459 CAS message is ON, and messages are OFF. Table 5.8.24 - MXCR Power (FL < 200) [INERT SEP] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.45 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 460 Table 5.8.24 - MXCR Power (FL < 200) [INERT SEP] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.46 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 461 CAS message is ON, and messages are OFF. Table 5.8.25 - MXCR Power (FL > 200) [INERT SEP] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.47 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 462 Table 5.8.25 - MXCR Power (FL > 200) [INERT SEP] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.48 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 463 ON. Table 5.8.26 - MXCR Power (FL < 200) [INERT SEP – P2.5 HI or P3] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.49 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 464 Table 5.8.26 - MXCR Power (FL < 200) [INERT SEP – P2.5 HI or P3] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.50 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 465 ON. Table 5.8.27 - MXCR Power (FL > 200) [INERT SEP – P2.5 HI or P3] Flight Level (FL) (°C) Continue ► PIM TBM 960 - Edition 0 Page 5.8.51 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 466 Table 5.8.27 - MXCR Power (FL > 200) [INERT SEP – P2.5 HI or P3] Flight Level (FL) (°C) NOTE Refer to General conditions at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.8.52 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 467: Takeoff Distances

    7% on hard grass, 10% on short grass, 15% on wet runway, 25% on high grass, 30% on slippery runway. Rotation speed determination: PIM TBM 960 - Edition 0 Page 5.9.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 468 V R (KIAS) Airspeed 6,500 7,000 (lbs) 6,579 7,394 (up to 7,615) Weight 2,984 3,354 (up to 3,454) (kg) 2,800 3,000 3,200 PIM TBM 960 - Edition 0 Page 5.9.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 469: Weight 5,512 Lbs (2,500 Kg)

    15° attitude after 6,000 100% 1,450 2,190 100% 1,510 2,275 rotation. 8,000 100% 1,620 2,415 100% 1,695 2,505 * TRQ at brake release PIM TBM 960 - Edition 0 Page 5.9.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 470: Weight 5,512 Lbs (2,500 Kg) - Inert Sep

    2,205 1,780 2,670 15° attitude after 6,000 1,675 2,530 2,025 3,000 rotation. 8,000 1,960 2,940 2,290 3,385 * TRQ at brake release PIM TBM 960 - Edition 0 Page 5.9.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 471: Weight 6,579 Lbs (2,984 Kg)

    15° attitude after 6,000 100% 2,155 2,920 100% 2,250 3,030 rotation. 8,000 100% 2,410 3,220 100% 2,515 3,340 * TRQ at brake release PIM TBM 960 - Edition 0 Page 5.9.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 472: Weight 6,579 Lbs (2,984 Kg) - Inert Sep

    2,970 2,675 3,640 15° attitude after 6,000 2,505 3,435 3,045 4,115 rotation. 8,000 2,965 4,020 3,490 4,685 * TRQ at brake release PIM TBM 960 - Edition 0 Page 5.9.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 473: Weight 7,394 Lbs (3,354 Kg)

    12.5° attitude after 6,000 100% 2,950 3,920 100% 3,075 4,070 rotation. 8,000 100% 3,285 4,320 100% 3,425 4,485 * TRQ at brake release PIM TBM 960 - Edition 0 Page 5.9.7 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 474: Weight 7,394 Lbs (3,354 Kg) - Inert Sep

    4,090 3,790 5,100 12.5° attitude after 6,000 3,540 4,770 4,360 5,835 rotation. 8,000 4,230 5,645 5,050 6,730 * TRQ at brake release PIM TBM 960 - Edition 0 Page 5.9.8 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 475: Weight 7,615 Lbs (3,454 Kg)

    12.5° attitude after 6,000 100% 3,075 4,080 100% 3,205 4,235 rotation. 8,000 100% 3,455 4,500 100% 3,595 4,670 * TRQ at brake release PIM TBM 960 - Edition 0 Page 5.9.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 476: Weight 7,615 Lbs (3,454 Kg) - Inert Sep

    4,265 3,990 5,335 12.5° attitude after 6,000 3,730 4,985 4,595 6,115 rotation. 8,000 4,455 5,905 5,375 7,070 * TRQ at brake release PIM TBM 960 - Edition 0 Page 5.9.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 477: 5.10 - Climb Performance

    5.10 - Climb Performance This subsection provides performance data for the climb phase, as well as vertical speeds for climb after a go-around and climb with the flaps in the TO position. PIM TBM 960 - Edition 0 Page 5.10.1 Rev. 01...

  • Page 478: Mxcl - Vertical Speeds (Ias = 124 Kias)

    1,960 1,945 1,925 1,910 1,890 1,870 (3,454 kg) 6,000 1,940 1,920 1,900 1,880 1,860 1,840 8,000 1,915 1,895 1,870 1,850 1,830 1,810 PIM TBM 960 - Edition 0 Page 5.10.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 479: Mxcl - Vertical Speeds (Ias = 170 Kias / M 0.40)

    1,690 1,660 1,635 1,605 1,580 1,555 (3,454 kg) 6,000 1,655 1,625 1,595 1,565 1,540 1,510 8,000 1,615 1,585 1,555 1,525 1,495 1,465 PIM TBM 960 - Edition 0 Page 5.10.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 480: Mxcl - Time, Consumption And Climb Distance

    ISA + 20 °C 124 KIAS Table 5.10.4 Table 5.10.5 Table 5.10.6 170 KIAS / M 0.40 Table 5.10.7 Table 5.10.8 Table 5.10.9 PIM TBM 960 - Edition 0 Page 5.10.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 481 15:00 18.4 15:30 18.5 30,000 11:30 13.9 13:45 16.6 16:30 19.8 17:00 20.0 31,000 12:00 14.4 14:30 17.2 17:15 20.6 17:45 20.8 PIM TBM 960 - Edition 0 Page 5.10.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 482 16:00 19.4 16:30 19.6 30,000 12:15 14.6 14:30 17.5 17:45 21.1 18:15 21.3 31,000 12:45 15.1 15:30 18.2 18:45 21.9 19:15 22.2 PIM TBM 960 - Edition 0 Page 5.10.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 483 17:45 21.0 18:30 21.3 30,000 13:30 15.6 16:30 18.9 20:15 23.2 21:15 23.5 31,000 14:15 16.3 17:30 19.8 21:45 24.4 22:45 24.8 PIM TBM 960 - Edition 0 Page 5.10.7 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 484 17:30 21.3 18:00 21.2 30,000 13:45 16.5 16:00 19.3 19:00 22.7 19:15 22.6 31,000 14:15 16.9 16:45 19.9 19:45 23.4 20:00 23.4 PIM TBM 960 - Edition 0 Page 5.10.8 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 485 18:45 22.9 19:15 22.9 30,000 14:45 17.6 17:15 20.8 20:30 24.6 21:00 24.6 31,000 15:15 18.2 18:15 21.5 21:30 25.5 22:00 25.5 PIM TBM 960 - Edition 0 Page 5.10.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 486 22:00 26.1 22:30 26.1 30,000 17:15 19.8 20:30 23.7 25:00 28.5 25:30 28.6 31,000 18:00 20.6 21:45 24.7 26:30 29.8 27:15 30.0 PIM TBM 960 - Edition 0 Page 5.10.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 487: Climb Performance After Go-Around

    1,160 1,140 1,115 1,090 1,065 95 KIAS 6,000 1,190 1,150 1,130 1,100 1,075 1,045 1,020 8,000 1,160 1,120 1,090 1,060 1,030 1,000 PIM TBM 960 - Edition 0 Page 5.10.11 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 488: Climb Performance - Flaps To

    1,825 1,805 1,790 1,775 115 KIAS 6,000 1,865 1,835 1,815 1,800 1,780 1,765 1,745 8,000 1,840 1,810 1,795 1,775 1,755 1,735 1,715 PIM TBM 960 - Edition 0 Page 5.10.12 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 489: Cruise Performance

    Table 5.11.13 Table 5.11.14 Table 5.11.15 P2.5 Table 5.11.20 Table 5.11.21 Table 5.11.22 P2.5 HI or Table 5.11.27 Table 5.11.28 Table 5.11.29 PIM TBM 960 - Edition 0 Page 5.11.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 490 Vp (KTAS) 7,100 lbs 6,300 lbs NOTE P2.5 HI The curves above are plotted for the condition INERT SEP OFF, and messages OFF. PIM TBM 960 - Edition 0 Page 5.11.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 491 21,000 67.0 22,000 66.5 23,000 66.1 24,000 65.8 25,000 65.5 26,000 65.3 27,000 65.1 28,000 65.1 29,000 65.1 30,000 65.3 31,000 65.1 PIM TBM 960 - Edition 0 Page 5.11.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 492 21,000 67.7 22,000 67.2 23,000 66.7 24,000 66.4 25,000 66.1 26,000 65.9 27,000 65.8 28,000 65.7 29,000 64.8 30,000 62.3 31,000 60.1 PIM TBM 960 - Edition 0 Page 5.11.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 493 21,000 68.0 22,000 67.6 23,000 67.1 24,000 66.8 25,000 66.5 26,000 66.3 27,000 66.1 28,000 66.0 29,000 63.9 30,000 61.5 31,000 59.2 PIM TBM 960 - Edition 0 Page 5.11.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 494 21,000 68.3 22,000 67.9 23,000 67.4 24,000 67.1 25,000 66.8 26,000 66.6 27,000 66.5 28,000 64.9 29,000 62.8 30,000 60.7 31,000 58.3 PIM TBM 960 - Edition 0 Page 5.11.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 495 21,000 68.7 22,000 68.2 23,000 67.8 24,000 67.4 25,000 67.2 26,000 66.9 27,000 65.1 28,000 62.8 29,000 60.8 30,000 58.8 31,000 56.5 PIM TBM 960 - Edition 0 Page 5.11.7 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 496 21,000 69.1 22,000 68.6 23,000 68.1 24,000 67.7 25,000 67.4 26,000 65.2 27,000 63.0 28,000 60.8 29,000 58.8 30,000 56.7 31,000 54.5 PIM TBM 960 - Edition 0 Page 5.11.8 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 497 21,000 69.8 22,000 69.3 23,000 67.5 24,000 65.2 25,000 63.2 26,000 61.1 27,000 58.8 28,000 56.9 29,000 54.8 30,000 52.8 31,000 50.8 PIM TBM 960 - Edition 0 Page 5.11.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 498 21,000 68.0 22,000 67.5 23,000 67.0 24,000 66.7 25,000 66.4 26,000 66.2 27,000 66.1 28,000 66.0 29,000 66.0 30,000 65.5 31,000 63.0 PIM TBM 960 - Edition 0 Page 5.11.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 499 21,000 68.7 22,000 68.2 23,000 67.7 24,000 67.4 25,000 67.1 26,000 67.0 27,000 66.8 28,000 65.6 29,000 63.3 30,000 60.8 31,000 58.6 PIM TBM 960 - Edition 0 Page 5.11.11 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 500 21,000 69.0 22,000 68.6 23,000 68.1 24,000 67.7 25,000 67.5 26,000 67.3 27,000 66.7 28,000 64.2 29,000 61.9 30,000 59.6 31,000 57.2 PIM TBM 960 - Edition 0 Page 5.11.12 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 501 21,000 69.4 22,000 69.0 23,000 68.5 24,000 68.1 25,000 67.8 26,000 67.5 27,000 65.2 28,000 62.9 29,000 60.7 30,000 58.5 31,000 56.0 PIM TBM 960 - Edition 0 Page 5.11.13 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 502 21,000 69.8 22,000 69.3 23,000 68.9 24,000 68.5 25,000 67.6 26,000 65.4 27,000 63.2 28,000 60.9 29,000 58.8 30,000 56.5 31,000 54.1 PIM TBM 960 - Edition 0 Page 5.11.14 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 503 21,000 70.2 22,000 69.7 23,000 69.3 24,000 67.6 25,000 65.4 26,000 63.2 27,000 61.0 28,000 58.8 29,000 56.7 30,000 54.5 31,000 52.2 PIM TBM 960 - Edition 0 Page 5.11.15 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 504 21,000 69.8 22,000 69.3 23,000 67.5 24,000 65.2 25,000 63.2 26,000 61.1 27,000 58.8 28,000 56.9 29,000 54.8 30,000 52.8 31,000 50.8 PIM TBM 960 - Edition 0 Page 5.11.16 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 505 21,000 69.6 22,000 67.0 23,000 64.6 24,000 62.0 25,000 59.8 26,000 57.5 27,000 55.4 28,000 53.3 29,000 51.4 30,000 49.4 31,000 47.5 PIM TBM 960 - Edition 0 Page 5.11.17 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 506 21,000 65.7 22,000 63.3 23,000 61.2 24,000 58.9 25,000 56.8 26,000 54.6 27,000 52.8 28,000 50.8 29,000 48.9 30,000 47.0 31,000 45.1 PIM TBM 960 - Edition 0 Page 5.11.18 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 507 21,000 64.3 22,000 62.0 23,000 60.0 24,000 57.8 25,000 55.8 26,000 53.7 27,000 51.9 28,000 50.1 29,000 48.4 30,000 46.5 31,000 44.5 PIM TBM 960 - Edition 0 Page 5.11.19 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 508 21,000 63.0 22,000 60.9 23,000 58.8 24,000 56.9 25,000 54.8 26,000 52.9 27,000 51.1 28,000 49.3 29,000 47.6 30,000 45.8 31,000 44.0 PIM TBM 960 - Edition 0 Page 5.11.20 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 509 21,000 61.6 22,000 59.5 23,000 57.4 24,000 55.5 25,000 53.5 26,000 51.6 27,000 49.8 28,000 48.2 29,000 46.4 30,000 44.6 31,000 42.8 PIM TBM 960 - Edition 0 Page 5.11.21 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 510 21,000 60.1 22,000 58.1 23,000 56.1 24,000 54.1 25,000 52.2 26,000 50.2 27,000 48.5 28,000 46.8 29,000 45.1 30,000 43.4 31,000 41.6 PIM TBM 960 - Edition 0 Page 5.11.22 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 511 21,000 56.6 22,000 54.7 23,000 52.8 24,000 51.0 25,000 49.1 26,000 47.4 27,000 45.7 28,000 44.1 29,000 42.5 30,000 40.8 31,000 39.3 PIM TBM 960 - Edition 0 Page 5.11.23 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 512 21,000 68.5 22,000 66.0 23,000 63.5 24,000 61.0 25,000 58.8 26,000 56.6 27,000 54.5 28,000 52.4 29,000 50.4 30,000 48.5 31,000 46.6 PIM TBM 960 - Edition 0 Page 5.11.24 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 513 21,000 64.1 22,000 61.8 23,000 59.7 24,000 57.4 25,000 55.3 26,000 53.2 27,000 51.3 28,000 49.2 29,000 47.5 30,000 45.5 31,000 43.7 PIM TBM 960 - Edition 0 Page 5.11.25 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 514 21,000 62.7 22,000 60.5 23,000 58.4 24,000 56.2 25,000 54.2 26,000 52.2 27,000 50.3 28,000 48.5 29,000 46.6 30,000 44.8 31,000 42.8 PIM TBM 960 - Edition 0 Page 5.11.26 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 515 21,000 61.5 22,000 59.3 23,000 57.2 24,000 55.2 25,000 53.2 26,000 51.3 27,000 49.4 28,000 47.6 29,000 45.8 30,000 44.2 31,000 42.2 PIM TBM 960 - Edition 0 Page 5.11.27 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 516 21,000 59.8 22,000 57.8 23,000 55.7 24,000 53.7 25,000 51.8 26,000 50.0 27,000 48.2 28,000 46.4 29,000 44.7 30,000 43.0 31,000 41.1 PIM TBM 960 - Edition 0 Page 5.11.28 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 517 21,000 58.1 22,000 56.1 23,000 54.2 24,000 52.2 25,000 50.3 26,000 48.5 27,000 46.7 28,000 45.0 29,000 43.3 30,000 41.6 31,000 39.8 PIM TBM 960 - Edition 0 Page 5.11.29 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 518 21,000 53.9 22,000 51.8 23,000 49.8 24,000 47.9 25,000 46.1 26,000 44.3 27,000 42.5 28,000 40.6 29,000 38.7 30,000 36.9 31,000 35.4 PIM TBM 960 - Edition 0 Page 5.11.30 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 519 ISA + 10 °C ISA + 20 °C P2.5 Table 5.11.35 Table 5.11.36 Table 5.11.37 P2.5 HI or P3 Table 5.11.42 Table 5.11.43 Table 5.11.44 PIM TBM 960 - Edition 0 Page 5.11.31 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 520 Vp (KTAS) 7,100 lbs 6,300 lbs NOTE P2.5 HI The curves above are plotted for the condition INERT SEP OFF, and messages OFF. PIM TBM 960 - Edition 0 Page 5.11.32 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 521 BLEED switch on AUTO, and messages OFF. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.31 - RCR Performance – ISA - 20 °C Airspeeds (kt) Pressure Fuel...
  • Page 522 BLEED switch on AUTO, and messages OFF. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.32 - RCR Performance – ISA - 10 °C Airspeeds (kt) Pressure Fuel...
  • Page 523 BLEED switch on AUTO, and messages OFF. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.33 - RCR Performance – ISA - 5 °C Airspeeds (kt) Pressure Fuel...
  • Page 524 P2.5 HI BLEED switch on AUTO, and messages OFF. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.34 - RCR Performance – ISA Airspeeds (kt) Pressure Fuel 5,500 lbs...
  • Page 525 BLEED switch on AUTO, and messages OFF. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.35 - RCR Performance – ISA + 5 °C Airspeeds (kt) Pressure Fuel...
  • Page 526 BLEED switch on AUTO, and messages OFF. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.36 - RCR Performance – ISA + 10 °C Airspeeds (kt) Pressure Fuel...
  • Page 527 BLEED switch on AUTO, and messages OFF. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.37 - RCR Performance – ISA + 20 °C Airspeeds (kt) Pressure Fuel...
  • Page 528 BLEED switch on AUTO, and message ON. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.38 - RCR Performance – ISA - 20 °C [P2.5 HI or P3] Airspeeds (kt) Pressure Fuel...
  • Page 529 BLEED switch on AUTO, and message ON. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.39 - RCR Performance – ISA - 10 °C [P2.5 HI or P3] Airspeeds (kt) Pressure Fuel...
  • Page 530 BLEED switch on AUTO, and message ON. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.40 - RCR Performance – ISA - 5 °C [P2.5 HI or P3] Airspeeds (kt) Pressure Fuel...
  • Page 531 BLEED switch on AUTO, and message ON. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.41 - RCR Performance – ISA [P2.5 HI or P3] Airspeeds (kt) Pressure Fuel...
  • Page 532 BLEED switch on AUTO, and message ON. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.42 - RCR Performance – ISA + 5 °C [P2.5 HI or P3] Airspeeds (kt) Pressure Fuel...
  • Page 533 BLEED switch on AUTO, and message ON. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.43 - RCR Performance – ISA + 10 °C [P2.5 HI or P3] Airspeeds (kt) Pressure Fuel...
  • Page 534 BLEED switch on AUTO, and message ON. INERT SEP ON Table valid only if CAS message is OFF. Power recommended by Daher for better fuel efficiency. Table 5.11.44 - RCR Performance – ISA + 20 °C [P2.5 HI or P3] Airspeeds (kt) Pressure Fuel...
  • Page 535 ISA + 10 °C ISA + 20 °C P2.5 Table 5.11.50 Table 5.11.51 Table 5.11.52 P2.5 HI or P3 Table 5.11.57 Table 5.11.58 Table 5.11.59 PIM TBM 960 - Edition 0 Page 5.11.47 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 536 Vp (KTAS) 7,100 lbs 6,300 lbs NOTE P2.5 HI The curves above are plotted for the condition INERT SEP OFF, and messages OFF. PIM TBM 960 - Edition 0 Page 5.11.48 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 537 21,000 37.6 22,000 36.6 23,000 36.2 24,000 35.4 25,000 35.1 26,000 35.3 27,000 35.6 28,000 36.0 29,000 35.9 30,000 35.8 31,000 35.1 PIM TBM 960 - Edition 0 Page 5.11.49 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 538 21,000 38.0 22,000 37.5 23,000 37.1 24,000 36.3 25,000 35.4 26,000 35.7 27,000 36.0 28,000 36.4 29,000 36.3 30,000 36.1 31,000 35.5 PIM TBM 960 - Edition 0 Page 5.11.50 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 539 21,000 38.4 22,000 37.5 23,000 37.0 24,000 36.2 25,000 35.9 26,000 35.6 27,000 35.9 28,000 36.3 29,000 36.1 30,000 36.0 31,000 35.4 PIM TBM 960 - Edition 0 Page 5.11.51 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 540 21,000 38.9 22,000 37.9 23,000 37.5 24,000 36.6 25,000 36.3 26,000 36.1 27,000 36.4 28,000 36.8 29,000 36.6 30,000 36.5 31,000 35.9 PIM TBM 960 - Edition 0 Page 5.11.52 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 541 21,000 38.8 22,000 38.3 23,000 37.9 24,000 37.0 25,000 36.2 26,000 36.5 27,000 36.3 28,000 37.2 29,000 36.5 30,000 36.4 31,000 35.7 PIM TBM 960 - Edition 0 Page 5.11.53 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 542 21,000 39.2 22,000 38.8 23,000 37.8 24,000 37.5 25,000 36.6 26,000 36.9 27,000 36.7 28,000 37.7 29,000 37.0 30,000 36.9 31,000 36.2 PIM TBM 960 - Edition 0 Page 5.11.54 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 543 21,000 40.1 22,000 39.1 23,000 38.7 24,000 37.8 25,000 37.0 26,000 37.3 27,000 37.6 28,000 38.1 29,000 37.4 30,000 37.3 31,000 36.6 PIM TBM 960 - Edition 0 Page 5.11.55 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 544 21,000 38.6 22,000 37.6 23,000 37.1 24,000 36.3 25,000 36.0 26,000 36.2 27,000 36.5 28,000 36.9 29,000 36.8 30,000 36.7 31,000 36.0 PIM TBM 960 - Edition 0 Page 5.11.56 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 545 21,000 39.0 22,000 38.5 23,000 38.1 24,000 37.2 25,000 36.4 26,000 36.7 27,000 37.0 28,000 37.4 29,000 37.2 30,000 37.1 31,000 36.4 PIM TBM 960 - Edition 0 Page 5.11.57 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 546 21,000 39.5 22,000 38.5 23,000 38.1 24,000 37.2 25,000 36.9 26,000 36.6 27,000 36.9 28,000 37.3 29,000 37.1 30,000 37.1 31,000 36.4 PIM TBM 960 - Edition 0 Page 5.11.58 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 547 21,000 39.9 22,000 39.0 23,000 38.5 24,000 37.6 25,000 37.3 26,000 37.1 27,000 37.4 28,000 37.8 29,000 37.7 30,000 37.6 31,000 36.9 PIM TBM 960 - Edition 0 Page 5.11.59 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 548 21,000 39.9 22,000 39.4 23,000 39.0 24,000 38.1 25,000 37.2 26,000 37.5 27,000 37.3 28,000 38.3 29,000 37.6 30,000 37.5 31,000 36.8 PIM TBM 960 - Edition 0 Page 5.11.60 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 549 21,000 40.4 22,000 39.9 23,000 38.9 24,000 38.5 25,000 37.7 26,000 38.0 27,000 37.8 28,000 38.8 29,000 38.1 30,000 38.0 31,000 37.3 PIM TBM 960 - Edition 0 Page 5.11.61 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 550 21,000 41.3 22,000 40.3 23,000 39.9 24,000 38.9 25,000 38.1 26,000 38.4 27,000 38.8 28,000 39.2 29,000 38.5 30,000 38.4 31,000 37.8 PIM TBM 960 - Edition 0 Page 5.11.62 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 551 06:40 05:00 04:00 8,000 05:20 04:00 03:10 6,000 04:00 03:00 02:25 4,000 02:40 02:00 01:35 2,000 01:20 01:00 00:50 00:00 00:00 00:00 PIM TBM 960 - Edition 0 Page 5.12.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 552 Section 5 Performance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 5.12.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 553 10 min 30 min 10 min 30 min (ft) 23.5 24.1 5,000 20.8 21.4 10,000 18.7 19.4 15,000 17.3 18.1 20,000 15.9 16.7 PIM TBM 960 - Edition 0 Page 5.13.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 554 Section 5 Performance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 5.13.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 555 Increase distances by: 7% on hard grass, 10% on short grass, 15% on wet runway, 25% on high grass, 30% on slippery runway. PIM TBM 960 - Edition 0 Page 5.14.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 556 2,590 3,280 2,725 3,410 2,855 3,570 2,920 3,640 CAUTION Refer to General notes and correction factors at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.14.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 557 1,705 2,790 1,770 2,885 1,835 2,985 1,900 3,085 CAUTION Refer to General notes and correction factors at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.14.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 558 1,445 2,790 1,510 2,885 1,560 2,985 1,610 3,085 CAUTION Refer to General notes and correction factors at the beginning of this subsection. PIM TBM 960 - Edition 0 Page 5.14.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 559 Weight and Balance Examples (m, kg) ......... 6.4.11 Weight and Balance Examples (in, lbs) ........ 6.4.14 Determining Empty Airplane Characteristics ......6.4.16 - List of Equipment ............... 6.5.1 PIM TBM 960 - Edition 0 Page 6.0.1 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 560 Section 6 Weight and Balance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 6.0.2 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 561: General

    Equipment. The list of specific optional equipment installed on the airplane as delivered from the factory can be found in the records carried in the airplane. PIM TBM 960 - Edition 0 Page 6.1.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 562 Section 6 Weight and Balance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 6.1.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 563 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. PIM TBM 960 - Edition 0 Page 6.2.1 Rev. 00...
  • Page 564 Section 6 Weight and Balance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 6.2.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 565 Frame C14 – see Figure 7.2.2. Refer to Paragraph Baggage Limits in Subsection 2.7. for limitations. PIM TBM 960 - Edition 0 Page 6.3.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 566 When using the large net, distribute the weight in each zone, delineated by the step up in the floor, according to the zone limits. PIM TBM 960 - Edition 0 Page 6.3.2 Rev. 00...
  • Page 567 FWD compartment, then, if required, load the AFT compartment. Compute and check the weight and balance diagram to ensure the airplane is within the allowable limits. PIM TBM 960 - Edition 0 Page 6.3.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 568 Section 6 Weight and Balance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 6.3.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 569: Utilization Of Weight And Balance Graphs

    Compute the zero fuel weight arm and C.G. (MAC %) (5c) using the given formulas. PIM TBM 960 - Edition 0 Page 6.4.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 570 19. Check that all points are within the weight and balance limits and check that they are vertically aligned. 20. Record these data in your navigation log. PIM TBM 960 - Edition 0 Page 6.4.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 571: Airplane Loading Form (M, Kg)

    Trip fuel (kg) (14a) 4.820 (14b) Landing weight (< 3,225 kg) (15a) (17) (15b) (17c) * Seat weights include the seat heating system PIM TBM 960 - Edition 0 Page 6.4.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 572: Example Of Airplane Weight And Balance Report

    Small net Large net Example of Airplane Weight and Balance Report NOTE The airplane's original report shall be kept with the airplane's POH. PIM TBM 960 - Edition 0 Page 6.4.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 573 3 - Values not taken into account if the oil tank was full when the airplane was weighed. DATE : INSPECTION VISA : NOTE The airplane's original report shall be kept with the airplane's POH. PIM TBM 960 - Edition 0 Page 6.4.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 574 3 - Values not taken into account if the oil tank was full when the airplane was weighed. DATE : INSPECTION VISA : PIM TBM 960 - Edition 0 Page 6.4.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 575: Weight And Balance Form And Diagram (M, Kg)

    Takeoff weight (< 3,454 kg) Trip fuel (kg) 4.820 Landing weight (< 3,225 kg) * Seat weights include the seat heating system PIM TBM 960 - Edition 0 Page 6.4.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 576 Max Landing Weight (MLW) Max Zero Fuel Weight (MZFW) (MAC %) 14 16 18 20 22 24 26 28 30 32 34 36 PIM TBM 960 - Edition 0 Page 6.4.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 577: Weight And Balance Form And Diagram (In, Lbs)

    Takeoff weight (< 7,615 lbs) Trip fuel (lbs) 189.8 Landing weight (< 7,110 lbs) * Seat weights include the seat heating system PIM TBM 960 - Edition 0 Page 6.4.9 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 578 Max Landing Weight (MLW) Max Zero Fuel Weight (MZFW) (MAC %) 14 16 18 20 22 24 26 28 30 32 34 36 PIM TBM 960 - Edition 0 Page 6.4.10 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 579: Weight And Balance Examples (M, Kg)

    Table 6.4.4 - Weight and Balance Form Example (m, kg) Weight Moment C.G. Item (kg) (m.kg) (MAC %) Empty weight (kg) 2,170 4.727 10,258 22.2 Continue ► PIM TBM 960 - Edition 0 Page 6.4.11 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 580 - 600 4.820 - 2,892 Landing weight (< 3,225 kg) 2,830 4.914 13,908 34.6 * Seat weights include the seat heating system PIM TBM 960 - Edition 0 Page 6.4.12 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 581 Max Zero Fuel Weight (MZFW) Zero Fuel Weight Empty Weight (MAC %) 14 16 18 20 22 24 26 28 30 32 34 36 PIM TBM 960 - Edition 0 Page 6.4.13 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 582: Weight And Balance Examples (In, Lbs)

    - 50 lbs Trip fuel - 1,450 lbs Arm (in) − 172.93 Moment = Weight × Arm CG (MAC %) = × 100 59.45 PIM TBM 960 - Edition 0 Page 6.4.14 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 583 - 1,450 189.8 - 275,210 Landing weight (< 7,110 lbs) 6,064 192.9 1,169,507 33.6 * Seat weights include the seat heating system PIM TBM 960 - Edition 0 Page 6.4.15 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 584: Determining Empty Airplane Characteristics

    Empty airplane characteristics (weight and balance) may vary in relation to those indicated on the weighing form based on the installed optional equipment and installed seats. PIM TBM 960 - Edition 0 Page 6.4.16 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 585 The arm is expressed in inches with relation to the reference datum. FWD baggage compartment: 128.0 in (3.250 m) Baggage compartment in pressurized cabin: 303.0 in (7.695 m) Fuel: 189.8 in (4.820 m) PIM TBM 960 - Edition 0 Page 6.4.17 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 586 (4.400) (5.175) - R.H. low + top pilot case support 9.70 203.74 (4.400) (5.175) 0207-00 Carpet 35.27 211.42 (16.000) (5.370) Continue ► PIM TBM 960 - Edition 0 Page 6.4.18 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 587 - Partition net at Frame 14 (between the cabin 3.64 289.53 and the baggage compartment) (1.650) (7.354) T700B2590001, of which: . Partition net 1.70 289.53 (0.77) (7.354) PIM TBM 960 - Edition 0 Page 6.4.19 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 588 Section 6 Weight and Balance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 6.4.20 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 589: List Of Equipment

    A separate list of equipment items installed at the factory in your specific airplane is provided in the records carried in the airplane. PIM TBM 960 - Edition 0 Page 6.5.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 590 Section 6 Weight and Balance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 6.5.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 591 Landing Gear Position Indicator ........... 7.5.2 Safety ................... 7.5.6 Ground Maneuvers ............... 7.5.9 Brake System ............... 7.5.12 Parking Brake ............... 7.5.12 - Powerplant ................7.6.1 PIM TBM 960 - Edition 0 Page 7.0.1 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 592 Fuel Gauging Installation ............7.8.10 Fuel System Monitoring ............7.8.10 Fuel System Draining and Clogging Indicator ...... 7.8.11 - Electrical System ............... 7.9.1 PIM TBM 960 - Edition 0 Page 7.0.2 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 593 Heating of Pitots and Stall Warning Sensor ......7.14.5 Turbine Air Inlet Protection ........... 7.14.5 7.15 - Miscellaneous Equipment ............7.15.1 Stall Warning System ............7.15.1 PIM TBM 960 - Edition 0 Page 7.0.3 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 594 Data Collection and Transmission Unit (DCTU) ....7.15.8 Garmin Integrated Flight Deck (GIFD) Approaches ..... 7.15.9 HomeSafe Emergency Function ........... 7.15.14 Optional Equipment .............. 7.15.17 PIM TBM 960 - Edition 0 Page 7.0.4 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 595: General

    Details of other optional systems and equipment are presented in Section 9: Supplements of the POH. PIM TBM 960 - Edition 0 Page 7.1.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 596 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.1.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 597: Airframe

    An optional pilot door located forward of the cabin on the left side allows access to the cockpit by means of folding stairs. The aft cabin section is a baggage compartment. PIM TBM 960 - Edition 0 Page 7.2.1 Rev. 00...
  • Page 598 Section 7 Description Pilot's Information Manual Figure 7.2.1 - Cabin Arrangement – 6-seat Accommodation PIM TBM 960 - Edition 0 Page 7.2.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 599 Section 7 Description Pilot's Information Manual Figure 7.2.2 - Cabin Arrangement – 4-seat Accommodation with Large Securing PIM TBM 960 - Edition 0 Page 7.2.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 600 Section 7 Description Pilot's Information Manual Figure 7.2.3 - Cabin Arrangement – 4-seat Accommodation with Small Securing PIM TBM 960 - Edition 0 Page 7.2.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 601: Wings

    (UP - TO - LDG). For each control position, a deflection angle is defined (0°, 10°, 34°). A monitoring device interrupts flaps movement as soon as a deflection dissymmetry is detected. PIM TBM 960 - Edition 0 Page 7.2.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 602 Pilot's Information Manual Key to Figure 7.2.4 1) Geared motor 2) Internal actuator 3) Intermediate bearings 4) Wing flap 5) External actuator 6) Rods PIM TBM 960 - Edition 0 Page 7.2.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 603 Section 7 Description Pilot's Information Manual Figure 7.2.4 - Wing Flaps (1/2) PIM TBM 960 - Edition 0 Page 7.2.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 604 Section 7 Description Pilot's Information Manual Key to Figure 7.2.5 1) Control selector PIM TBM 960 - Edition 0 Page 7.2.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 605 Section 7 Description Pilot's Information Manual Figure 7.2.5 - Wing Flaps (2/2) PIM TBM 960 - Edition 0 Page 7.2.9 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 606: Empennages

    The empennage leading edge is equipped with a deicing system. PIM TBM 960 - Edition 0 Page 7.2.10 Rev. 00...

  • Page 607: Accomodations

    [two primary flight displays (PFD) and one multi-function display (MFD)] – refer to the Garmin Pilot's Guide for detailed description. Apart from the Garmin flight deck system, equipment listed below complete the instrument panel. PIM TBM 960 - Edition 0 Page 7.3.1 Rev. 01...
  • Page 608 General Alarms Warning Lights and CAS Messages WARNING CAUTION ADVISORY messages appear in the CAS window to alert crew about monitored systems discrepancies. As a message appears, a PIM TBM 960 - Edition 0 Page 7.3.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 609 800 ft AGL "Check gear / Check gear" gear up and extended flaps below 800 ft AGL Continue ► PIM TBM 960 - Edition 0 Page 7.3.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 610 It is integrated in the ceiling upholstery panel. The emergency lighting rheostat is electrically supplied by BATT BUS bar and protected by PANEL EMER circuit breaker. PIM TBM 960 - Edition 0 Page 7.3.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 611 LEFT INSTRUMENT RIGHT INSTRUMENT PANEL PANEL See figure 7.3.3 See figure 7.3.5 BREAKERS PANEL See figure 7.3.7 BOTTOM PEDESTAL CONSOLE See figure 7.3.6 PIM TBM 960 - Edition 0 Page 7.3.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 612 10) INT LIGHTS internal lighting switches – see Figure 7.9.8 11) EXT LIGHTS external lighting switches – see Figure 7.9.7 12) TEST pushbutton 13) Left-side cockpit floodlight PIM TBM 960 - Edition 0 Page 7.3.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 613 Section 7 Description Pilot's Information Manual Figure 7.3.2 - Upper Panel and Cockpit Overhead Panel PIM TBM 960 - Edition 0 Page 7.3.7 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 614 Figure 7.11.1 22) COM 2 (Standby / Active) 23) Stormscope clear 24) Transponder Ident sequence 25) Chronometer management 26) Left station rudder pedals PIM TBM 960 - Edition 0 Page 7.3.8 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 615 Section 7 Description Pilot's Information Manual Figure 7.3.3 - Left Instrument Panel (Typical arrangement) PIM TBM 960 - Edition 0 Page 7.3.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 616 4) LVL pushbutton 5) HomeSafe activation button 6) Registration 7) MFD 8) Touchscreen controllers 9) ECS and PRESSURIZATION panels – see Figure 7.10.4 PIM TBM 960 - Edition 0 Page 7.3.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 617 Section 7 Description Pilot's Information Manual Figure 7.3.4 - Central Instrument Panel (Typical arrangement) PIM TBM 960 - Edition 0 Page 7.3.11 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 618 15) Cabin emergency air control (EMERGENCY RAM AIR control knob) 16) Static source selector 17) Chronometer management 18) Transponder Ident sequence 19) Stormscope clear 20) COM 2 (Standby / active) PIM TBM 960 - Edition 0 Page 7.3.12 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 619 Section 7 Description Pilot's Information Manual Figure 7.3.5 - Right Instrument Panel (Typical arrangement) PIM TBM 960 - Edition 0 Page 7.3.13 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 620 4) Manual FUEL TANK SELECTOR – see Figure 7.8.3 5) Roll trim tab control 6) Pitch trim tab control 7) GND FEATHER switch PIM TBM 960 - Edition 0 Page 7.3.14 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 621 Section 7 Description Pilot's Information Manual Figure 7.3.6 - Pedestal Console (Typical arrangement) PIM TBM 960 - Edition 0 Page 7.3.15 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 622 Section 7 Description Pilot's Information Manual Figure 7.3.7 - Circuit Breakers Panel PIM TBM 960 - Edition 0 Page 7.3.16 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 623 Section 7 Description Pilot's Information Manual Figure 7.3.8 - General Alarms Warning Lights MASTER MASTER WARNING CAUTION PIM TBM 960 - Edition 0 Page 7.3.17 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 624: Homesafe Interface Panel

    CAS window as long as cabin access door and pilot access door, if installed, are not correctly locked. CAUTION Before opening access door, make sure door deflection area is clear. PIM TBM 960 - Edition 0 Page 7.3.18 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 625 In case of geared motor failure, the door can be manually tilted downwards by pulling sufficiently to override action of compensating struts. PIM TBM 960 - Edition 0 Page 7.3.19 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 626 Section 7 Description Pilot's Information Manual Figure 7.3.9 - Cabin Access Door PIM TBM 960 - Edition 0 Page 7.3.20 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 627 To close the door from outside the airplane, push the door until it aligns with fuselage and lock it by moving outside handle upwards, then fold handle in its recess. PIM TBM 960 - Edition 0 Page 7.3.21 Rev. 01...
  • Page 628 CAS window as long as FWD compartment door is not locked. Windows Windows do not open. The windshield consists of two parts electrically deiced. PIM TBM 960 - Edition 0 Page 7.3.22 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 629 Section 7 Description Pilot's Information Manual Figure 7.3.10 - Cockpit Access Door (pilot door) PIM TBM 960 - Edition 0 Page 7.3.23 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 630 Taxiing and flying with thief-proof safety pin installed is forbidden. To open the emergency exit, pull one of the two handles and tilt the emergency exit from top to bottom towards inside of airplane. PIM TBM 960 - Edition 0 Page 7.3.24 Rev. 01...
  • Page 631 Section 7 Description Pilot's Information Manual Figure 7.3.11 - Emergency Exit PIM TBM 960 - Edition 0 Page 7.3.25 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 632: Seats, Belts And Harnesses

    When not powered, the dimmable windows are 50% shaded. Figure 7.3.12 - Dimmable Windows Control CABIN Seats, Belts and Harnesses Heated Seats Figure 7.3.13. PIM TBM 960 - Edition 0 Page 7.3.26 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 633 The seats heaters control box and relays located under the floor panel. Each seat is equipped with a power supply wire with a connector. A clip attaches the connector to the seat to prevent damage during seat operation or seat storage. PIM TBM 960 - Edition 0 Page 7.3.27 Rev. 01...
  • Page 634 Key to Figure 7.3.13 1) SEATS HTRS MASTER switch 2) Backrest surface heating 3) Seat surface heating 4) HI/OFF/LOW three-position switch 5) Tactile marks PIM TBM 960 - Edition 0 Page 7.3.28 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 635 Section 7 Description Pilot's Information Manual Figure 7.3.13 - Heated Seat DISPLAY BACKUP SEATS HTRS MASTER ALTERNATE LOCATION PIM TBM 960 - Edition 0 Page 7.3.29 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 636 The seat heater can be damaged by fluids spilt on the seat. Never switch the seat heater on when it is wet. Cockpit Seats Figure 7.3.14. PIM TBM 960 - Edition 0 Page 7.3.30 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 637 The seat back angle is adjusted by pulling up side handle. >> All PIM TBM 960 - Edition 0 Page 7.3.31 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 638 (Item 13) to tilt left-side seat assembly forwards. If necessary, pull forwards the backrest of rear bench right- side seat. PIM TBM 960 - Edition 0 Page 7.3.32 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 639 Section 7 Description Pilot's Information Manual Figure 7.3.14 - Seats – 6-Seat Accommodation PIM TBM 960 - Edition 0 Page 7.3.33 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 640 5) Front seat(s) longitudinal shift control 6) Front seat(s) height control 7) Front seat(s) backrest tilt control 8) Intermediate seat(s) backrest tilt control PIM TBM 960 - Edition 0 Page 7.3.34 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 641 Section 7 Description Pilot's Information Manual Figure 7.3.15 - Seats – 4-Seat Accommodation PIM TBM 960 - Edition 0 Page 7.3.35 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 642 Facing installed 5 *(1) YES *(1) 1 or 0 *(1) 1 or 0 1 or 0 *(1) Centered on the fuselage axis PIM TBM 960 - Edition 0 Page 7.3.36 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 643 (1) This configuration accepts small net or large net (2) In this position, the seats heaters system cannot be connected to the rear seat. Each cross indicates that a seat is installed at the corresponding location number. PIM TBM 960 - Edition 0 Page 7.3.37 Rev. 01...
  • Page 644 The central buckle must be positioned so that the belt straps remain at hip level (just below the center of gravity) to prevent the body from slipping under the belts. PIM TBM 960 - Edition 0 Page 7.3.38 Rev. 01...
  • Page 645 Central buckle Each passenger seat is equipped with a three-point restraint system consisting of an adjustable lap belt and an inertia reel-type shoulder harness. PIM TBM 960 - Edition 0 Page 7.3.39 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 646 Section 7 Description Pilot's Information Manual Figure 7.3.17 - Front and Rear Seat Belts with Movable Straps and Harnesses PIM TBM 960 - Edition 0 Page 7.3.40 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 647 Adjust the belt straps, Fasten and adjust the harnesses. Figure 7.3.18 - Fastening the Seat Belts on Front Seats PIM TBM 960 - Edition 0 Page 7.3.41 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 648: Baggage Compartments

    Frame C11 and Frame C13bis – see Figure 7.2.3. PIM TBM 960 - Edition 0 Page 7.3.42 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 649 Prohibited area Authorized anchoring area Authorized anchoring points are identified with green self-adhesive labels affixed to the inside of the seat rail. PIM TBM 960 - Edition 0 Page 7.3.43 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 650: Use Of Cargo Nets

    50%, seam of tensioning straps attached on the rails damaged on less than 30% of its length: reduce maximum load by 50%, PIM TBM 960 - Edition 0 Page 7.3.44 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 651 3.9 in (100 mm): do not carry small objects which dimensions are smaller than 4.9 x 4.9 x 4.9 in (125 x 125 x 125 mm). PIM TBM 960 - Edition 0 Page 7.3.45 Rev.
  • Page 652 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.3.46 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 653: Flight Controls

    The trim tab is connected through two links to an electric actuator located in the aileron. A trim switch located on pedestal controls the roll trim tab maneuver. Roll trim tab electrical circuit is protected by the AIL TRIM breaker. PIM TBM 960 - Edition 0 Page 7.4.1 Rev. 00...
  • Page 654 1) Pedestal assembly 2) Control wheels 3) Fuselage roll lever 4) Spoiler 5) Aileron 6) Aileron control in wing 7) Spoiler control PIM TBM 960 - Edition 0 Page 7.4.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 655 Section 7 Description Pilot's Information Manual Figure 7.4.1 - Roll (1/2) PIM TBM 960 - Edition 0 Page 7.4.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 656 Key to Figure 7.4.2 1) Pedestal assembly 2) Control wheels 3) Fuselage roll lever 4) Aileron 5) Aileron control in wing 6) Spoiler control PIM TBM 960 - Edition 0 Page 7.4.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 657 Section 7 Description Pilot's Information Manual Figure 7.4.2 - Roll (2/2) PIM TBM 960 - Edition 0 Page 7.4.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 658 Pilot's Information Manual Key to Figure 7.4.3 1) Roll trim tab 2) Aileron 3) Adjustable rods 4) Actuator 5) Trim tab control wiring PIM TBM 960 - Edition 0 Page 7.4.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 659 Section 7 Description Pilot's Information Manual Figure 7.4.3 - Roll Trim (1/2) PIM TBM 960 - Edition 0 Page 7.4.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 660 Pilot's Information Manual Key to Figure 7.4.4 1) Trim switch on pedestal console 2) Roll trim tab 3) Adjustable rods 4) Actuator PIM TBM 960 - Edition 0 Page 7.4.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 661 Section 7 Description Pilot's Information Manual Figure 7.4.4 - Roll Trim (2/2) PIM TBM 960 - Edition 0 Page 7.4.9 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 662: Elevator

    The electrical circuit for pitch trims is protected by the AP SERVOS breaker. Manual control wheel is installed vertically on left side of pedestal console. PIM TBM 960 - Edition 0 Page 7.4.10 Rev. 00...
  • Page 663 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.4.11 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 664 3) Lever assembly, fuselage rear part 4) Elevator bellcrank 5) Rod with presseal connection 6) Lever assembly under floor 7) Pedestal assembly 8) Stick shaker PIM TBM 960 - Edition 0 Page 7.4.12 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 665 Section 7 Description Pilot's Information Manual Figure 7.4.5 - Elevator (1/2) PIM TBM 960 - Edition 0 Page 7.4.13 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 666 Key to Figure 7.4.6 1) Control wheel assembly 2) Elevators 3) Lever assembly, fuselage rear part 4) Elevator bellcrank 5) Pedestal assembly 6) Actuator PIM TBM 960 - Edition 0 Page 7.4.14 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 667 Section 7 Description Pilot's Information Manual Figure 7.4.6 - Elevator (2/2) PIM TBM 960 - Edition 0 Page 7.4.15 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 668 Section 7 Description Pilot's Information Manual Key to Figure 7.4.7 1) Cables 2) Pulleys 3) Pitch trim tabs 4) Actuating rods 5) Actuator PIM TBM 960 - Edition 0 Page 7.4.16 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 669 Section 7 Description Pilot's Information Manual Figure 7.4.7 - Pitch Trim (1/2) PIM TBM 960 - Edition 0 Page 7.4.17 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 670 Pilot's Information Manual Key to Figure 7.4.8 1) Pitch trim manual control wheel 2) Electric pitch trim control 3) Actuating rods 4) Actuator PIM TBM 960 - Edition 0 Page 7.4.18 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 671 Section 7 Description Pilot's Information Manual Figure 7.4.8 - Pitch Trim (2/2) PIM TBM 960 - Edition 0 Page 7.4.19 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 672: Rudder

    Trim tab is linked by two rods to an electric actuator attached to rudder. It is controlled by rudder trim switch (Y L / Y R) located on pilot control wheel. Electrical circuit of rudder trim tab is protected by RUD TRIM breaker. PIM TBM 960 - Edition 0 Page 7.4.20 Rev. 00...
  • Page 673 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.4.21 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 674 1) Roll / rudder combination bellcrank installation 2) Rudder pedals assembly 3) Control cables 4) Pulleys 5) Rudder lever assembly 6) Rod 7) Rudder PIM TBM 960 - Edition 0 Page 7.4.22 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 675 Section 7 Description Pilot's Information Manual Figure 7.4.9 - Rudder (1/2) PIM TBM 960 - Edition 0 Page 7.4.23 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 676 1) Roll / rudder combination bellcrank installation 2) Rudder pedals assembly 3) Rudder 4) Rudder lever assembly 5) Nose gear steering rod 6) Rod PIM TBM 960 - Edition 0 Page 7.4.24 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 677 Section 7 Description Pilot's Information Manual Figure 7.4.10 - Rudder (2/2) PIM TBM 960 - Edition 0 Page 7.4.25 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 678 Figure 7.4.11 - Rudder Trim (1/2) 1) Trim switch on control wheel 2) Actuator 3) Rudder trim tab 4) Rods 5) Rudder trim control wiring PIM TBM 960 - Edition 0 Page 7.4.26 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 679 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.4.27 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 680 Description Pilot's Information Manual Key to Figure 7.4.12 1) Trim switch on control wheel 2) Actuator 3) Rudder trim tab 4) Rods PIM TBM 960 - Edition 0 Page 7.4.28 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 681 Section 7 Description Pilot's Information Manual Figure 7.4.12 - Rudder Trim (2/2) PIM TBM 960 - Edition 0 Page 7.4.29 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 682 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.4.30 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 683: Landing Gear

    At the end of this lever is a knob that represents a wheel. Raising and lowering of the landing gear is performed by pulling on the lever and moving it to either the UP (retracted) or DN (extended) position. PIM TBM 960 - Edition 0 Page 7.5.1 Rev. 01...

  • Page 684: Landing Gear Position Indicator

    16 hertz. Pressing the LIGHT TEST pushbutton enables the testing of all LANDING GEAR panel lights, which will flash at a rate of one hertz. PIM TBM 960 - Edition 0 Page 7.5.2 Rev. 01...
  • Page 685 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.5.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 686 1) Green indicator light 2) Red warning light 3) LANDING GEAR lever 4) CHECK DOWN pushbutton 5) LIGHT TEST pushbutton 6) Amber light PIM TBM 960 - Edition 0 Page 7.5.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 687 Section 7 Description Pilot's Information Manual Figure 7.5.1 - Control Panel and Landing Gear Indicating LANDING GEAR GEAR UNSAFE CHECK DOWN LIGHT TEST PIM TBM 960 - Edition 0 Page 7.5.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 688: Safety

    This control is accessible by removing the floor panel located aft of the pedestal. After the bypass selector is closed, the hand pump operation sends hydraulic fluid directly into the landing gear actuators. PIM TBM 960 - Edition 0 Page 7.5.6 Rev. 01...
  • Page 689 110 cycles of the hand pump. During the final pumping cycles, increased pressure must be felt while actuating the hand pump to confirm its proper operation in extending and locking the landing gear. PIM TBM 960 - Edition 0 Page 7.5.7 Rev. 01...
  • Page 690 Section 7 Description Pilot's Information Manual Figure 7.5.2 - Emergency Landing Gear Extension Control Emergency pump handle Bypass selector PIM TBM 960 - Edition 0 Page 7.5.8 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 691: Ground Maneuvers

    – see Figure 7.5.4. NOTE As tight turns result in untimely tire wear, turns should be made using the largest possible turning radius. PIM TBM 960 - Edition 0 Page 7.5.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 692 Figure 7.5.3 - Minimum Turn Diameter [Full travel of rudder pedals without differential braking applied] 24,00 m 78.74 ft 7,88 m 25.85 ft 19° 4,00 m 13.12 ft PIM TBM 960 - Edition 0 Page 7.5.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 693 Figure 7.5.4 - Minimum Turn Diameter [Full travel of rudder pedals with differential braking applied] 20,50 m 67.26 ft 6,13 m 20.11 ft 28° 2,55 m 8.37 ft PIM TBM 960 - Edition 0 Page 7.5.11 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 694: Brake System

    To release the parking brake, press on the rudder pedals' toe brake and set the PARK BRAKE control knob to OFF. Check that disappears at the same time. PIM TBM 960 - Edition 0 Page 7.5.12 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 695 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.5.13 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 696 6) PARK BRAKE control knob 7) PARK BRAKE valve 8) Drain 9) Pilot's position master cylinders 10) Left-side brake assembly 11) Right-side brake assembly PIM TBM 960 - Edition 0 Page 7.5.14 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 697 Section 7 Description Pilot's Information Manual Figure 7.5.5 - Brake System Supply hose Flexible pressure pipe Rigid pressure pipe Instrument panel PIM TBM 960 - Edition 0 Page 7.5.15 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 698 Section 7 Description Pilot's Information Manual Figure 7.5.6 - Brake Bystem – Park Brake Controls PARK BRAKE PIM TBM 960 - Edition 0 Page 7.5.16 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 699: Powerplant

    Hot gases are evacuated through two exhaust stubs located laterally on both sides forward of engine cowling. PIM TBM 960 - Edition 0 Page 7.6.1 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 700 11) Axial compressors 12) Centrifugal impeller 13) Combustion chamber 14) Gas generator turbine 15) Reduction gearbox 16) Propeller shaft 17) Beta ring PIM TBM 960 - Edition 0 Page 7.6.2 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 701 Section 7 Description Pilot's Information Manual Figure 7.6.1 - Powerplant PIM TBM 960 - Edition 0 Page 7.6.3 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 702: Full Authority Digital Engine Control (Fadec)

    Channel A is supplied by the ESS BUS 1 bar and protected by the FADEC CH.A breaker, Channel B is supplied by the BUS 2 bar and protected by the FADEC CH.B breaker. PIM TBM 960 - Edition 0 Page 7.6.4 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 703 Np exceedance during engine operation by reducing the fuel flow and, if necessary, by feathering the propeller, uncommanded propeller reverse in flight, by feathering the propeller, PIM TBM 960 - Edition 0 Page 7.6.5 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 704 The control system has experienced a FADEC FADEC FAULT system componant fault that has been automatically accommodated to provide continued operation without operational impact. Continue ► PIM TBM 960 - Edition 0 Page 7.6.6 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 705 THROTTLE position. Indicates that the propeller is feathered and the FEATHER engine set to idle after a FADEC system componant failure. Continue ► PIM TBM 960 - Edition 0 Page 7.6.7 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 706: Engine Control Lever

    IDLE position of the THROTTLE can lead to two different engine settings: in flight, flight IDLE setting with dedicated Ng and propeller pitch values, PIM TBM 960 - Edition 0 Page 7.6.8 Rev. 02...
  • Page 707 Np, modulated depending on the THROTTLE position in the REV range. Return to IDLE position is performed by pushing the THROTTLE forward. PIM TBM 960 - Edition 0 Page 7.6.9 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 708 Pilot's Information Manual Figure 7.6.3 - Engine Control Lever 1) THROTTLE 2) Trigger for reverse 3) TO/GA pushbutton 4) AT DISC pushbutton PIM TBM 960 - Edition 0 Page 7.6.10 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 709 When the Autothrottle function is activated, the THROTTLE movements are defined by the Autothrottle servomotor. The autothrottle controls are integrated within the AFCS control unit located above the MFD. PIM TBM 960 - Edition 0 Page 7.6.11 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 710 Section 7 Description Pilot's Information Manual Figure 7.6.4 - Autothrottle Assembly 1) Pedestal console 2) Gears 3) Servomotor PIM TBM 960 - Edition 0 Page 7.6.12 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 711: Engine Monitoring

    (i.e. normal, amber or red): When the engine is OFF, during engine start and engine shutdown, the primarily displayed indication is ITT, PIM TBM 960 - Edition 0 Page 7.6.13 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 712 1925 1925 °C °C °C Figure 7.6.6 - Priority Indication = NG PROP PROP °C °C 1925 1925 106.3 104.1 °C °C PIM TBM 960 - Edition 0 Page 7.6.14 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 713 When engine is running: ITT > 850 °C for less than 20 seconds. PROP RPM ≥ 2,100 RPM, or PROP PROP RPM > 2,030 RPM for more than 20 seconds. Continue ► PIM TBM 960 - Edition 0 Page 7.6.15 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 714: Engine Lubrication

    A cooler located on the left side in the engine compartment maintains oil temperature within the limits. Oil flow into the cooler is metered by a thermostatic valve. Engine oil also supplies the PCU and the engine torquemeter. PIM TBM 960 - Edition 0 Page 7.6.16 Rev. 02...

  • Page 715: Engine Operations

    CAS window as long as the spark igniter plugs are supplied. The table hereafter gives the status light colors corresponding to the state of the system. PIM TBM 960 - Edition 0 Page 7.6.17 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 716 – refer to Paragraph Dry Motoring The FADEC has also the capability to interrupt the engine start sequence if: PIM TBM 960 - Edition 0 Page 7.6.18 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 717 GTC sub-menu ("MFD Home," "Aircraft Systems," "Engine Crank") when the ENGINE MODE switch is set to OFF. Then, the pilot manually operates the starter by setting and maintaining the STARTER switch to PIM TBM 960 - Edition 0 Page 7.6.19 Rev. 02...
  • Page 718 For further details about activation of the Engine Crank mode in GTC, refer to the Garmin Pilot's Guide. STARTER is displayed in the CAS window as long as the starter generator is operating. PIM TBM 960 - Edition 0 Page 7.6.20 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 719 Section 7 Description Pilot's Information Manual Figure 7.6.8 - Engine Control Panel AUTO/ON ABORT ENGINE IGNITION STARTER MODE ENGINE / FUEL PIM TBM 960 - Edition 0 Page 7.6.21 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 720: Engine Air Inlet

    System state Status light INERT SEP ON ON (AUTO mode) INERT SEP ON ON (MAN mode) Continue ► PIM TBM 960 - Edition 0 Page 7.6.22 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 721: Exhaust System

    It provides electrical power to the FADEC when the engine is running. The Permanent Magnet Alternator frequency is sensed by the FADEC and used to derive the gas generator speed (Ng). PIM TBM 960 - Edition 0 Page 7.6.23 Rev. 02...

  • Page 722: Propeller Operations

    Reverse Operation Propeller reverse pitch enables reduced landing roll. Reverse is selected via the THROTTLE – refer to Paragraph Engine Control Lever PIM TBM 960 - Edition 0 Page 7.6.24 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 723 When the propeller is feathered after a pilot request, the autothrottle servomotor is clutched to prevent the THROTTLE from moving easily out of the IDLE position. PIM TBM 960 - Edition 0 Page 7.6.25 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 724 Activation of FADEC Protections Minimum blade angle protection: if dedicated sensors indicate that the THROTTLE is in forward position and propeller blade angle goes below the PIM TBM 960 - Edition 0 Page 7.6.26 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 725 Overspeed protection: if propeller speed goes above the maximum threshold, the solenoid commands propeller feathering. PIM TBM 960 - Edition 0 Page 7.6.27 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 726 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.6.28 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 727: Use Of Autothrottle

    ESP on. AT Engine Protections AT engine protections automatically reduce engine power, to ensure that ITT never remains above 840 °C in flight. PIM TBM 960 - Edition 0 Page 7.7.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 728: At Engagement And Disengagement

    To disconnect AT in a standard manner, apply any of the following: Press the AT button on the AFCS control unit Press the AT DISC pushbutton on the THROTTLE PIM TBM 960 - Edition 0 Page 7.7.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 729: Engine Start Or Engine Air Start

    75%, until AT takes control over the THROTTLE. AT mode and status both become active. AT mode sets and maintains maximum TRQ available. PIM TBM 960 - Edition 0 Page 7.7.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 730: Climb

    Its value corresponds to the Maximum Climb power – refer to Subsection 5.8. Engine Operation. Figure 7.7.1 - Maximum Climb Torque Index PIM TBM 960 - Edition 0 Page 7.7.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 731: Cruise

    If the active leg of the flight plan has a speed constraint, the speed constraint is XXXkt. displayed above the airspeed indicator and the AT mode switches to PIM TBM 960 - Edition 0 Page 7.7.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 732 If Long Range Cruise schedule is selected, a white "T" is displayed, which corresponds to the Long Range Cruise power – refer to Subsection 5.8. Engine Operation. Figure 7.7.2 - Maximum Cruise Torque Index PIM TBM 960 - Edition 0 Page 7.7.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 733 Altitude 3,000 ft, Selected Cruise Schedule: Maximum Cruise. Speed Constraint = 120 kt. SPD 120kt Displayed AT mode: Managed AT TRQ ≃ 28% PIM TBM 960 - Edition 0 Page 7.7.7 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 734: Approach

    AT automatically disengages at GS/GP capture and cannot be re-engaged, if in FMS mode. As a result, only MAN mode is permitted for approach, to ensure an appropriate airspeed management until touchdown. PIM TBM 960 - Edition 0 Page 7.7.8 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 735: Go-Around

    FD Vertical Modes and Corresponding AT Modes Summary The following table provides the correspondence between FD vertical modes and AT modes, depending on the MAN/FMS mode. PIM TBM 960 - Edition 0 Page 7.7.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 736 SPD XXXkt CLIMB CLIMB (climb) DESC DESC (descent) GS, GP, PATH SPD XXXkt SPD XXXkt SPD XXXkt SPD XXXkt None (FD disengaged) PIM TBM 960 - Edition 0 Page 7.7.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 737: Fuel System

    The fuel system is comprised of fuel tanks, a fuel unit, manual and automatic selectors, electric and mechanical boost pumps, an engine fuel system, a gauging installation, a monitoring installation and drains. PIM TBM 960 - Edition 0 Page 7.8.1 Rev. 00...
  • Page 738 20) Fuel level gauges 21) Tank drain valve 22) Check-valve 23) Low level detector 24) Suction strainer 25) Fuel amplifier 26) Sequencer PIM TBM 960 - Edition 0 Page 7.8.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 739 FADEC FUEL WARNINGS NOZZLES CAUTION ALARMS FUEL QUANTITIES Avionics system Firewall AUTO/MAN AUTO SHIFT FUEL ENGINE / FUEL L R OFF A200 PIM TBM 960 - Edition 0 Page 7.8.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 740 Section 7 Description Pilot's Information Manual Key to Figure 7.8.2 1) AUX BP switch 2) FUEL SEL pushbutton 3) SHIFT pushbutton PIM TBM 960 - Edition 0 Page 7.8.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 741 Section 7 Description Pilot's Information Manual Figure 7.8.2 - Fuel Control Panel AUTO/MAN AUTO FUEL AUX BP SHIFT ENGINE / FUEL PIM TBM 960 - Edition 0 Page 7.8.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 742: Fuel Tanks

    OFF position prevents an involuntary positioning of the selector OFF. FUEL OFF When the unit is set to OFF, is displayed in the CAS window. PIM TBM 960 - Edition 0 Page 7.8.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 743 Section 7 Description Pilot's Information Manual Figure 7.8.3 - Manual Selector of Fuel Tanks 553L 553L us gal us gal PIM TBM 960 - Edition 0 Page 7.8.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 744: Automatic Tank Selector

    FUEL LOW L-R message of a fuel low situation is displayed. When displayed, the sequencer changes tanks every 1 minute and 15 seconds. PIM TBM 960 - Edition 0 Page 7.8.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 745: Electric Boost Pump (Aux Bp)

    ON, the electric boost pump operates permanently, when set to AUTO, the electric boost pump is automatically operated if there is a fuel pressure drop at the mechanical boost pump outlet. PIM TBM 960 - Edition 0 Page 7.8.9 Rev. 00...

  • Page 746: Main Mechanical Boost Pump

    FUEL CLOGGING Fuel filter clogging is imminent Electric fuel boost pump is running (manual or AUX BP ON automatic mode) Continue ► PIM TBM 960 - Edition 0 Page 7.8.10 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 747: Fuel System Draining And Clogging Indicator

    A pushbutton adjacent to the inspection door controls the illumination of a light that provides improved visibility of the clogging indicator. This indicator shall be visually checked during preflight inspection. PIM TBM 960 - Edition 0 Page 7.8.11 Rev. 00...
  • Page 748 In this situation, the engine is supplied with non-filtered fuel. Maintenance action is required before further flight. PIM TBM 960 - Edition 0 Page 7.8.12 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 749 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.8.13 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 750 1) Lighting pushbutton 2) Mirror door 3) Clogging indicator 4) Central access door 5) Filter drain 6) Tank drain 7) Drain bowl PIM TBM 960 - Edition 0 Page 7.8.14 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 751 Section 7 Description Pilot's Information Manual Figure 7.8.4 - Fuel System Draining Points and Clogging Indicator PIM TBM 960 - Edition 0 Page 7.8.15 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 752 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.8.16 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 753: Electrical System

    In case of failure detection, the "EPS – Service required" message appears in the message window of the GTC. PIM TBM 960 - Edition 0 Page 7.9.1 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 754 ESS BUS 2 EMER NORM ESS. BUS TIE ST - BY MAIN ST - BY GENERATOR RESET BATT MAIN SOURCE GENERATOR ELECTRIC POWER PIM TBM 960 - Edition 0 Page 7.9.2 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 755 EMER Battery Battery Battery None (*) In that case, power is done by MAIN or ST-BY and battery is used as a floated battery. PIM TBM 960 - Edition 0 Page 7.9.3 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 756 Key to Figure 7.9.2 1) MAIN GENERATOR RESET pushbutton 2) ST-BY GENERATOR RESET pushbutton 3) Crash lever 4) SOURCE selector 5) GENERATOR selector PIM TBM 960 - Edition 0 Page 7.9.4 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 757 Pilot's Information Manual Figure 7.9.2 - Electrical Control ST - BY MAIN ST - BY MAIN BATT GENERATOR RESET SOURCE GENERATOR ELECTRIC POWER PIM TBM 960 - Edition 0 Page 7.9.5 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 758: Starter Generator

    BAT OFF is displayed in the CAS window when the battery is isolated from the main bus and when main bus is supplied through another source. PIM TBM 960 - Edition 0 Page 7.9.6 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 759: Ground Power Receptacle

    (pressed down) if the breaker trips again, do not reset. PIM TBM 960 - Edition 0 Page 7.9.7 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 760 GPS NAV 1 protection ADC 1 Air Data Computer 1 protection ENGINE AIRFRAME 1 Powerplant cont. protec.: Oil temp. & pres., torque, propeller Continue ► PIM TBM 960 - Edition 0 Page 7.9.8 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 761 Controller-Pilot Data Link Communications system, if installed protection AIRFRAME DE ICE Empennage and wing leading edges deicing INERT DE ICE Inertial separator protection Continue ► PIM TBM 960 - Edition 0 Page 7.9.9 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 762 TAS, if installed protection Weather radar protection DATA LINK Data Link, if installed protection LDG CONT Landing gear control protection Continue ► PIM TBM 960 - Edition 0 Page 7.9.10 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 763 BATT BUS EMER LIGHT Instrument panel emergency lighting protection GND CLR Ground clearance protection ACCESS Cabin access lighting protection Electrical power system protection PIM TBM 960 - Edition 0 Page 7.9.11 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 764 L WS PITOT R PRESS & STALL DE ICE ALTI EMER LH LDG RH LDG PULSE TAXI ACCESS LIGHT LIGHT LIGHT LIGHT SYST PIM TBM 960 - Edition 0 Page 7.9.12 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 765 L WS DE ICE PITOT R & STALL TAXI LIGHT LH LDG LIGHT RADIO ALTI RH LDG LIGHT PULSE SYST FUEL SEL PIM TBM 960 - Edition 0 Page 7.9.13 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 766 DATA HUB DIM WINDOWS (if installed) 115 VAC PLUG HEATERS CMD NOTE Breakers located on Frame C13bis and Frame C15. NOT USED PIM TBM 960 - Edition 0 Page 7.9.14 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 767 XPDR 1 EMER AHRS 1 BUS 2 LDG SIG CPCS PWR1 CAB BLEED IGNITION EMER LIGHT GND CLR ACCESS (driving geared motor) PIM TBM 960 - Edition 0 Page 7.9.15 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 768: Emergency Use

    Ground power receptacle access door is not closed Protection - Safety Table 7.9.1 Figure 7.9.2. The electrical power system provides systems protection in case of: overvoltage, short-circuits. PIM TBM 960 - Edition 0 Page 7.9.16 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 769: Exterior Lighting

    NOTE At night, do not use anti-collision lights in fog, clouds, or mist – as reflection of the flashing lights may lead to dizziness and disorientation. PIM TBM 960 - Edition 0 Page 7.9.17 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 770 Fuel Unit Compartment Light The lighting of the fuel unit compartment allows improving the visibility of the clogging indicator by pressing the pushbutton located besides the inspection door. PIM TBM 960 - Edition 0 Page 7.9.18 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 771 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.9.19 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 772 Key to Figure 7.9.7 1) Taxi and landing light switch 2) Pulselite system switch 3) Navigation lights switch 4) Strobe lights switch PIM TBM 960 - Edition 0 Page 7.9.20 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 773 Section 7 Description Pilot's Information Manual Figure 7.9.7 - Exterior Lighting Controls TAXI NAV STROBE PULSE EXT LIGHTS PIM TBM 960 - Edition 0 Page 7.9.21 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 774: Interior Lighting

    Breaker Panel Lighting Breaker panel lighting is controlled by a switch located on the instrument panel near the pilot’s control wheel. PIM TBM 960 - Edition 0 Page 7.9.22 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 775 A rheostat located on the cockpit overhead panel controls emergency lighting operation and intensity. Forward rotation of control knob allows changing from OFF position to minimum lighting then increasing lighting to maximum brightness. PIM TBM 960 - Edition 0 Page 7.9.23 Rev. 02...
  • Page 776 1) Instrument panel lighting switch (rheostat) 2) Cabin lighting switch (rear seats reading light) 3) Access lighting pushbutton 4) Emergency lighting switch 5) Breaker panel lighting switch PIM TBM 960 - Edition 0 Page 7.9.24 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 777 Section 7 Description Pilot's Information Manual Figure 7.9.8 - Internal Lighting Controls PANEL CABIN ACCESS INT LIGHTS CB LIGHT PIM TBM 960 - Edition 0 Page 7.9.25 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 778: 115 V Plug

    The Quick-Disconnect connector shall be connected to the battery to allow the BatteryMINDer charger to keep the charge of the battery. For servicing, refer to Paragraph BatteryMINDer Charger in Subsection 8.7. PIM TBM 960 - Edition 0 Page 7.9.26 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 779: 7.10 - Cabin Air Temperature And Pressurization

    The pilot monitors the system through information and CAS messages displayed in the CAS window. These indications are independent of the ECS controls and internal sensors. PIM TBM 960 - Edition 0 Page 7.10.1 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 780 28) Bleed controller with muffler and flow sensor 29) Bleed check valve 30) Compressor 31) Flow Control Shut-Off Valve (FCSOV) 32) Bleed Ejector Valve (BEV) 33) Shut-Off Valve (SOV) PIM TBM 960 - Edition 0 Page 7.10.2 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 781 34) Bleed air high temperature sensor 35) Temperature Modulating Valve (TMV) 36) Ground Fan (GF) 37) Ram air check valve 38) Heat exchanger PIM TBM 960 - Edition 0 Page 7.10.3 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 782 PRESSU OFF Cockpit zone bulkhead Firewall Conditioned air generation Conditioned distribution Refrigerant fluid Flapper Fresh air distribution Ambient air NACA inlet port Pneumatic PIM TBM 960 - Edition 0 Page 7.10.4 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 783: Engine Bleed Air System

    ITT within engine limitations. Figure 7.10.2 - Bleed Status Display PROP PROP °C °C 96.8 1925 96.8 1925 P2.5 HI °C °C PIM TBM 960 - Edition 0 Page 7.10.5 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 784: Cabin Pressurization Control System

    Figure 7.10.4. BLEED switch actuation in the AUTO position is required for proper operation of the CPCS which regulates the cabin altitude. PIM TBM 960 - Edition 0 Page 7.10.6 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 785 These indications are independent of the ECS controls and internal sensors. PIM TBM 960 - Edition 0 Page 7.10.7 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 786 9,800 ft. The cabin pressurization is degraded without total ECS DEGRADED loss of cabin pressurization, or the heating system is degraded. PIM TBM 960 - Edition 0 Page 7.10.8 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 787: Dual-Zone Temperature Control System (Tcs)

    PIM TBM 960 - Edition 0 Page 7.10.9 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 788 FAN selector. When set to AUTO, the ECS controller drives the fan speed in order to reach the selected temperature in the most efficient way. PIM TBM 960 - Edition 0 Page 7.10.10 Rev. 02...
  • Page 789 RAM AIR control knob. If necessary, depressurize the cabin. System Protection Power for the ECS is supplied by the BUS 2 bar and is protected by the AIR COND breaker. PIM TBM 960 - Edition 0 Page 7.10.11 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 790 Ground Fan (GF), turns off the Condenser Fan (COND FAN), opens the compressor clutch. during engine start: turns off the Vapor Cycle System (VCS). PIM TBM 960 - Edition 0 Page 7.10.12 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 791 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.10.13 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 792 3) DEFOG pushbutton 4) CABIN CTRL pushbutton 5) Cockpit FAN selector 6) DUMP switch 7) Cabin temperature control 8) Cabin fan control PIM TBM 960 - Edition 0 Page 7.10.14 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 793 Section 7 Description Pilot's Information Manual Figure 7.10.4 - ECS Controls PRESSURIZATION DUMP BLEED AUTO NORM OFF/RST TEMP AUTO CABIN CTRL AUTO PIM TBM 960 - Edition 0 Page 7.10.15 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 794 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.10.16 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 795: Emergency Oxygen System

    64 and 85 PSIG (4.4 and 5.9 bars), a low-pressure safety valve calibrated to 116 PSIG (8 bars). A control panel located in the cockpit's overhead panel includes: PIM TBM 960 - Edition 0 Page 7.11.1 Rev. 00...
  • Page 796 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. PIM TBM 960 - Edition 0 Page 7.11.2 Rev. 00...
  • Page 797 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.) on the user's face. PIM TBM 960 - Edition 0 Page 7.11.3 Rev. 00...
  • Page 798 Section 7 Description Pilot's Information Manual Key to Figure 7.11.1 1) MICRO/MASK switch 2) OXYGEN switch 3) PASSENGER OXYGEN switch PIM TBM 960 - Edition 0 Page 7.11.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 799 Section 7 Description Pilot's Information Manual Figure 7.11.1 - Emergency Oxygen System MICRO STBY DEPLOY OXYGEN PIM TBM 960 - Edition 0 Page 7.11.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 800 1) Harness inflation side vanes 2) N (Normal) - 100% regulator control tab 3) EMERGENCY control knob 4) PRESS TO TEST function 5) Vent valve PIM TBM 960 - Edition 0 Page 7.11.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 801 Section 7 Description Pilot's Information Manual Figure 7.11.2 - Crew Oxygen Masks - Regulator Controls 100% PUSH EMERGENCY PRESS TEST PIM TBM 960 - Edition 0 Page 7.11.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 802: Flight Above 15,000 Ft With Possible Emergency Descent

    10 °F -10 °F Cockpit Cabin (21°C) (43 °C) (32 °C) (10°C) (-1°C) (-12°C) (-23°C) 1010 1,056 1,137 1,096 1,015 Continue ► PIM TBM 960 - Edition 0 Page 7.11.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 803: Enroute Altitude

    Flight above 15,000 ft. All equipment in use, One hour of utilization by each pilot and passenger, Plus one hour of utilization by each pilot under 15,000 ft. PIM TBM 960 - Edition 0 Page 7.11.9 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 804: Flight Between 15,000 Ft And 10,000 Ft

    Flight under 15,000 ft, 90 minutes of utilization by each pilot and one passenger, Plus 30 minutes of utilization by each pilot at 10,000 ft. PIM TBM 960 - Edition 0 Page 7.11.10 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 805 NOTE Increase the pressure in the table by 8% if the airplane has been parked in sunlight for an extended period of time. PIM TBM 960 - Edition 0 Page 7.11.11 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 806 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.11.12 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 807: 7.12 - Air Data System And Instruments

    In this case, static pressure from the alternate line is only provided to the standby instrument. Static pressure from the alternate line is not provided to either ADC. PIM TBM 960 - Edition 0 Page 7.12.1 Rev. 00...

  • Page 808: Dynamic Pressure Systems

    Subsection Ice Protection Equipment. CAUTION To avoid probe overheating while on the ground, do not turn on the pitot heat for long periods. PIM TBM 960 - Edition 0 Page 7.12.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 809 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.12.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 810 12) Instrument panel 13) Dynamic system drain 14) Pitot R 15) Rear pressure bulkhead 16) Static port 17) Alternate static port 18) Static port PIM TBM 960 - Edition 0 Page 7.12.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 811 Section 7 Description Pilot's Information Manual Figure 7.12.1 - Air Data System PIM TBM 960 - Edition 0 Page 7.12.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 812 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.12.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 813: 7.13 - Vacuum System And Instruments

    In case of pressure drop, a pressure switch installed in VACUUM LOW the system indicates the failure, and is displayed in the CAS window. PIM TBM 960 - Edition 0 Page 7.13.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 814 1) Regulating and relief valve 2) Air ejector 3) Air check valve 4) Suction relief valve 5) Pressure switch 6) Failure CAS message PIM TBM 960 - Edition 0 Page 7.13.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 815 Pilot's Information Manual Figure 7.13.1 - Vacuum System Powerplant atmosphere Firewall Deicing system CAS window High pressure VACUUM LOW Controlled pressure Avionics display Vacuum PIM TBM 960 - Edition 0 Page 7.13.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 816: Standby Attitude Module (Md302)

    The magnetic heading data is provided by the MD32 magnetometer installed on the left wing. The standby attitude module is located on the instrument panel's top left-hand corner. PIM TBM 960 - Edition 0 Page 7.13.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 817: 7.14 - Ice Protection Equipment

    D E I C E D E I C E S H I E L D L I G H T AUTO PIM TBM 960 - Edition 0 Page 7.14.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 818 Then all the ice protection systems turn off. ICE DETECTION FAIL is displayed in the CAS window in the following cases: PIM TBM 960 - Edition 0 Page 7.14.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 819: Wing And Empennage Deicing

    PROP DE ICE system is activated either manually or automatically. Each cycle is 180 seconds long. The cycles continue as long as the system is activated. PIM TBM 960 - Edition 0 Page 7.14.3 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 820: Windshield Deicing

    56 °C (133 °F). In that case, the windshield is no longer heated, the pilot can reset the system by setting the WINDSHIELD switch to OFF, then to ON. PIM TBM 960 - Edition 0 Page 7.14.4 Rev. 00...

  • Page 821: Heating Of Pitots And Stall Warning Sensor

    Correct operation of the audible stall warning may be altered by severe or prolonged icing. Turbine Air Inlet Protection Operation and description are detailed in Paragraph Engine Air Inlet in Subsection 7.6. PIM TBM 960 - Edition 0 Page 7.14.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 822 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.14.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 823: 7.15 - Miscellaneous Equipment

    Whenever possible, avoid known severe precipitation areas to prevent loss of dependable PIM TBM 960 - Edition 0 Page 7.15.1 Rev. 01...

  • Page 824: Cabin Fire Extinguisher

    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. PIM TBM 960 - Edition 0 Page 7.15.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 825 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.15.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 826 1) MFD 2) Radar mode 3) Area of weather display 4) Antenna stabilization status 5) Touchscreen controllers 6) Scale for weather display PIM TBM 960 - Edition 0 Page 7.15.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 827 Figure 7.15.1 - Weather Radar Display and Controls WEATHER STAB ON TILT SCALE TILT UP 1.50° HEAVY BEARING L 0° SECTOR SCAN FULL LIGHT GAIN CALIBRATED PIM TBM 960 - Edition 0 Page 7.15.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 828: Emergency Locator Transmitter

    B. On the remote control box, red indicator light flashes. C. On the ELT, red indicator light flashes. D. Near the ELT, the buzzer sounds. PIM TBM 960 - Edition 0 Page 7.15.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 829: Lightweight Data Recorder (Ldr 1000)

    ADS-B OUT data. Depending on the nature of the fault or failure, the transponder may no longer be transmitting all of the required data in the ADS-B OUT messages. PIM TBM 960 - Edition 0 Page 7.15.7 Rev. 01...

  • Page 830: Flight Deck Information System (Gdl 60)

    The DCTU is installed in the front cargo compartment and is connected to the FADEC. It does not require a pilot input to operate. The DCTU is electrically supplied by: PIM TBM 960 - Edition 0 Page 7.15.8 Rev. 01...

  • Page 831: Garmin Integrated Flight Deck (Gifd) Approaches

    SBAS, although high GPS vertical error estimate anomalies could result in loss of advisory vertical guidance. If GPS is lost, the LNAV approach will be aborted. L/VNAV RNAV (GPS) or RNAV (GNSS) – PIM TBM 960 - Edition 0 Page 7.15.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 832 Final Approach Segment (FAS) Altimeter systems follow the ISA temperature modelling. When actual atmospheric conditions deviate from the ISA model, errors in altitude will occur. PIM TBM 960 - Edition 0 Page 7.15.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 833 Temperature Compensation of Approach Minimums PIM TBM 960 - Edition 0 Page 7.15.11 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 834 (the VDI will be flagged "NO GP" until APR DWNGRADE has been acknowledged). APR DWNGRADE L/VNAV is acknowledged, is displayed in magenta. PIM TBM 960 - Edition 0 Page 7.15.12 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 835 When the approach is no longer a part of a flight plan, these waypoints are deleted. A visual approach can be inserted onto the Active Flight Plan or the Standby Flight Plan. A visual approach also can be inserted into a PIM TBM 960 - Edition 0 Page 7.15.13 Rev. 01...

  • Page 836: Homesafe Emergency Function

    Garmin Pilot's Guide. HomeSafe is an emergency autopilot function that is meant to be used in the event of pilot incapacitation, i.e. in situations where the pilot is not capable of PIM TBM 960 - Edition 0 Page 7.15.14 Rev. 01...
  • Page 837 Land and stop the airplane on the runway, Shut down the engine. To perform this entire sequence, HomeSafe requires the airplane's systems to be fully operational. PIM TBM 960 - Edition 0 Page 7.15.15 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 838 MFD reconfiguration can take up to one minute. During this time, engine instruments and CAS messages can be displayed on the PFD by using DISPLAY BACKUP. PIM TBM 960 - Edition 0 Page 7.15.16 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 839: Optional Equipment

    TAS – are described in the Garmin Pilot's Guide. NOTE Refer to Paragraph Chartview System Operating Limitations in Subsection 2.6. for operating limitations of the Chartview system. PIM TBM 960 - Edition 0 Page 7.15.17 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 840 Section 7 Description Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 7.15.18 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 841 Propeller Care ..............8.8.2 Engine Care ................8.8.2 Interior Care ................8.8.2 - Preparation of the Airplane (Equipment and Furnishings) ..8.9.1 PIM TBM 960 - Edition 0 Page 8.0.1 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 842 8.10 - Utilization in Cold Weather (-0 °C to -25 °C) or Very Cold Weather (-25 °C to -40 °C) ............8.10.1 PIM TBM 960 - Edition 0 Page 8.0.2 Rev. 02 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 843: General

    For additional information, refer to the manufacturer's Airplane Maintenance Manual. PIM TBM 960 - Edition 0 Page 8.1.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 844 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 8.1.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 845: Identification Plate

    – together with the model number, type certificate number and production certificate number – is stamped on the identification plate attached to the left side of the fuselage beneath the horizontal stabilizer. PIM TBM 960 - Edition 0 Page 8.2.1 Rev. 00...
  • Page 846 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 8.2.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 847: Publications

    Airplane Maintenance Manual, Illustrated Parts Catalog, Catalog of Service Bulletins, Service Letters. CAUTION The POH must always be carried in the airplane. PIM TBM 960 - Edition 0 Page 8.3.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 848 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 8.3.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 849: Inspection Periods

    An Airplane Maintenance Manual must be consulted prior to performing any preventive maintenance to make sure that proper procedures are followed. Maintenance must be performed by licensed personnel. PIM TBM 960 - Edition 0 Page 8.4.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 850 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 8.4.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 851: Alterations Or Repairs

    Alterations or repairs must be performed by licensed personnel. PIM TBM 960 - Edition 0 Page 8.5.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 852 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 8.5.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 853: Ground Handling

    When parking the aircraft for periods of longer than 24 hours, use the protective windshield cover, securing it with the lateral and underside straps. PIM TBM 960 - Edition 0 Page 8.6.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 854: Tie-Down

    Airplane fueling: keep fuel tanks full to minimize condensation in the tanks. Battery: Pull the BATT BUS breaker in the front cargo compartment, PIM TBM 960 - Edition 0 Page 8.6.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 855: Long Term Storage Without Flying (More Than 28 Days)

    Close the oxygen cylinder isolation valve. Long Term Storage Without Flying (More Than 28 Days) Refer to the Airplane Maintenance Manual for the procedures to follow. PIM TBM 960 - Edition 0 Page 8.6.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 856 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Figure 8.6.1 - Turning Angle Limits 28° 28° PIM TBM 960 - Edition 0 Page 8.6.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 857 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Figure 8.6.2 - Control Lock PIM TBM 960 - Edition 0 Page 8.6.5 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 858 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 8.6.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 859: Servicing

    To prevent overfilling of the engine oil system, and high oil consumption, an oil level check is recommended within 30 minutes after engine shutdown. The ideal interval is 15 to 20 minutes. If more than 30 minutes have passed and the dipstick PIM TBM 960 - Edition 0 Page 8.7.1 Rev. 00...

  • Page 860: Fuel

    If the quality of fuel used is not correct, defuel airplane completely and refuel with proper quality fuel. PIM TBM 960 - Edition 0 Page 8.7.2 Rev. 00...
  • Page 861 One exception to this can be encountered when operating under the combined effect of the use of certain fuels with high humidity conditions on the ground, PIM TBM 960 - Edition 0 Page 8.7.3 Rev. 00...
  • Page 862 It is possible to use kerosene GOST 10227 RT with the addition of anti-icing additive: Liquid И - GOST 8313-88 The above-mentioned additive is added in the quantity equal to 0.3% per volume. PIM TBM 960 - Edition 0 Page 8.7.4 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 863 Handling, Servicing and Maintenance Pilot's Information Manual CAUTION Refer to the P&WC Engine Maintenance Manual's latest revision for appropriate quantities of anti-ice additive. PIM TBM 960 - Edition 0 Page 8.7.5 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 864 Fuel ( Litres ) ( Litres ) ( U.S qt ) 1050 1200 210 240 270 300 330 Fuel ( U.S Gal ) PIM TBM 960 - Edition 0 Page 8.7.6 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 865: Landing Gear

    PSIG. A chart located on the inside of the cylinder service door – see Figure 8.7.2 – indicates the maximum cylinder charge pressure for the ambient temperature. PIM TBM 960 - Edition 0 Page 8.7.7 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 866 200 PSIG (13.7 bars) per minute. CAUTION Replenishment of the oxygen system should only be performed by qualified personnel. PIM TBM 960 - Edition 0 Page 8.7.8 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 867 Make sure all tools and materials are removed and the work area is clean and free from debris. Close the oxygen service door. PIM TBM 960 - Edition 0 Page 8.7.9 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 868 Fold the headstrap into the facepiece. Pull the lanyard cord outward to the facepiece’s side so that it does not interfere with repacking. Lay the reservoir bag on a flat surface and smooth out any wrinkles. PIM TBM 960 - Edition 0 Page 8.7.10 Rev. 00...
  • Page 869 Gently fold reservoir bag lengthwise into thirds (outside edges folded inward over the bag’s center). Do not crease the bag. 6,35 57,1 mm 2.1/4 in PIM TBM 960 - Edition 0 Page 8.7.11 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 870 Bottom view Breathing valves Coil the oxygen tubing inside facepiece over the reservoir bag. Connect oxygen tubing to the manifold oxygen fitting. PIM TBM 960 - Edition 0 Page 8.7.12 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 871: Batteryminder Charger

    After use, disconnect the BatteryMINDer charger plugs (7) then (5), put the cap (1) back on the connector (2) and push the BATT BUS breaker located in the front cargo compartment. PIM TBM 960 - Edition 0 Page 8.7.13 Rev. 00...
  • Page 872 Key to Figure 8.7.3 1) Cap 2) Connector 3) Quick-Disconnect connector 4) Battery 5) BatteryMINDer charger connector plug 6) BatteryMINDer charger 7) Plug PIM TBM 960 - Edition 0 Page 8.7.14 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 873 (Hold for 3 sec.) DESULFATING COMPENSATION For sealed or Filler Lead-Acid GA Batteries ONLY - NOT FOR NiCad BatteryMINDers.com / 800-379-79 (ET) PIM TBM 960 - Edition 0 Page 8.7.15 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 874 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 8.7.16 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 875: Airplane Cleaning And Care

    Painted Surfaces Refer to the Airplane Maintenance Manual for the products and procedures to apply. PIM TBM 960 - Edition 0 Page 8.8.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 876: Propeller Care

    To remove dust and loose dirt from the upholstery and carpet, clean the interior regularly with a vacuum cleaner. For additional information, refer to the Airplane Maintenance Manual. PIM TBM 960 - Edition 0 Page 8.8.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 877 To prevent damage to seat cushion covers, protective covers should be put on the seats. 1) Install protective covers. 2) Unlock backrest using backrest tilting handle and fold it forward. PIM TBM 960 - Edition 0 Page 8.9.1 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 878 Ensure proper storage of strap with left-side rear seat to avoid loosing part. D. Removal of intermediate seats – see Figure 8.9.2 Figure 8.9.4 PIM TBM 960 - Edition 0 Page 8.9.2 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 879 E. Removal of a cabinet NOTE This operation must be carried out by a service center. Installation of intermediate seats – see Figure 8.9.2 Figure 8.9.4 PIM TBM 960 - Edition 0 Page 8.9.3 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 880 8) Install backrest bottom upholstery. NOTE Adjust it properly; make sure not to obstruct deflector outlet. 9) Slide properly the carpet under the seat. PIM TBM 960 - Edition 0 Page 8.9.4 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 881 1) Make sure the work area is clean and free from debris. 2) Clear the carpet from seat area to facilitate moving in rails. 3) Check that knobs maintain locks in up position. PIM TBM 960 - Edition 0 Page 8.9.5 Rev. 01...
  • Page 882 However, it is the pilot's responsibility to ensure that all necessary authorizations are obtained from the appropriate regulatory authority. PIM TBM 960 - Edition 0 Page 8.9.6 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 883 Installation Paragraph 2.E. Removal Paragraph 1.D. Intermediate seat Installation Paragraph 1.F. Paragraph Use of Cargo net Installation Cargo Nets in Subsection 7.3. PIM TBM 960 - Edition 0 Page 8.9.7 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 884 3) Lock 4) Pad 5) Rail 6) Backrest tilting handle 7) Quick link 8) Knob 9) Strap 10) Seat heaters and headset connectors PIM TBM 960 - Edition 0 Page 8.9.8 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 885 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Figure 8.9.1 - Removal / Installation of Rear Seat PIM TBM 960 - Edition 0 Page 8.9.9 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 886 Key to Figure 8.9.2 1) Locking handle 2) Lock 3) Pad 4) Rail 5) Backrest bottom upholstery 6) Seat heaters and headset connectors PIM TBM 960 - Edition 0 Page 8.9.10 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 887 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Figure 8.9.2 - Removal / Installation of Intermediate Seat C13 bis PIM TBM 960 - Edition 0 Page 8.9.11 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 888 Handling, Servicing and Maintenance Pilot's Information Manual Key to Figure 8.9.3 1) Blanking plug 2) Blanking plug 3) Blanking device assy 4) Deflector PIM TBM 960 - Edition 0 Page 8.9.12 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 889 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Figure 8.9.3 - Cabin Comfort – Hot Air Outlets and Deflectors PIM TBM 960 - Edition 0 Page 8.9.13 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 890 Handling, Servicing and Maintenance Pilot's Information Manual Key to Figure 8.9.4 1) Deflector 2) Deflector hole 3) Red mark 4) Color mark PIM TBM 960 - Edition 0 Page 8.9.14 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 891 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Figure 8.9.4 - Cabin Comfort – Installation of Deflector Aligned PIM TBM 960 - Edition 0 Page 8.9.15 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 892 Section 8 Handling, Servicing and Maintenance Pilot's Information Manual Intentionally left blank PIM TBM 960 - Edition 0 Page 8.9.16 Rev. 01 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 893 Table 8.10.1 - Tire and Shock Absorber Pressures in Cold or Very Cold Weather OAT (°C) Inflation Pressures Main landing gear shock absorber (bars) (13) (13.5) (14) (15) (17) Continue ► PIM TBM 960 - Edition 0 Page 8.10.1 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 894 Nose gear shock absorber (bars) (7.5) (8.5) (9.5) Main landing gear tire (bars) (9.96) (9.96) (8.96) (8.96) (8.96) Nose gear tire (bars) (6.5) (6.5) PIM TBM 960 - Edition 0 Page 8.10.2 Rev. 00 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 895 Supplement 6 WX-500 stormscope Pilot's Operating Handbook SUPPLEMENT WX-500 stormscope Table of contents Page General ..........9.6.2 Limitations .
  • Page 896 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 897 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 898 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 899 Supplement 49 GARMIN TAWS system Pilot's Operating Handbook SUPPLEMENT GARMIN TAWS system Table of contents Page General ..........9.49.2 Limitations .
  • Page 900 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 901 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 902 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 903 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 904 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 905 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 906 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 907 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 908 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 909 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 910 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 911 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 912 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 913 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 914: 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 915: 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 916: 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 917: 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 918: 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 919 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 920 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 921 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 922 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 923 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 924 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 925 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 926 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 927 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 928 Supplement 72 France specifics Pilot's Operating Handbook SUPPLEMENT France specifics Table of contents Page General ..........9.72.2 Limitations .
  • Page 929 Supplement 72 France specifics Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the airplane specifics, among others those required by the relevant Certification Authorities (limitations, description and operations necessary to the operation of the French registered TBM airplane). SECTION 2 Limitations The limitations hereafter supplement or replace those of the standard airplane...
  • Page 930 Supplement 72 France specifics Pilot's Operating Handbook On pilot door - Internal side, if installed On emergency exit handle Marking on cover Marking on handle Edition 0 - December 04, 2019 Page 9.72.3 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 931 Supplement 72 France specifics Pilot's Operating Handbook Above emergency exit door On rear passengers masks containers On internal face of rear passengers masks containers doors Page 9.72.4 Edition 0 - December 04, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 932 Supplement 72 France specifics Pilot's Operating Handbook >> Airplane equipped with lavatory compartment (Post-MOD70-0505-25) On access door, cabin side and toilet side Behind access door, cabin side and toilet side Edition 0 - December 04, 2019 Page 9.72.5 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 933 Supplement 72 France 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 934 Supplement 72 France specifics Pilot's Operating Handbook SECTION 8 Handling, servicing and maintenance No specifics Edition 0 - December 04, 2019 Page 9.72.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 935 Supplement 72 France specifics Pilot's Operating Handbook Intentionally left blank Page 9.72.8 Edition 0 - December 04, 2019 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 936 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook SUPPLEMENT Extended large storage cabinet Table of contents Page General ..........9.73.2 Limitations .

  • Page 937: General

    Supplement 73 Extended large storage cabinet Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, description and procedures necessary for operation when the airplane is equipped with the Extended large storage cabinet option. SECTION 2 Limitations The information in this section supplements and/or replaces the information in...

  • Page 938: Emergency Procedures

    Supplement 73 Extended large storage cabinet Pilot's Operating Handbook Inside small internal drawer, on side wall >> Cabinet equipped with electrical supply Beside 115 VAC plug SECTION 3 Emergency procedures Installation and operation of the Extended large storage cabinet do not change the emergency procedures of the airplane described in section 3 Emergency procedures of the standard POH.

  • Page 939: Performance

    Supplement 73 Extended large storage cabinet Pilot's Operating Handbook SECTION 5 Performance Installation and operation of the Extended large storage cabinet do not change the performance of the airplane described in section 5 Performance of the standard POH. SECTION 6 Weight and balance The information in this section supplements and/or replaces the information in section 6 Weight and balance of the standard POH when the airplane is equipped with...
  • Page 940 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook Using the weight and balance form CAUTION ▲ ▲ Use the empty weight, arm and CG % from the weight and balance report that includes the Extended large storage cabinet option. ▲...
  • Page 941 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook Airplane loading form (m, kg) Moment = Weight x Arm ( Arm (m) 4.392 ) − CG (MAC %) = × 100 1.51 Weight Moment Item (kg) (m.kg) (MAC %) Empty weight (kg) Baggage 3.250...
  • Page 942 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook Figure 9.73.1 - Weight and balance diagram Edition 0 - February 14, 2020 Page 9.73.7 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 943 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook Weight and balance form and diagram (in, lbs) ( Arm (in) 172.93 ) − CG (MAC %) = × 100 Moment = Weight x Arm 59.45 Weight Moment Item (lbs) (in) (in.lbs) (MAC %) Empty weight...
  • Page 944 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook Figure 9.73.2 - Weight and balance diagram Edition 0 - February 14, 2020 Page 9.73.9 Rev. 0 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

  • Page 945: Description

    Supplement 73 Extended large storage cabinet Pilot's Operating Handbook SECTION 7 Description The information in this section supplements and/or replaces the information in section 7 Description of the standard POH when the airplane is equipped with the Extended large storage cabinet option. The Extended large storage cabinet is installed at the place of the left intermediate seat.
  • Page 946 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook The cabinet is composed of two large drawers and a small drawer completing the storage volume of a large drawer. One large drawer opens sideways into the aisle. A small drawer is installed inside this large storage volume.
  • Page 947 Supplement 73 Extended large storage cabinet Pilot's Operating Handbook The cabinet is electically supplied by the BUS 4 bar and is protected by the CABINET breaker located on frame C13bis. Circuit breakers are located under the roof of the aft large drawer (refer to A). Figure 9.73.6 - Circuit breakers and plugs List of circuit breakers located inside the cabinet : BUS 4...
  • Page 948 Supplement 75 GDR66 CPDLC and COM3 VHF Pilot's Operating Handbook communications Supplement GDR66 CPDLC and COM3 VHF communications Table of contents Page General ..........9.75.2 Limitations .

  • Page 949: General

    Supplement 75 GDR66 CPDLC and COM3 VHF communications Pilot's Operating Handbook SECTION 1 General This supplement is intended to inform the pilot about the equipment limitations, descriptions and procedures necessary for operation when the airplane is equipped with the GDR66 transceiver. The information in this section supplements and/or replaces the information in section 1: General of the standard POH when the airplane is equipped with the GDR66 transceiver.

  • Page 950: Limitations

    Supplement 75 GDR66 CPDLC and COM3 VHF Pilot's Operating Handbook communications SECTION 2 Limitations The information in this section supplements and/or replaces the information in section 2: Limitations of the standard POH when the airplane is equipped with the GDR66 transceiver. 2.6 - Operation limits CPDLC limitations, if installed WARNING...

  • Page 951: Emergency Procedures

    Supplement 75 GDR66 CPDLC and COM3 VHF communications Pilot's Operating Handbook SECTION 3 Emergency procedures The information in this section supplements and/or replaces the information in section 3: Emergency procedures of the standard POH when the airplane is equipped with the GDR66 transceiver. >>...

  • Page 952: Weight And Balance

    Supplement 75 GDR66 CPDLC and COM3 VHF Pilot's Operating Handbook communications SECTION 6 Weight and balance The information in this section supplements and/or replaces the information in section 6: Weight and Balance of the standard POH when the airplane is equipped with the GDR66 transceiver.

  • Page 953: Description

    Supplement 75 GDR66 CPDLC and COM3 VHF communications Pilot's Operating Handbook SECTION 7 Description The information in this section supplements and/or replaces the information in section 7: Description of the standard POH when the airplane is equipped with the GDR66 transceiver. 7.15 - Miscellaneous equipment The GDR 66 is a digital communications transceiver.
  • Page 954 Supplement 75 GDR66 CPDLC and COM3 VHF Pilot's Operating Handbook communications VHF COM3 communications ● NOTE ● COM1 and COM2 remain the primary means of communications. ● The pilot can operate COM3 communications through the GTC. It will be available as GDR audio channel.
  • Page 955 Supplement 75 GDR66 CPDLC and COM3 VHF communications Pilot's Operating Handbook Figure 9.75.2 - Partial electrical distribution of BUS bars Page 9.75.8 Edition 0 - March 15, 2021 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
  • Page 956 Supplement 75 GDR66 CPDLC and COM3 VHF Pilot's Operating Handbook communications SECTION 8 Handling, servicing and maintenance Installation and operation of the GDR66 transceiver do not change the handling, servicing and maintenance of the airplane described in section 8: Handling, servicing and maintenance of the standard POH.
  • Page 957 Supplement 75 GDR66 CPDLC and COM3 VHF communications Pilot's Operating Handbook Intentionally left blank Page 9.75.10 Edition 0 - March 15, 2021 Rev. 1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...

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