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General| Synthetic Vision Technology | Yes |
|---|---|
| Touchscreen Controller | Yes |
| Engine Indicating and Crew Alerting System | Yes |
| Traffic Information Service | Yes |
| Terrain Awareness and Warning System | Yes |
Provides basic data and information of general interest, including definitions and explanations of abbreviations and terminology.
Outlines the operating airspeed limitations and their significance for safe flight.
Specifies limitations for the engine, oil, fuel, and propeller systems.
Defines the limits for starter operation sequences and timings.
Details the maximum airplane weights and center of gravity limits.
Covers operational limits such as maneuver, temperature, load factor, and system limitations.
Explains markings on airspeed indicators, pressurization, and engine instruments.
Details various placards found on the airplane, including flight limitations and weight information.
This section of the airplane POH presents the various operating limitations, the significance of such limitations, instrument markings, color coding, and basic placards necessary for safe operation.
Provides general information about the TBM 960, its certification, and the scope of the limitations section.
Outlines the operating airspeed limitations and their significance for safe flight.
Specifies limitations for the engine, oil, fuel, and propeller systems.
Defines the limits for starter operation sequences and timings.
Details the maximum airplane weights and center of gravity limits.
Covers operational limits such as maneuver, temperature, load factor, and system limitations.
Includes limits for seating, baggage, crew, occupancy, doors, and cargo net installation.
Explains markings on airspeed indicators, pressurization, and engine instruments.
Details various placards found on the airplane, including flight limitations and weight information.
This section provides the recommended procedures in the event of a major failure and/or an emergency situation.
Provides an overview of recommended procedures for major failures and emergency situations, referencing checklists and memory items.
Outlines procedures for engine failure before rotation and for other reasons.
Details procedures for engine failure before rotation, after rotation, and in flight.
Provides information on the engine air start envelope and procedure.
Covers procedures for engine fire on ground/in flight and cabin electrical fire or smoke.
Presents emergency descent profiles and procedures.
Details procedures for forced landings, ditching, tire blowout, and flap asymmetry.
Outlines procedures for fuel pressure, low level, and fuel clogging issues.
Describes procedures related to bus bars and electrical system failures.
Covers procedures for cabin altitude, pressurization, and ECS malfunctions.
States that there are no specific emergency procedures for the deicing system.
Details procedures for unsuccessful AT disconnection, trim runaway, USP active, and system failures.
Covers miscellaneous emergency procedures like cockpit window cracks, emergency exit use, and ELT use.
This section provides the recommended procedures in cases of minor failure and abnormal situation.
Provides recommended procedures for minor failures and abnormal situations, referencing checklists and memory items.
States that there are no abnormal procedures for rejected takeoff and refers to Section 3 for emergency procedures.
Details procedures for ITT HI, CHIP, ENG PROT ACTIVE, FEATHER MISMATCH, SET PWR TO IDLE, ENG OP DEGRADED, FADEC FAULT, FADEC COM 1 CHL, and NP 2000 MAX.
States that there are no abnormal procedures for air start and refers to Section 3 for emergency procedures.
States that there are no abnormal procedures for fire and smoke and refers to Section 3 for emergency procedures.
Presents emergency descent profiles and procedures.
Details procedures for forced landings, ditching, tire blowout, and flap asymmetry.
Details procedures for FUEL PRESS, AUX BP ON, AUTO SEL, FUEL IMBALANCE, LOW LVL FAIL L-R, and FUEL CLOGGING.
Covers abnormal procedures for BAT AMP, BAT OFF, MAIN GEN, LOW VOLTAGE, and MAIN GEN and LOW VOLTAGE.
Details procedures for ECS DEGRADED, PRESSU BACKUP, Cabin Not Depressurized After Landing, VACUUM LOW, and Defog Malfunction.
Covers abnormal procedures for AFRM DEICE FAIL, PROP DEICE FAIL, INERT SEP FAIL, Windshield Deicing Failure, and Windshield Misting or Internal Icing.
Details procedures for ESP FAIL, ESP DEGRADED IAS, ESP DEGRADED AOA, Airspeed Indicating System Failure, AP ON YD OFF, Autopilot or Electric Pitch Trim Malfunction, Dual GPS/SBAS failure, APR DWNGRADE, PIT in AP Vertical Mode, VDI or VDI on Approach, Left PFD Failure, AHRS Failure, ADC Failure, MFD Failure, XPDR1 FAIL or XPDR2 FAIL, XPDR1 ADS-B FAIL or XPDR2 ADS-B FAIL, GWX FAIL, TCAS FAIL, TRAFFIC FAIL, EXCEEDANCE.
Covers miscellaneous abnormal procedures like CARGO DOOR, GPU DOOR, IGNITION, and LMTD DISPATCH.
This section provides procedures for the conduct of normal operation of the TBM airplane, including checklists and amplified procedures.
Provides procedures for the conduct of normal operation of the TBM airplane, including checklists and amplified procedures.
Lists normal operation airspeeds for various configurations like rotation, climb, approach, and cruise.
Details the procedures for inside inspection, before starting engine, engine start, taxiing, takeoff, climb, cruise, descent, approach, and landing.
Describes the step-by-step procedure for conducting a preflight inspection of the aircraft.
Provides guidance on operating the aircraft in known icing conditions, including system checks and airspeeds.
This subsection provides performance data for the climb phase, as well as vertical speeds for climb after a go-around and climb with flaps in TO position.
Provides required performance data for airplane operations, along with additional related information.
States the maximum noise level permitted and the demonstrated noise level for TBM airplanes.
Presents indicated airspeed values assuming zero instrument error for cruise flight.
Shows the cabin altitude obtainable at different flight levels based on airport altitude, cruise FL, and LFE.
Provides conversion tables for units between Imperial/U.S and Metric systems.
Lists stall speeds for various airplane weights, configurations, and bank angles.
Illustrates how to calculate wind components based on wind direction and flight path angle.
Details tables and optimum torque indicator usage for normal engine operation.
Provides takeoff distances for various weight configurations with INERT SEP ON and OFF.
Offers performance data for climb phase, vertical speeds after go-around, and climb with flaps in TO position.
Provides references to performance tables based on INERT SEP ON/OFF status and bleed status.
This section provides procedures to determine the airplane's weight and balance.
Provides pilot procedures for determining the airplane's weight and balance.
Refers to the Airplane Maintenance Manual for weighing procedures.
Details the two baggage compartments, their capacities, and types of securing nets.
Explains the importance of pilot responsibility for proper loading and adhering to weight and balance limits.
References the MyTBM.aero website and airplane records for optional equipment lists.
This section provides description and operation of the airplane and its systems, noting optional equipment.
Provides description and operation of the airplane and its systems, noting optional equipment.
Describes the airplane as a six-place, low wing, semi-monocoque all-metal structure with retractable landing gear.
Details instruments and controls on the instrument panel, including upper, central, and right/left panels.
Explains the roll control activation via rods and cables linked to control wheels, ailerons, and spoilers.
Describes the landing gear system, including hydraulic pressure, lever, position indicator, safety features, and emergency extension.
Describes the PT6E-66XT turboprop engine, its rating, and FADEC control.
Introduces the Autothrottle (AT) function, its integration with AFCS, and SEI.
Details fuel tanks, fuel unit, tank selectors, boost pumps, and fuel system monitoring.
Covers electrical system components, power sources, distribution, and protection.
Details cabin air temperature and pressurization control systems, including ECS, CPCS, and TCS.
Explains the gaseous oxygen system for crew and passengers, its reserve, and operating pressures.
Describes the airplane's air data system including static and dynamic pressure systems and pitot heating.
Details the vacuum system for leading edge deicing operation and its components.
Covers ice detection, pneumatic deicing, propeller deicing, windshield deicing, pitot heating, and turbine air inlet protection.
Describes stall warning system, static dischargers, cabin fire extinguisher, autopilot, GPS, and weather radar.
This section contains the manufacturer-recommended procedures for the airplane's proper ground handling, routine care, and servicing.
Contains manufacturer-recommended procedures for ground handling, care, and servicing of the airplane.
Explains that correspondence should include serial number, model, and type certificate numbers stamped on the identification plate.
Lists POH, Garmin Pilot's Guide, and supplemental data; owner access to AMM, IPC, SBs, SLs on MyTBM.aero.
Refers to regulations and Airplane Maintenance Manual for preventive maintenance procedures and licensed personnel.
Emphasizes contacting airworthiness authorities before alterations/repairs and using licensed personnel.
Provides cautions regarding towing procedures, use of tow bar, and turning angle limits.
Specifies oil types, capacity, servicing intervals, and oil level check procedures.
Provides cleaning instructions for windshield and windows, advising against certain chemicals and buffing machines.
Describes procedures for converting cabin layouts and installing/removing equipment items.
Details procedures for operating the aircraft in cold and very cold weather conditions, including preflight and takeoff.
Provides information on equipment limitations, description, and operations for the GARMIN GSR 56 weather datalink and satellite phone.
Supplements or replaces standard limitations for the TBM airplane equipped with the GARMIN GSR 56 option.
Details placards on the cabin forward of access door and on access door internal side.
Supplements or replaces standard emergency procedures for the airplane equipped with the GARMIN GSR 56 transceiver.
Outlines normal operating procedures for the GARMIN GSR 56 weather datalink and satellite phone system.
Describes the basic performance of the airplane when equipped with the GARMIN GSR 56 weather datalink and satellite phone.
Supplements or replaces standard weight and balance information for the airplane equipped with the GARMIN GSR 56 option.
Provides general information on weight and balance for the GARMIN GSR 56 option.
Supplements or replaces standard descriptions for the airplane equipped with the GARMIN GSR 56 transceiver.
States that installation and operation of the GDR66 transceiver do not change basic handling, servicing, and maintenance procedures.
Provides information on equipment limitations, description, and operations for the GARMIN TAWS system.
Supplements or replaces standard limitations for the airplane equipped with the GARMIN TAWS system.
Supplements or replaces standard emergency procedures for the airplane equipped with the GARMIN TAWS system.
Outlines normal operating procedures for the GARMIN TAWS system.
Describes the basic performance of the airplane when equipped with the GARMIN TAWS system.
Supplements or replaces standard weight and balance information for the airplane equipped with the GARMIN TAWS system.
Provides general information on weight and balance for the GARMIN TAWS system.
Supplements or replaces standard descriptions for the airplane equipped with the GARMIN TAWS system.
States that installation and operation of GARMIN TAWS system do not change basic handling, servicing, and maintenance procedures.
Provides information on equipment limitations, description, and operations for the GARMIN Synthetic Vision System.
Supplements or replaces standard limitations for the airplane equipped with the GARMIN Synthetic Vision System.
Supplements or replaces standard emergency procedures for the airplane equipped with the GARMIN Synthetic Vision System.
Outlines normal operating procedures for the GARMIN Synthetic Vision System.
Describes the basic performance of the airplane when equipped with the GARMIN Synthetic Vision System.
Supplements or replaces standard weight and balance information for the airplane equipped with the GARMIN Synthetic Vision System.
Provides general information on weight and balance for the GARMIN Synthetic Vision System.
Supplements or replaces standard descriptions for the airplane equipped with the GARMIN Synthetic Vision System.
Informs about airplane specifics required by Certification Authorities for the French registered TBM airplane.
Supplements or replaces standard limitations for the airplane equipped with the Extended large storage cabinet option.
Details placards on the cabin forward of access door and on access door internal side.
States that installation and operation of the Extended large storage cabinet do not change basic emergency procedures.
States that installation and operation of the Extended large storage cabinet do not change normal procedures.
States that installation and operation of the Extended large storage cabinet do not change basic performance.
Supplements or replaces standard weight and balance information for airplanes equipped with the Extended large storage cabinet option.
Emphasizes pilot responsibility for proper loading and adhering to weight and balance limits.
Explains using updated reports and tables to calculate weight and balance after cabinet installation.
Supplements or replaces standard descriptions for the airplane equipped with the Extended large storage cabinet option.
Provides information on equipment limitations, description, and operations for the Extended large storage cabinet option.
Supplements or replaces standard limitations for the airplane equipped with the Extended large storage cabinet option.
Details placards on the cabin forward of access door and on access door internal side.
States that installation and operation of the Extended large storage cabinet do not change basic emergency procedures.
States that installation and operation of the Extended large storage cabinet do not change normal procedures.
States that installation and operation of the Extended large storage cabinet do not change basic performance.
Supplements or replaces standard weight and balance information for the airplane equipped with the Extended large storage cabinet option.
Emphasizes pilot responsibility for proper loading and adhering to weight and balance limits.
Explains using updated reports and tables to calculate weight and balance after cabinet installation.
Supplements or replaces standard descriptions for the airplane equipped with the Extended large storage cabinet option.
Supplements or replaces standard emergency procedures for the GDR66 transceiver.
States that installation and operation of the GDR66 transceiver do not change normal procedures.
States that installation and operation of the GDR66 transceiver do not change basic performance.
Supplements or replaces standard weight and balance information for the airplane equipped with the GDR66 transceiver.
Supplements or replaces standard descriptions for the airplane equipped with the GDR66 transceiver.
States that installation and operation of the GDR66 transceiver do not change basic handling, servicing, and maintenance procedures.
