Daher-Socata TBM 900 Quick setup guide

TBM 900
PILOT'S INFORMATION
MANUAL
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It must not be used for any purpose other than that for which it is
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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.
© 2014 - socata -
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DAHER-SOCATA
Customer support
65921 TARBES CEDEX 9
FRANCE Printed in FRANCE
From S/N 1000
P/N T00.DMHPIPYEE0 - EDITION 0 - REVISION 1
CAUTION
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.

PILOT’S OPERATING HANDBOOK
SECTION 0
Edition 0 -- October 31, 2013
Rev. 1
Page 0.5A
SOCATA MODIFICATIONS - INDEX
NOTE
The standardized name for SOCATA modifications is : MODXXX-XX
MOD70 No. SUBJECT CLASSIF.
70-0234-24 Electrical distribution and primary distribution Major
70-0322-00 Evolution of wing tips, tail cone and lights Major
70-0323-71 Propulsion efficiency improvement Major
70-0324-00 Modified pedestal and Single Lever Power Control Assy Major
70-0325-21 Automatic altitude cabin selection Major
70-0330-00 New metal-metal bonding Major
70-0336-26 Fire extinguisher relocation in cockpit minor
70-0341-32 New TBM700 Landing Gear Control and Display Panel minor
70-0342-52 Lower main landing gear doors minor
70-0346-55 New rudder ledge contour minor
70-0347-53 Improved G1000 instrument panel minor
70-0348-27 Control wheel CROUZET minor
70-0357-71 Takeoff and landing at 850shp - Increase of takeoff power Major
70-0359-71 Air inlet inertial separator actuator minor
70-0361-32 Landing gear wide washer minor
70-0364-25 Modified pylon upholstery minor
70-0369-25 Obsolescence of cabin lighting LED and lenses minor
70-0370-52 Wide door motor obsolescence minor
70-0372-33 Back lighted panels minor
70-0373-33 PL1 (Circuit breaker panel) lighting and label minor
70-0374-33 Servicing plugs minor
70-0375-28 Modification of MT40 fuel pressure sensor installation minor
70-0376-33 Pedestal lighting improvement minor
70-0379-23 Capability for future integration of the CPDLC (Controller Pilot Data Link
Communication) antenna minor
70-0381-31 M51 Hourmeter - Improvement of flight time calculation minor
70-0383-00 Software V14.01 - G1000 Integrated Flight Deck for TBM 850/900 Major
70-0384-77 TORQUE & IGNITION functions maintained during switching of S1 from
"NORMAL" position to "EMERGENCY" position minor
70-0385-23 AVIONICS MASTER and GROUND CLEARANCE architecture modification minor

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Rev. 1
Page 0.5B
CLASSIF.SUBJECTMOD70 No.
70-0393-25 Replacement of air circuit seal on pilot door minor
70-0400-28 Removal of MT40 transducer minor
70-0401-92 Illuminated push-buttons minor
70-0402-28 Fuel sequencer evolution minor
70-0403-24 Battery firewall modification minor
70-0404-57 Aileron trimming minor
NOTE
Optional modifications are integrated in the list of equipment - refer to the list of
equipment available in SOCATA Report reference NAV No. 34/90-RJ-App 2, located at the
end of this POH.

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Page 0.6
TABLE OF CONTENTS
SECTION
GENERAL 1
LIMITATIONS 2
EMERGENCY PROCEDURES 3
NORMAL PROCEDURES 4
PERFORMANCE 5
WEIGHT AND BALANCE 6
DESCRIPTION 7
AIRPLANE HANDLING, SERVICING AND MAINTENANCE 8
SUPPLEMENTS 9

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SECTION 1
GENERAL
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Rev. 1
Page 1.0.1
SECTION 1
GENERAL
TABLE OF CONTENTS
1.1 - GENERAL 1.1.1...................................................................
1.2 - THREE VIEW DRAWING 1.2.1......................................................
1.3 - DESCRIPTIVE DATA 1.3.1.........................................................
ENGINE 1.3.1..................................................................
PROPELLER 1.3.1..............................................................
FUEL 1.3.2.....................................................................
ENGINE OIL 1.3.3...............................................................
MAXIMUM CERTIFICATED WEIGHTS 1.3.3.......................................
STANDARD AIRPLANE WEIGHTS 1.3.3...........................................
CABIN AND ENTRY DIMENSIONS 1.3.4...........................................
SPECIFIC LOADINGS 1.3.4......................................................
1.4 - ABBREVIATIONS AND TERMINOLOGY 1.4.1........................................
METEOROLOGICAL TERMINOLOGY 1.4.1........................................
GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS 1.4.1.......................
POWER TERMINOLOGY 1.4.2...................................................
AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY 1.4.2.........
WEIGHT AND BALANCE TERMINOLOGY 1.4.2....................................
GENERAL ABBREVIATIONS 1.4.4................................................
RADIO - NAVIGATION ABBREVIATIONS 1.4.7.....................................
1.5 - CONVERSION FACTORS 1.5.1.....................................................
1.6 - PRESSURE AND STANDARD ATMOSPHERE 1.6.1...................................
STANDARD ATMOSPHERE 1.6.1.................................................
PRESSURE CONVERSION TABLE 1.6.2..........................................

PILOT’S OPERATING HANDBOOK
SECTION 1
GENERAL
Edition 0 -- October 31, 2013
Rev. 1
Page 1.1.1
1.1 - GENERAL
This Handbook contains 9 Sections, and includes the material required by FAR Part 23 to be furnished to the pilot
for operation of the TBM 900 airplane. It also contains supplemental data supplied by the manufacturer.
The ”GARMIN” G1000 Integrated Flight Deck Cockpit Reference Guide for the Socata TBM 900,
No. 190-00708-05, or any later version as applicable, must be permanently kept in the airplane with the Pilot's
Operating Handbook.
The Pilot's Guide for the Electronic Standby Indicator MODEL ESI-2000 P/N 0040-32500-01 Rev. E or any later
version as applicable, must be permanently kept in the airplane with the Pilot's Operating Handbook.
DepartureintoIMCisnotauthorizedifthebatterysymbolispresentwithanamberbatterysymbol(lessthan1hour
remaining), or an amber or red ”X” over the battery symbol or a ”CAL DUE” message by the battery symbol.
Section 1 provides basic data and information of general interest. It also contains definitions or explanations of
abbreviations and terminology commonly used.
The general for complex optional systems are given in Section 9, ”Supplements” of the Pilot's Operating
Handbook.

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GENERAL
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Rev. 1
Page 1.2.1
1.2 - THREE VIEW DRAWING
Figure 1.2.1 (1/2) - THREE VIEW DRAWING
* Airplane on level field with fully extended FWD shock-absorber

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Page 1.2.2
Figure 1.2.1 (2/2) - THREE VIEW DRAWING

PILOT’S OPERATING HANDBOOK
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GENERAL
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Rev. 1
Page 1.3.1
1.3 - DESCRIPTIVE DATA
ENGINE
Number of engines : 1
Engine manufacturer : PRATT & WHITNEY CANADA
Engine model number : PT6A - 66D
Engine type : Free turbine, reverse flow and 2 turbine sections
Compressor type : 4 axial stages
1 centrifugal stage
Combustion chamber type : Annular
Turbine type : 1 gas generator turbine stage
2 power turbines stages
Horsepower rating and propeller speed : 850 SHP at 2000 RPM
PROPELLER
Number of propellers : 1
Propeller manufacturer : HARTZELL
Propeller model number : HC-E4N-3 / E9083S (K)
Number of blades : 4
Propeller diameter :
Minimum : 90 inches (2.286 m)
Maximum : 91 inches (2.311 m)
Propeller type : Adjustable constant speed, with feathering and hydraulic control reverse
Propeller blade setting at 30 inches station
Low pitch : 21°
Feathering : 86°
Maximum reverse : - 11°
Propeller governor : 8210.007 WOODWARD

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FUEL
Total capacity : 301 USG (1140 Litres)
Total capacity each tank : 150.5 USG (570 Litres)
Total usable : 292 USG (1106 Litres)
CAUTION
THE USED FUEL MUST CONTAIN AN ANTI-ICE ADDITIVE, IN ACCORDANCE WITH
SPECIFICATION MIL-I-27686 or MIL-I-85470. ADDITIVE CONCENTRATIONS (EGME or
DIEGME) SHALL BE COMPRISED BETWEEN A MINIMUM OF 0.06 % AND A MAXIMUM OF
0.15 % BY VOLUME. REFER TO SECTION 8 ”HANDLING, SERVICING AND MAINTENANCE”
FOR ADDITIONAL INFORMATION.
CAUTION
THE USE OF AVIATION GASOLINE (AVGAS) MUST BE RESTRICTED TO EMERGENCY
PURPOSES ONLY. AVGAS SHALL NOT BE USED FOR MORE THAN 150 CUMULATIVE
HOURS DURING ANY PERIOD BETWEEN ENGINE OVERHAUL PERIODS
NOTE
Use of AVGAS to be recorded in engine module logbook
US Specification (US) French Specification (FR) English Specification (UK) NATO Code
ASTM-D1655 JET A
ASTM-D1655 JET A1
ASTM-D1655 JET B AIR 3405C Grade F35 DERD 2494 Issue 9 F35 without
additive
MIL-DTL-5624
Grade JP-4 AIR 3407B DERD 2454 Issue 4 Amdt 1 F40 with additive
MIL-DTL-5624
Grade JP-5 AIR 3404C Grade F44 DERD 2452 Issue 2 Amdt 1 F44 with additive when utilization
MIL-DTL-83133
Grade JP-8 AIR 3405C Grade F34 DERD 2453 Issue 4 Amdt 1 F34 with additive S748
AIR 3404C Grade F43 DERD 2498 Issue 7 F43 without
additive
Figure 1.3.1 - RECOMMENDED FUEL TYPES
(Reference : Service Bulletin P & W C. No. 14004)

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GENERAL
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Page 1.3.3
ENGINE OIL
System total capacity : 12.7 Quarts (12 Litres) (oil cooler included)
Usable capacity : 6 Quarts (5.7 Litres)
Maximum consumption : 0.14 qt / hr (0.13 l / hr)
[0.3 lb/hr (0.136 kg/h)]
CAUTION
DO NOT MIX DIFFERENT BRANDS OR TYPES
Nominal
Viscosity US Specification (US) French Specification (FR) English Specification (UK) NATO
Code
Type
5cSt MIL-L-23699C Amdt1 MIL-L-23699C Amdt1 DERD 2499 Issue 1 O.156
Figure 1.3.2 - RECOMMENDED ENGINE OIL TYPES
(Reference : Service Bulletin P & W C. No. 14001)
MAXIMUM CERTIFICATED WEIGHTS
Ramp : 7430 lbs (3370 kg)
Takeoff : 7394 lbs (3354 kg)
Landing : 7024 lbs (3186 kg)
Baggage weight
- refer to Section 2 (Paragraph 2.5) for weight and C.G. limits
- refer to Section 6 for cargo loading instructions
STANDARD AIRPLANE WEIGHTS
Standard empty weight : 4583 lbs (2079 kg)
Maximum useful load : 2811 lbs (1275 kg)

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CABIN AND ENTRY DIMENSIONS
Maximum cabin width : 3' 11.64” (1.21 m)
Maximum cabin length : 13' 3.45” (4.05 m)
Maximum cabin height : 4' (1.22 m)
Number of cabin entries : 1 (standard) + 1 ”pilot” door (if installed)
Entry width (standard) : 3' 6.52” (1.08 m)
Entry height (standard) : 3' 10.85” (1.19 m)
”Pilot” entry mean width : 2' 3.6” (0.70 m)
”Pilot” entry mean height : 3' 2.16” (0.97 m)
SPECIFIC LOADINGS
Wing loading : 38.16 lbs / sq.ft (186.3 kg / m2)
Power loading : 8.7 lbs / SHP (3.95 kg / SHP)

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1.4 - ABBREVIATIONS AND TERMINOLOGY
METEOROLOGICAL TERMINOLOGY
ISA : International standard atmosphere
OAT : Outside air temperature
SAT : Static air temperature
QFE : Atmospheric pressure at the airport reference point.
QNH : Atmospheric pressure at sea level, at airplane position.
NOTE
On the ground, the altimeter will indicate ”zero” if it is set to QFE ; it will indicate airport
altitude if it is set to QNH.
Standard Temperature :
Is15°C(59°F)atsealevelpressurealtitudeanddecreasesby2°C(3.6°F)foreach1000ftofaltitude.
Pressure altitude :
Is the altitude read from an altimeter when the altimeter's barometric scale has been set to
29.92 inches of mercury (1013.2 hPa).
GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS
KCAS : Knots Calibrated Airspeed is the indicated airspeed expressed in knots corrected for position
and instrument error. Knots calibrated airspeed is equal to KTAS in standard atmosphere at sea
level.
KIAS : Knots Indicated Airspeed is the speed shown on the airspeed indicator and expressed in knots.
KTAS : KnotsTrueAirspeedistheairspeedexpressedinknotsrelativetoundisturbed airwhichisKCAS
corrected for altitude and temperature.
VA:Maneuvering Speed is the maximum speed at which full or abrupt control movements may be
used.
VFE :Maximum Flap Extended Speed isthehighestspeedpermissiblewithwingflapsinaprescribed
extended position.
VLE :Maximum Landing Gear Extended Speed is the maximum speed at which an airplane can be
safely flown with the landing gear extended.
VLO :Maximum Landing Gear Operating Speed is the maximum speed at which the landing gear can
be safely extended or retracted.
VMO :Maximum Operating Speed is the speed limit that may not be deliberately exceeded in normal
flight operations.
VR:Rotation Speed is the speed at which rotation is initiated during takeoff to achieve takeoff safety
speed at screen height.
VSO :Stalling Speed or the minimum steady flight speed at which the airplane is controllable in the
landing configuration.
VS1 :Stalling Speed or the minimum steady flight speed obtained in a specific configuration.

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GENERAL
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Vx:Best Angle of Climb Speed is the airspeed which delivers the greatest gain of altitude in the
shortest possible horizontal distance.
VY:Best Rate of Climb Speed is the airspeed which delivers the greatest gain in altitude in the
shortest possible time.
POWER TERMINOLOGY
Recovery altitude :
Maximum altitude at which it is possible, in standard temperature, to maintain a specified power.
Overheated start :
Engine start or attempt to start which causes the interturbine temperature to be higher than the
maximum value permissible during start .
Flame out : Involuntary loss of the combustion chamber flame during operation.
GPU : Ground power unit.
Feathering : Action which reduces the drag of a propeller by positioning blades at the pitch angle allowing
minimal drag.
Maximum Cruise Power :
Power developed corresponding to outside (Flight Level and Temperature) conditions (Refer to
Chapter 5 ”PERFORMANCE”).
Ng : Gas generator RPM.
Np : Propeller rotation speed.
Reverse : Drag produced when the propeller blade setting is negative.
RPM : Revolutions per minute.
SHP : Shaft Horsepower.
TRQ : Torque.
AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY
Climb gradient :
Is the ratio of the change in height during a portion of climb, to the horizontal distance traversed in
thesametimeinterval.
Demonstrated crosswind velocity :
Isthevelocityofthecrosswindcomponentforwhichadequatecontroloftheairplaneduringtakeoff
and landing was actually demonstrated during certification tests. The value shown is not
considered to be limiting.
g:Is acceleration due to gravity.
Usable fuel : Total fuel which can be effectively consumed by the engine.
WEIGHT AND BALANCE TERMINOLOGY
Reference datum :
Datumperpendiculartothelongitudinalairplanecenterlinefromwhichalldistancesaremeasured
for balance purpose.

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Arm : Is the distance from the reference datum to the center of gravity (C.G.) of an item.
Moment : Is the product of the weight of an item multiplied by its arm.
Center of gravity (C.G.) :
Airplanebalancepoint.Itsdistancefrom thereferencedatumisfoundbydividingthetotalmoment
by the total weight of the airplane.
C.G. limits : CenterofGravityLimitsaretheextremecenterofgravitylocationswithinwhichtheairplanemust
be operated at a given weight.
Standard empty weight :
Weight of a standard airplane including unusable fuel and full operating fluids (oil and hydraulic
fluids).
Basic empty weight :
Standard empty weight plus optional equipment.
Useful load : Is the difference between maximum ramp weight and the basic empty weight.
Maximum ramp weight :
Isthe maximum weight approvedforgroundmaneuver.(Itincludestheweightofstart,taxiandrun
up fuel).
Maximum takeoff weight :
Is the maximum weight approved at the beginning of the takeoff run.
Maximum landing weight :
Is the maximum weight approved for landing touchdown.

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GENERAL ABBREVIATIONS
A:Ampere or Amber
ADC : Air Data Computer
AGL : Above ground level
ALT. SEL. : Altitude selector
ALTI : Altimeter
AMP. : Ampere
AP : Autopilot
AUTO SEL : Automatic selector
AUX BP : Auxiliary boost pump
BAT : Battery
BAT OVERHEAT: Battery overheat (only with Cadmium-Nickel battery)
BRT : Brightness
CAS : Crew Alerting System
°C:Celsius degree
CHiPS : Cable Harness Protection System
CONT. : Control
DIEGME : Diethylene glycol monomethyl ether
DISC : Disconnect
DN : Down
ECS : Environmental control system
EGME : Ethylene glycol monomethyl ether
EMER : Emergency
ENCOD. ALTI : Encoding altimeter
ESHP : Estimated shaft horsepower
ESS. BUS TIE : Essential BUS tie
EXT. LIGHTS : Exterior lightings
°F:Fahrenheit degree
FCU : Fuel control unit
FIRE EXTING : Fire extinguisher
FL : Flight level
FOB : Fuel On Board
FPL : Flight Plan
ft : Feet
ft/min : Feet per minute
G:Green
HI : High
HP : High pressure
hPa : Hectopascal
hr : Hour
HTR : Heater
IGNIT : Ignition
in : Inch
INERT SEP : Inertial separator
INDIC : Indicator
in.Hg : Inch of mercury
INT. LIGHTS : Interior lightings
INSTR. : Instrument
ITT : Interturbine temperature
kg : Kilogram
kt : Knot (1 nautical mile/hr - 1852 m/hr)
kW :Kilowatt

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l:Litre
L:Left
l/h : Litre / hour
lb or lbs : Pound(s)
L/D : Lift-to-drag
LDG : Landing
LDG GR : Landing gear
LFE : Landing Field Elevation
LRCR : Long Range Cruise
LO : Low
LP : Low pressure
LRN : Long range navigation
LTS TEST : Lightings test
m:Metre
m.a.c. : Mean aerodynamic chord
MAIN GEN : Main generation
MAN : Manual
MAN OVRD : Manual override
MAX RPM : Maximum revolutions per minute
MFD : Multi-function Display
MIN : Minimum
min : Minute
mm : Millimetre
MLW : Maximum Landing Weight
MRW : Maximum Ramp Weight
MTOW : Maximum Takeoff Weight
MXCR : Maximum Cruise
MZFW : Maximum Zero Fuel Weight
NM : Nautical mile
NOCR : Normal cruise (recommended)
NORM : Normal
PFD : Primary Flight Display
PHF : Plan Horizontal Fixe (Horizontal stabilizer)
PRESS : Pressure
PROP : Propeller
psi : Pounds per square inch
qt : Quart (¼USG)
QTY : Quantity
R:Red or Right
RUD : Rudder
sorsec : Second
SEL : Selector
SIG : Signalization
SL : Sea level
S/N : Serial number
SPKR : Speaker
ST - BY : Stand-by
STALL HTR : Stall heater
Std : Standard
T°:Temperature
TEMP : Temperature
TO : Takeoff
TURN COORD : Turn coordinator

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USG : Gallon U.S
V:Volt or Voltage
WARN : Warning
W/S : Windshield

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RADIO - NAVIGATION ABBREVIATIONS
ADF : Automatic Direction Finder System
ADI : Attitude Director Indicator
AFCS : Automated Flight Control System
AHRS : Attitude and Heading Reference System
ATC : Transponder
B RNAV : Basic aRea NAVigation
CDI : Course Deviation Indicator
COM : Communications Transceivers
DME : Distance Measuring Equipment
ELT : Emergency Locator Transmitter
ESI : Electronic Standby Instrument
FMS : Flight Management System
GPS : Ground Positioning System
HF : High Frequency
IFR : Instrument Flight Rules
ILS : Instrument Landing System
IMC : Instrument Meteorological Conditions
LNAV : Lateral NAVigation
LPV : Localizer Precision Vertical
MKR : Marker Radio Beacon
NAV : Navigation Indicators or Receivers
P RNAV : Precision aRea NAVigation
RNAV : Area NAVigation
RNP : Required Navigation Performance
TAS : Traffic Advisory System
TAWS : Terrain Awareness Warning System
VFR : Visual Flight Rules
VHF : Very High Frequency
VMC : Visual Meteorological Conditions
VNAV : Vertical NAVigation
VOR : VHF Omnidirectional Range
VOR / LOC : VHF Omnidirectional Range LOCalizer
WAAS : Wide Area Augmentation System
WXR : Weather surveillance radar
XPDR : Transponder

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1.5 - CONVERSION FACTORS
IMPERIAL AND U.S UNITS TO
METRIC UNITS METRIC UNITS TO IMPERIAL AND U.S UNITS
MULTIPLY BY TO OBTAIN MULTIPLY BY TO OBTAIN
FEET 0.3048 METRE METRE 3.2808 FEET
INCH 25.4 mm mm 0.03937 INCH
Imp.Gal 4.546 Litre Litre 0.220 Imp.Gal
USG 3.785 Litre Litre 0.264 USG
lb 0.45359 kg kg 2.2046 lb
Figure 1.5.1 - IMPERIAL AND U.S UNITS TO METRIC UNITS