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Daher TBM 700 Pilot's Information Manual

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INFORMATION MANUAL

THIS INFORMATION MANUAL IS A NON---OFFICIAL COPY OF THE PILOT'S

OPERATING HANDBOOK AND MAY BE USED FOR GENERAL INFORMATION

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 lists of effective pages in this manual correspond to those 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 maintained.

It must not be used for any purpose other than that for which it is supplied, nor may

information contained in it be disclosed to unauthorized persons. It must not be

reproduced nor transmitted in any form in whole or in part without permission in

Information in this document is subject to change without notice.



For any information concerning this document, please contact :

DAHER AEROSPACE

Customer Care

65921 TARBES CEDEX 9 - FRANCE

March 25, 2019 --- Rev. 16

PIM - DO NOT USE FOR FLIGHT OPERATIONS

TBM 700

Versions A and B

PILOT'S

CAUTION

PURPOSES ONLY.

Pilot's Operating Handbook.

writing from the owners of the Copyright.

2019 - - DAHER AEROSPACE - - All rights reserved

Printed in FRANCE

P/N : T00.DMAPIPYE

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Summary of Contents for Daher TBM 700

Page 1 The lists of effective pages in this manual correspond to those 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 T B M SECTION 0 PILOT’S OPERATING HANDBOOK TABLE OF CONTENTS SECTION GENERAL LIMITATIONS EMERGENCY PROCEDURES NORMAL PROCEDURES PERFORMANCE WEIGHT AND BALANCE DESCRIPTION AIRPLANE HANDLING, SERVICING AND MAINTENANCE SUPPLEMENTS Page 0.6 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 3 T B M SECTION 0 PILOT’S OPERATING HANDBOOK LIST OF EFFECTIVE PAGES AND VALIDITIES ORIGINAL ISSUE OF JANUARY 31, 1990 From S/N 1 thru S/N 243, except S/N 205 and 240 P/N Z00.DMAFM00EE0R16EN (*) Refer to the validities below in order to perform a personalization of your Manual : (a) : Specific pages for aircraft, which have not received the modification No.
Page 4 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 0.60 2.4.2 3.3.3 2.5.1 3.3.4 2.5.2 3.3.5 1.0.1 1.0.2 2.6.1 3.3.6 1.1.1 2.6.2 3.3.7 2.6.3 3.3.8 1.1.2 1.2.1 2.6.4 3.3.9 1.2.2 2.6.5 3.3.10 1.2.3 2.6.6 3.3.11 1.2.4 2.6.7 3.3.12 1.3.1 2.6.8 3.4.1 1.3.2 2.7.1 3.4.2...
Page 5 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 3.9.7 4.3.8 4.4.6 3.9.8 4.3.9 4.4.7 3.10.1 4.3.10 4.4.8 3.10.2 4.3.11 4.4.9 3.10.3 4.3.12 4.4.10 3.10.4 4.3.13 4.4.11 3.10.5 4.3.14 4.4.12 3.10.6 4.3.15 4.4.13 * 3.11.1 (a) 4.3.16 4.4.14 * 3.11.2 (a) 4.3.17 4.4.15 * 3.11.1 (b)
Page 6 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 4.4.48 4.5.22 5.10.3 * 4.4.49 (a) 16 4.5.23 5.10.4 * 4.4.50 (a) 16 4.5.24 5.10.5 * 4.4.49 (b) 16 4.5.25 5.10.6 * 4.4.50 (b) 16 4.5.26 5.10.7 4.4.51 5.10.8 4.4.52 5.0.1 5.10.9 4.4.53 5.0.2 5.10.10...
Page 7 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 6.4.6 6.5.24 7.0.1 6.4.7 6.5.25 7.0.2 6.4.8 6.5.26 7.0.3 6.4.9 6.5.27 7.0.4 6.4.10 6.5.28 7.1.1 6.4.11 6.5.29 7.1.2 6.4.12 6.5.30 7.2.1 6.4.13 6.5.31 7.2.2 6.4.14 6.5.32 7.2.3 6.4.15 6.5.33 7.2.4 6.4.16 6.5.34 7.2.5 6.4.17 6.5.35...
Page 8 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 7.3.19D 7.5.7 7.8.5 7.3.19E 7.5.8 7.8.6 7.3.19F 7.5.9 7.8.7 7.3.19G 7.5.10 7.8.8 7.3.19H 7.5.11 7.8.9 7.3.20 7.5.12 7.8.9A 7.3.21 7.6.1 7.8.9B 7.3.22 7.6.2 7.8.9C 7.3.22A 7.6.3 7.8.9D 7.3.22B 7.6.4 7.8.10 7.3.23 7.6.5 7.8.11 7.3.24 7.6.6...
Page 9 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 7.9.9 8.3.1 7.9.10 8.3.2 7.10.1 8.4.1 7.10.2 8.4.2 7.10.3 8.5.1 7.10.4 8.5.2 7.10.5 8.6.1 7.10.6 8.6.2 7.11.1 8.6.3 7.11.2 8.6.4 7.11.3 8.6.5 7.11.4 8.6.6 7.12.1 8.7.1 7.12.2 8.7.2 7.12.3 8.7.3 7.12.4 8.7.4 7.12.5 8.7.5 7.12.6...
Page 10 T B M SECTION 0 PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 0.60 Rev. 16 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 11 T B M SECTION 0 PILOT’S OPERATING HANDBOOK LIST OF EFFECTIVE PAGES AND VALIDITIES NOTE : Bold- -faced and italic types are used for ”U.S.” specific pages. ORIGINAL ISSUE OF JANUARY 31, 1990 From S/N 1 thru S/N 243, except S/N 205 and 240 P/N Z00.DMAFM00EE0R16US (*) Refer to the validities below in order to perform a personalization of your Manual :...
Page 12 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 2.3.3 3.3.1 0.60 2.3.4 3.3.2 0.61 0.62 2.4.1 3.3.3 2.4.2 3.3.4 0.63 0.64 2.5.1 3.3.5 2.5.2 3.3.6 1.0.1 2.6.1 3.3.7 1.0.2 2.6.2 3.3.8 1.1.1 2.6.3 3.3.9 1.1.2 2.6.4 3.3.10 1.2.1 2.6.5 3.3.11 1.2.2 2.6.6 3.3.12...
Page 13 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 3.9.5 4.3.6 4.4.4 3.9.6 4.3.7 4.4.5 3.9.7 4.3.8 4.4.6 3.9.8 4.3.9 4.4.7 3.10.1 4.3.10 4.4.8 3.10.2 4.3.11 4.4.9 3.10.3 4.3.12 4.4.10 3.10.4 4.3.13 4.4.11 3.10.5 4.3.14 4.4.12 3.10.6 4.3.15 4.4.13 * 3.11.1 (a) 4.3.16 4.4.14 * 3.11.2 (a)
Page 14 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 4.4.46 4.5.20 5.10.1 4.4.47 4.5.21 5.10.2 4.4.48 4.5.22 5.10.3 * 4.4.49 (a) 16 4.5.23 5.10.4 * 4.4.50 (a) 16 4.5.24 5.10.5 * 4.4.49 (b) 16 4.5.25 5.10.6 * 4.4.50 (b) 16 4.5.26 5.10.7 4.4.51 5.10.8...
Page 15 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 6.4.4 6.5.22 6.5.64 6.4.5 6.5.23 6.5.65 6.4.6 6.5.24 6.4.7 6.5.25 7.0.1 6.4.8 6.5.26 7.0.2 6.4.9 6.5.27 7.0.3 6.4.10 6.5.28 7.0.4 6.4.11 6.5.29 7.1.1 6.4.12 6.5.30 7.1.2 6.4.13 6.5.31 7.2.1 6.4.14 6.5.32 7.2.2 6.4.15 6.5.33 7.2.3...
Page 16 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 7.3.19A 7.5.4 7.8.2 7.3.19B 7.5.5 7.8.3 7.3.19C 7.5.6 7.8.4 7.3.19D 7.5.7 7.8.5 7.3.19E 7.5.8 7.8.6 7.3.19F 7.5.9 7.8.7 7.3.19G 7.5.10 7.8.8 7.3.19H 7.5.11 7.8.9 7.3.20 7.5.12 7.8.9A 7.3.21 7.6.1 7.8.9B 7.3.22 7.6.2 7.8.9C 7.3.22A 7.6.3...
Page 17 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 7.9.6 8.2.1 7.9.7 8.2.2 7.9.8 8.3.1 7.9.9 8.3.2 7.9.10 8.4.1 7.10.1 8.4.2 7.10.2 8.5.1 7.10.3 8.5.2 7.10.4 8.6.1 7.10.5 8.6.2 7.10.6 8.6.3 7.11.1 8.6.4 7.11.2 8.6.5 7.11.3 8.6.6 7.11.4 8.7.1 7.12.1 8.7.2 7.12.2 8.7.3 7.12.3...
Page 18 T B M SECTION 0 PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Rev. 16 Page 0.64 U.S. Version PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 19 T B M SECTION 0 PILOT’S OPERATING HANDBOOK LIST OF EFFECTIVE PAGES AND VALIDITIES NOTE : Bold- -faced and italic types are used for ”BRAZIL” specific pages. ORIGINAL ISSUE OF JANUARY 31, 1990 From S/N 1 thru S/N 243, except S/N 205 and 240 P/N Z00.DMAFM00EE0R16BZ (*) Refer to the validities below in order to perform a personalization of your Manual :...
Page 20 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 2.4.1 3.3.2 0.57 2.4.2 3.3.3 0.58 2.5.1 3.3.4 1.0.1 2.5.2 3.3.5 1.0.2 2.6.1 3.3.6 1.1.1 2.6.2 3.3.7 1.1.2 2.6.3 3.3.8 1.2.1 2.6.4 3.3.9 1.2.2 2.6.5 3.3.10 1.2.3 2.6.6 3.3.11 1.2.4 2.6.7 3.3.12 1.3.1 2.6.8 3.4.1...
Page 21 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 3.9.6 4.3.7 4.4.5 3.9.7 4.3.8 4.4.6 3.9.8 4.3.9 4.4.7 3.10.1 4.3.10 4.4.8 3.10.2 4.3.11 4.4.9 3.10.3 4.3.12 4.4.10 3.10.4 4.3.13 4.4.11 3.10.5 4.3.14 4.4.12 3.10.6 4.3.15 4.4.13 * 3.11.1 (a) 4.3.16 4.4.14 * 3.11.2 (a) 4.3.17 4.4.15...
Page 22 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 4.4.47 4.5.21 5.10.2 4.4.48 4.5.22 5.10.3 * 4.4.49 (a) 16 4.5.23 5.10.4 * 4.4.50 (a) 16 4.5.24 5.10.5 * 4.4.49 (b) 16 4.5.25 5.10.6 * 4.4.50 (b) 16 4.5.26 5.10.7 4.4.51 5.10.8 4.4.52 5.0.1 5.10.9...
Page 23 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 6.4.5 6.5.23 6.4.6 6.5.24 7.0.1 6.4.7 6.5.25 7.0.2 6.4.8 6.5.26 7.0.3 6.4.9 6.5.27 7.0.4 6.4.10 6.5.28 7.1.1 6.4.11 6.5.29 7.1.2 6.4.12 6.5.30 7.2.1 6.4.13 6.5.31 7.2.2 6.4.14 6.5.32 7.2.3 6.4.15 6.5.33 7.2.4 6.4.16 6.5.34 7.2.5...
Page 24 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 7.3.19C 7.5.6 7.8.4 7.3.19D 7.5.7 7.8.5 7.3.19E 7.5.8 7.8.6 7.3.19F 7.5.9 7.8.7 7.3.19G 7.5.10 7.8.8 7.3.19H 7.5.11 7.8.9 7.3.20 7.5.12 7.8.9A 7.3.21 7.6.1 7.8.9B 7.3.22 7.6.2 7.8.9C 7.3.22A 7.6.3 7.8.9D 7.3.22B 7.6.4 7.8.10 7.3.23 7.6.5...
Page 25 T B M SECTION 0 PILOT’S OPERATING HANDBOOK 7.9.8 8.3.1 7.9.9 8.3.2 7.9.10 8.4.1 7.10.1 8.4.2 7.10.2 8.5.1 7.10.3 8.5.2 7.10.4 8.6.1 7.10.5 8.6.2 7.10.6 8.6.3 7.11.1 8.6.4 7.11.2 8.6.5 7.11.3 8.6.6 7.11.4 8.7.1 7.12.1 8.7.2 7.12.2 8.7.3 7.12.3 8.7.4 7.12.4 8.7.5 7.12.5...
Page 26 T B M SECTION 0 PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Rev. 16 Page 0.58 BRAZIL PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 27 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK SECTION 1 GENERAL TABLE OF CONTENTS Page GENERAL 1.1.1 ..........THREE VIEW DRAWING 1.2.1 .
Page 28 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 1.0.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 29 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 700 airplane. It also contains supplemental data supplied by the manufacturer.
Page 30 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 1.1.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 31 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK 1.2 - - THREE VIEW DRAWING * Airplane on line of flight with extended FWD shock--absorber Figure 1.2.1 (1 / 2) -- THREE VIEW DRAWING -- TBM700A Rev. 7 Page 1.2.1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 32 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK Figure 1.2.1 (2 / 2) -- THREE VIEW DRAWING -- TBM700A Rev. 13 Page 1.2.2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 33 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK * Airplane on line of flight with extended FWD shock--absorber Figure 1.2.1A (1 / 2 ) -- THREE VIEW DRAWING -- TBM700B Rev. 7 Page 1.2.3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 34 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK Figure 1.2.1A (2 / 2 ) -- THREE VIEW DRAWING -- TBM700B Rev. 13 Page 1.2.4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 35 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK 1.3 - - DESCRIPTIVE DATA ENGINE Number of engines : 1 Engine manufacturer : PRATT & WHITNEY CANADA Engine model number : PT6A -- 64 Engine type : Free turbine, reverse flow and 2 turbine sections Compressor type : 4 axial stages 1 centrifugal stage...
Page 36 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK FUEL Total capacity : 290.6 us gal (1100 Litres) Total capacity each tank : 145.3 us gal (550 Litres) Total usable : 281.6 us gal (1066 Litres) CAUTION THE USED FUEL MUST CONTAIN AN ANTI- -ICE ADDITIVE, IN ACCORDANCE WITH SPECIFICATION MIL- -I- -27686 or MIL- -I- -85470.
Page 37 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK ENGINE OIL System total capacity : 12.7 Quarts (12 Litres) (oil cooler included) Usable capacity : 6 Quarts (5.7 Litres) Maximum consumption in 10 hour period : 0.14 qt / hr (0.13 l / hr) [0.3 lb / hr (136 cc / hr)] Specification Nominal...
Page 38 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK MAXIMUM CERTIFICATED WEIGHTS Ramp : 6614 lbs (3000 kg) Takeoff : 6579 lbs (2984 kg) Landing : 6250 lbs (2835 kg) Baggage weight (refer to Section 6 for cargo loading instructions) : In FWD compartment (non pressurized) : 110 lbs (50 kg) In aft compartment (pressurized) : 220 lbs (100 kg) STANDARD AIRPLANE WEIGHTS...
Page 39 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK 1.4 - - ABBREVIATIONS AND TERMINOLOGY METEOROLOGICAL TERMINOLOGY International standard atmosphere Outside air temperature is the free air static temperature. It is expressed in either degrees Celsius or degrees Fahrenheit. Static air temperature IOAT Indicated outside air temperature Atmospheric pressure at the airport reference point.
Page 40 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK Maneuvering Speed is the maximum speed at which full or abrupt control movements may be used. Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position. Maximum Landing Gear Extended Speed is the maximum speed at which an airplane can be safely flown with the landing gear extended.
Page 41 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK 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 .
Page 42 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY Climb gradient : Is the ratio of the change in height during a portion of climb, to the horizontal distance traversed in the same time interval. Demonstrated crosswind velocity : Is the velocity of the crosswind component for which adequate control of the airplane during takeoff and landing...
Page 43 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK C.G. limits : Center of Gravity Limits are the extreme center of gravity locations within which the airplane must 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).
Page 44 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK GENERAL ABBREVIATIONS : Ampere or Amber : Air Data Computer AIL TRIM : Aileron trim ALT. SEL. : Altitude selector ALTI : Altimeter AMP. : Ampere : Autopilot AUTO SEL : Automatic selector AUX BP : Auxiliary boost pump : Battery...
Page 45 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK INDIC : Indicator in.Hg : Inch of mercury INT. LIGHTS : Interior lightings INSTR. : Instrument IRCR : Intermediate range cruise : Interturbine temperature : Kilogram : Knot (1 nautical mile/hr -- 1852 m/hr) : Kilowatt : Litre : Left...
Page 46 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK PROP : Propeller : Pounds per square inch : Quart (¼ us gal) : Quantity : Red or Right : Rudder s or sec : Second : Selector : Signalization : Sea level : Serial number SPKR : Speaker...
Page 47 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK RADIO - - NAVIGATION ABBREVIATIONS : Automatic Direction Finder System : Attitude Director Indicator : Transponder : Course Deviation Indicator : Communications Transceivers : Distance Measuring Equipment : Emergency Locator Transmitter : High Frequency : Horizontal Situation Indicator : Instrument Flight Rules...
Page 48 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK EFIS ABBREVIATIONS ATTITUDE FAIL: Attitude failure CMPST : Composite (EFIS composite mode ) : Control Panel : Course : Display Unit : Flight director EADI : Electronic Attitude Deviation Indicator EFIS : Electronic Flight Instrument System EHSI : Electronic Horizontal Situation Indicator...
Page 49 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK 1.5 - - CONVERSION FACTORS IMPERIAL AND U.S UNITS TO METRIC UNITS TO IMPERIAL AND METRIC UNITS U.S UNITS MULTIPLY TO OBTAIN MULTIPLY TO OBTAIN FEET 0.3048 METRE METRE 3.2808 FEET INCH 25.4 0.03937...
Page 50 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK Feet 30000 20000 10000 Mètres 2500 5000 7500 10000 Figure 1.5.2 -- FEET VERSUS METRES Page 1.5.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 51 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK 1000 Figure 1.5.3 -- INCHES VERSUS MILLIMETRES Rev. 2 Page 1.5.3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 52 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK 8000 6000 4000 2000 1000 2000 3000 4000 Figure 1.5.4 -- POUNDS VERSUS KILOGRAMS Page 1.5.4 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 53 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK 1.6 - - PRESSURE AND STANDARD ATMOSPHERE STANDARD ATMOSPHERE Pressure Pressure altitude °C °F (hPa) (ft) 1013.2 + 15.0 + 59.0 2000 942.1 + 11.0 + 51.8 4000 875.0 + 44.6 6000 811.9 + 37.6...
Page 54 T B M SECTION 1 GENERAL PILOT’S OPERATING HANDBOOK PRESSURE CONVERSION TABLE NOTE : The standard pressure of 1013.2 hPa is equal to 29.92 inches of mercury. 28.08 28.11 28.14 28.17 28.20 28.23 28.26 28.29 28.32 28.05 28.35 28.38 28.41 28.44 28.47 28.50...
Page 55 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved SECTION 2 LIMITATIONS TABLE OF CONTENTS Page GENERAL 2.1.1 ........... AIRSPEED LIMITATIONS 2.2.1 .
Page 56 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved TABLE OF CONTENTS (Continued) Page MISCELLANEOUS LIMITS 2.7.1 ....... . . 2.7.1 SEATING LIMITS C.G.
Page 57 EASA Approved 2.1 - - GENERAL The TBM 700 airplane 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 Pilot’s Operating Handbook.
Page 58 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 13 Page 2.1.2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 59 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved 2.2 - - AIRSPEED LIMITATIONS Airspeed limitations and their operational significance are shown in Figure 2.2.1. KCAS KIAS SPEED REMARKS Do not intentionally exceed Maximum operating speed this speed in normal flight category Do not make abrupt or full Maneuvering speed...
Page 60 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 13 Page 2.2.2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 61 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved 2.3 - - POWERPLANT LIMITATIONS ENGINE Number of engines : 1 Engine manufacturer : PRATT & WHITNEY CANADA Engine model number : PT6A -- 64 Engine operating limits for takeoff and continous operations : Maximum power : -- 700 SHP : MAX TRQ 100 % at Np = 2000 RPM...
Page 62 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved Oil grade (Specification) : French English Nominal US specification NATO specification specification viscosity (US) code (FR) (UK) MIL--L--23699C MIL--L--23699C DERD 2499 Type 5cSt O.156 Amdt 1 Amdt 1 Issue 1 Figure 2.3.1 -- ENGINE OIL RECOMMENDED TYPE (Reference : Service Bulletin P &...
Page 63 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved NOTE : Use of AVGAS to be recorded in engine module logbook. CAUTION MAXIMUM TIME FOR SIDESLIP CONDITION IS 30 SECONDS. English US Specification French Specification Specification NATO Code (US) (FR) (UK)
Page 64 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 13 Page 2.3.4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 65 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved 2.4 - - STARTER OPERATION LIMITS Starter operation sequence is limited as follows : if Ng ≤ 30 % ......... . . 30 seconds if Ng >...
Page 66 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 13 Page 2.4.2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 67 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved 2.5 - - WEIGHT AND C.G. LIMITS WEIGHT LIMITS Maximum ramp weight (MRW) : 6614 lbs (3000 kg) Maximum takeoff weight (MTOW) : 6579 lbs (2984 kg) Maximum landing weight (MLW) : 6250 lbs (2835 kg) Maximum zero fuel weight in wings (MZFW) : 6001 lbs (2722 kg) Maximum baggage weight in FWD compartment (non pressurized) : 110 lbs (50 kg)
Page 68 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 13 Page 2.5.2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 69 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved 2.6 - - OPERATION LIMITS MANEUVER LIMITS This airplane is certified in the normal category. The normal category is applicable to airplanes intended for non--aerobatic operations. Non--aerobatic operations include any maneuvers incidental to normal flying, stalls (except whip stalls), lazy eights, chandelles, and steep turns in which the angle of bank is no more than 60°.
Page 70 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved SEVERE ICING CONDITIONS WARNING SEVERE ICING MAY RESULT FROM ENVIRONMENTAL CONDITIONS OUTSIDE OF THOSE FOR WHICH THE AIRCRAFT IS CERTIFICATED. FLIGHT IN FREEZING RAIN, FREEZING DRIZZLE, OR MIXED ICING CONDITIONS (SUPERCOOLED LIQUID WATER AND ICE CRYSTALS) MAY RESULT IN ICE BUILD- -UP ON PROTECTED SURFACES EXCEEDING THE CAPABILITY OF THE ICE PROTECTION SYSTEM,...
Page 71 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved FLAP OPERATING ENVELOPE The use of flaps is not authorized above 15 000 ft. REVERSE UTILIZATION The use of control reverse BETA (β) range is prohibited : -- during flight, -- on ground, if the engine is not running.
Page 72 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved EQUIPMENT REQUIRED DEPENDING ON TYPE OF OPERATION The airplane is approved for day & night VFR and day & night IFR operations when appropriate equipment is installed and operating correctly. The type certification for each use requires the following equipment.
Page 73 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved Day VFR 1) Pilot instruments -- Airspeed indicator -- Sensitive and adjustable altimeter -- Magnetic compass with built--in compensator 2) Warning lights -- Oil pressure -- Low fuel pressure -- Fuel selector OFF -- Fuel auxiliary pump ON -- L.H.
Page 74 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved 5) Various indicators -- Fuel gauge indicators (2) -- Fuel pressure indicator -- Voltmeter -- Ammeter -- Outside air temperature 6) Installations -- Fuel mechanical pump (main) -- Fuel electrical pump (auxiliary) -- Fuel shut--off valve -- Fuel timer -- Starter generator...
Page 75 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved Night VFR 1) All equipment required for day VFR 2) Attitude display indicator 3) Instrument lighting 4) Instrument panel lighting 5) Emergency lighting 6) Vertical speed indicator 7) Navigation lights (4) 8) Anticollision lights (2) 9) Landing light 1) All equipment required for day VFR...
Page 76 RVSM Operational Approval is required by an ICAO Regional Navigation Agreement. NOTE : Only altimeters AM250 are compliant with TBM 700 operation in RVSM area. IN- -FLIGHT CIRCUIT BREAKER USE LIMITS A tripped circuit breaker should not be reset in flight unless deemed necessary for continued safe flight and landing.
Page 77 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved 2.7 - - MISCELLANEOUS LIMITS SEATING LIMITS C.G. From 1 to 6 seats : -- 2 seats at 180.5 inches (4.585 m) -- 2 seats at 219.1 inches (5.565 m) } see NOTE 1 -- 2 seats at 259.3 inches (6.585 m) -- 2 seats at 180.5 inches (4.585 m)
Page 78 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 13 Page 2.7.2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 79 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved 2.8 - - MARKINGS AIRSPEED INDICATOR Airspeed indicator markings and their color code significance are shown in Figure 2.8.1. KIAS MARKING SIGNIFICANCE (Value or range) White arc 60 -- 122 Full Flap Operating Range Lower limit is maximum weight in landing configuration.
Page 80 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved ENGINE INSTRUMENTS Engine instrument markings and their color code significance are shown in Figure 2.8.3. Yellow Line or Line or arc Green Arc Red Line INSTRUMENT Minimum Caution Normal Maximum Limit Range...
Page 81 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved 2.9 - - PLACARDS (1) Under L.H. front side window -- Valid S / N 1 to 23, 25, 28, 33 and 35, except airplanes equipped retrofit with modification Nr MOD 70--019--25 : ICING CONDITIONS ALLOWED FLIGHT CONDITIONS : DAY AND NIGHT VFR AND IFR...
Page 82 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (2) Calibration chart on compass and on windshield post WARNING Steer TURN L AND R WINDSHIELD DE- -ICE OFF BEFORE Steer COMPASS READING DATE : RADIO ON (3) On rear baggage compartment bottom bulkhead (pressurized) 100 kg - - 220 lbs MAXIMUM IT IS THE PILOT’S RESPONSIBILITY TO CHECK THAT ALL THE BAGGAGES ARE...
Page 83 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (5) TBM700A Under radio rack, in front of pedestal Rev. 13 Page 2.9.3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 84 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (5) TBM700B Under radio rack, in front of pedestal Rev. 13 Page 2.9.4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 85 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (6) On fuel selector (7) Near fuel tank caps Rev. 13 Page 2.9.5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 86 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (8) On internal face of L.H. engine cowling Oil system capacity 12 l 12.7 qt (9) On R.H. side, at front seat level and under seating of intermediate and rear passenger seats, which are fitted with oxygen EMERGENCY OXYGEN IN DRAWER UNDER SEAT ;...
Page 87 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (12) Under R.H. control wheel (13) On nose gear door (14) On nose gear leg NOSE LANDING GEAR TIRE PRESSURE : 6,5 bar 94 psi Rev. 13 Page 2.9.7 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 88 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (15) On main gear leg MAIN LANDING GEAR TIRE PRESSURE : 8,25 bar 120 psi (16) On engine cowling, in front of baggage compartment door EXTERNAL POWER 28 VOLTS D.C. NOMINAL 800 AMPS STARTING CAPACITY MIN DO NOT EXCEED 1400 AMPS...
Page 89 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (17) TBM700B On access door -- External side (18) TBM700B On outer fuselage skin aft of access door and in the cabin forward of access door Rev. 13 Page 2.9.9 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 90 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (19) TBM700A from S / N 1 to S / N 49, except airplanes equipped as a retrofit with modification No. MOD70--019--25 On access door -- Internal side (19) TBM700A from S / N 50, plus airplanes equipped as a retrofit with modification No.
Page 91 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (19) TBM700B On access door -- Internal side (19) TBM700B On ”pilot” door -- Internal side (if installed) Rev. 13 Page 2.9.11 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 92 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (20) From S / N 1 to 23, 25, 28, 33 and 35, except airplanes equipped as a retrofit with modification No. MOD 70--019--25 On emergency exit handle Rev. 13 Page 2.9.12 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 93 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (20) From S / N 24, 26, 27, 29 to 32, 34, 36 to 9999, plus airplanes equipped as a retrofit with modification No. MOD 70--019--25 On emergency exit handle Marking on cover Marking on handle Rev.
Page 94 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (21) TBM700A, TBM700B On last step of stairs STAIRS MAX LOAD : ONE PERSON (22) TBM700B On R.H. access door jamb DO NOT USE HAND RAIL TO RETRACT OR STOW STAIRS (23) On internal face of L.H.
Page 95 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved Post--MOD70--0391--26D (25) On R.H. side at front seat level (26) On the lower drawer of the R.H. cabinet Rev. 15 Page 2.9.15 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 96 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Page 2.9.16 Rev. 15 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 97 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved 2.9 - - PLACARDS (1) Under L.H. front side window -- Valid S / N 1 to 23, 25, 28, 33 and 35, except airplanes equipped retrofit with modification Nr MOD 70--019--25 : ICING CONDITIONS ALLOWED FLIGHT CONDITIONS : DAY AND NIGHT VFR AND IFR...
Page 98 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (2) Calibration chart on compass and on windshield post WARNING Steer TURN L AND R WINDSHIELD DE- -ICE OFF BEFORE Steer COMPASS READING DATE : RADIO ON (3) On rear baggage compartment bottom bulkhead (pressurized) (4) On FWD baggage compartment door frame (non pressurized) 50 KG MÁXIMO PARA INSTRUÇÕES DE CARREGAMENTO...
Page 99 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (5) TBM700A Under radio rack, in front of pedestal Rev. 13 Page 2.9.3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 100 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (5) TBM700B Under radio rack, in front of pedestal Page 2.9.4 Rev. 13 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 101 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (6) On fuel selector (7) Near fuel tank caps Rev. 13 BRAZIL Page 2.9.5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 102 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (8) On internal face of L.H. engine cowling Capacidade de óleo 12 l 12,7 qt (9) On R.H. side, at front seat level and under seating of intermediate and rear passenger seats, which are fitted with oxygen OXIGÊNIO DE EMERGÊNCIA NO COMPARTIMENTO ABAIXO DO ASSENTO,...
Page 103 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (12) Under R.H. control wheel (13) On nose gear door (14) On nose gear leg NOSE LANDING GEAR TIRE PRESSURE : 6,5 bar 94 psi Rev. 13 BRAZIL Page 2.9.7 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 104 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (15) On main gear leg MAIN LANDING GEAR TIRE PRESSURE : 8,25 bar 120 psi (16) On engine cowling, in front of baggage compartment door (17) TBM700A On access door -- External side TBM700B On ”pilot”...
Page 105 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (17) TBM700B On access door -- External side (18) TBM700B On outer fuselage skin aft of access door and in the cabin forward of access door Rev. 13 BRAZIL Page 2.9.9 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 106 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (19) TBM700A from S / N 1 to S / N 49, except airplanes equipped as a retrofit with modification No. MOD70--019--25 On access door -- Internal side (19) TBM700A from S / N 50, plus airplanes equipped as a retrofit with modification No.
Page 107 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (19) TBM700B On access door -- Internal side (19) TBM700B On ”pilot” door -- Internal side (if installed) Rev. 13 BRAZIL Page 2.9.11 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 108 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (20) From S / N 1 to 23, 25, 28, 33 and 35, except airplanes equipped as a retrofit with modification No. MOD 70--019--25 On emergency exit handle Page 2.9.12 BRAZIL Rev.
Page 109 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (20) From S / N 24, 26, 27, 29 to 32, 34, 36 to 9999, plus airplanes equipped as a retrofit with modification No. MOD 70--019--25 On emergency exit handle Marking on cover Marking on handle Rev.
Page 110 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (21) TBM700A, TBM700B On last step of stairs (22) TBM700B On R.H. access door jamb (23) On internal face of L.H. engine cowl Page 2.9.14 BRAZIL Rev. 13 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 111 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved (24) On the potty seat curtain (if installed), on pilot’s side CURTAIN MUST BE STOWED FOR TAKE- -OFF AND LANDING Post--MOD70--0391--26D (25) On R.H. side at front seat level (26) On the lower drawer of the R.H.
Page 112 T B M SECTION 2 LIMITATIONS PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Page 2.9.16 BRAZIL Rev. 13 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 113 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved SECTION 3 EMERGENCY PROCEDURES TABLE OF CONTENTS Page GENERAL 3.1.1 ..........REJECTED TAKEOFF PROCEDURE 3.2.1 .
Page 114 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved TABLE OF CONTENTS (Continued) Page EMERGENCY DESCENTS 3.6.1 ....... . . 3.6.1 PROCEDURE IN SMOOTH AIR .
Page 115 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved TABLE OF CONTENTS (Continued) Page AMBER WARNING LIGHT LO VOLT 3.9.3 normal functioning on ”MAIN GEN” ........AMBER WARNING LIGHT LO VOLT functioning on ”ST--BY GENERATOR”...
Page 116 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved TABLE OF CONTENTS (Continued) Page 3.12 DEICING SYSTEM 3.12.1 ......... 3.12.1 LEADING EDGES DEICING FAILURE .
Page 117 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.1 - - GENERAL The recommended procedures for different failures or emergency situations are provided in this Section. Emergency procedures associated with optional or particular equipment which require pilot’s operating handbook supplements are provided in Section 9 ”Supplements”.
Page 118 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved Alarm system recall Main failure or state modification of the different systems are provided by an advisory panel. This panel includes red warning lights indicating a failure which requires an immediate action from the pilot, and amber warning lights indicating failures or discrepancies which require an action as soon as practical.
Page 119 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.2 - - REJECTED TAKEOFF PROCEDURE Following an engine failure, refer to Chapter 3.3, Paragraph ”ENGINE FAILURE AT TAKEOFF BEFORE ROTATION”. For any other reason : 1 -- Power lever .
Page 120 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 13 Page 3.2.2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 121 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.3 - - ENGINE FAILURES ENGINE FAILURE AT TAKEOFF BEFORE ROTATION 1 -- Power lever ......... IDLE 2 -- Braking .
Page 122 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.3 -- ENGINE FAILURES ENGINE FAILURE AFTER ROTATION - - If altitude does not allow to choose a favourable runway or field : Land straight ahead keeping flaps at TO and without changing landing gear position.
Page 123 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.3 -- ENGINE FAILURES ENGINE FAILURE DURING FLIGHT 1 -- If AP engaged : “AP / TRIM DISC INT” push--button ....PRESSED 2 -- Power lever .
Page 124 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.3 -- ENGINE FAILURES OIL PRESSURE DROP OIL PRESS RED WARNING LIGHT 1 -- Oil pressure indicator ......CHECK 2 -- If the indicated pressure is correct .
Page 125 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.3 -- ENGINE FAILURES ENGINE REGULATION DISCREPANCY, POWER LOSS, POWER LEVER CONTROL LOSS (1/2) 1 -- If circumstances allow : Power lever ......... IDLE 2 -- Confirm engine still running 3 -- Check that no parameter exceeds allowed values...
Page 126 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.3 -- ENGINE FAILURES ENGINE REGULATION DISCREPANCY, POWER LOSS, POWER LEVER CONTROL LOSS (2/2) 6 -- Perform a normal landing WITHOUT REVERSE 7 -- Braking ........AS REQUIRED If minimum power obtained is excessive : 1 -- Reduce airspeed by setting airplane in nose--up attitude at...
Page 127 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.3 -- ENGINE FAILURES GOVERNOR REGULATION CONTROL NOT OPERATING May indicate a rupture of the linkage of the governor control. 1 -- Continue the flight. 2 -- If Np < 2000 RPM, do not perform a go--around and do not use the reverse.
Page 128 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.3 -- ENGINE FAILURES EXCESSIVE PROPELLER ROTATION SPEED Indicates : a propeller governor failure In that case, the propeller overspeed limiter will limit initially the rotation speed to 2100 RPM approximately. or a propeller governor and overspeed limiter failure In that case, only the torque limiter operates to limit the power.
Page 129 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.3 -- ENGINE FAILURES RED WARNING LIGHT ON (1/2) Indicates that ITT exceeds 800°C During an engine start Intertubine temperature °C 1000 Inform the maintenance department No action required Time (seconds)
Page 130 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.3 -- ENGINE FAILURES RED WARNING LIGHT ON (2/2) 3 -- Record the engine parameters read as well as ground conditions. 4 -- Inform maintenance department. During flight 1 -- ITT indicator .
Page 131 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.3 -- ENGINE FAILURES ENGINE DOES NOT STOP ON GROUND If the engine does not stop when the condition lever is set to CUT OFF, proceed as follows : 1 -- ”AP / TRIMS MASTER”...
Page 132 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 13 Page 3.3.12 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 133 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.4 - - AIR START AIR START ENVELOPE AIR START ENVELOPE Air start may be attempted outside of the enveloppe. However, above 20000 ft or with Ng < 13 %, ITT tends to increase during start and prudence is recommended.
Page 134 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.4 -- AIR START AIR START WITH STARTER (1/2) CAUTION THE STARTER CANNOT OPERATE IF THE ”GENERATOR” SELECTOR IS ON ”ST- -BY” CAUTION IGNITION IS NOT AVAILABLE IF THE ”ESS BUS TIE” SWITCH IS KEPT ”EMER”...
Page 135 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.4 -- AIR START AIR START WITH STARTER (2/2) 12 -- Condition lever ........LO / IDLE when Ng μ...
Page 136 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 13 Page 3.4.4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 137 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.5 - - FIRE AND SMOKE ENGINE FIRE ON GROUND Symptoms : ITT increasing, red warning light smoke, ... 1 -- Power lever ......... IDLE 2 -- Condition lever .
Page 138 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.5 -- FIRE AND SMOKE ENGINE FIRE IN FLIGHT Symptoms : ITT increasing, red warning light smoke, ... 1 -- Power lever ......... IDLE 2 -- Propeller governor lever .
Page 139 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.5 -- FIRE AND SMOKE CABIN ELECTRICAL FIRE OR SMOKE DURING FLIGHT (1/2) If the origin is known : 1 -- Oxygen and goggles (if installed) ..USE AS REQUIRED (pilot and passengers) 2 -- Defective equipment...
Page 140 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.5 -- FIRE AND SMOKE CABIN ELECTRICAL FIRE OR SMOKE DURING FLIGHT (2/2) If smoke or fire persists : 5 -- ”SOURCE” selector ........6 -- ”GENERATOR”...
Page 141 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.5 -- FIRE AND SMOKE SMOKE ELIMINATION 1 -- Smoke origin ........IDENTIFY 2 -- Oxygen and goggles (if installed) .
Page 142 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 13 Page 3.5.6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 143 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.6 - - EMERGENCY DESCENTS PROCEDURE IN SMOOTH AIR 1 -- Power lever ......... IDLE 2 -- Oxygen .
Page 144 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.6 -- EMERGENCY DESCENTS GLIDE DISTANCE AND OPTIMUM SPEED Configuration 1 -- Flaps ..........2 -- Landing gear .
Page 145 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.7 - - EMERGENCY LANDINGS FORCED LANDING (ENGINE CUT OFF) 1 -- Power lever ......... IDLE 2 -- Propeller governor lever .
Page 146 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.7 -- EMERGENCY LANDINGS TIRE BLOWOUT DURING LANDING 1 -- Control direction with brakes and nose wheel steering 2 -- REVERSE ....... . AS REQUIRED 3 -- Stop airplane to minimize damages 4 -- Perform engine SHUT--DOWN procedure (Refer to Chapter 4.3)
Page 147 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.7 -- EMERGENCY LANDINGS LANDING WITH UNLOCKED MAIN LANDING GEAR (1/2) 1 -- Ask control tower or another airplane to visually check landing gear position CAUTION IF ONE MAIN LANDING GEAR IS NOT DOWN, IT IS BETTER TO LAND WITH GEAR UP.
Page 148 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.7 -- EMERGENCY LANDINGS LANDING WITH UNLOCKED MAIN LANDING GEAR (2/2) 11 -- Condition lever ........CUT OFF 12 -- Engine stop procedure .
Page 149 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.7 -- EMERGENCY LANDINGS LANDING WITH DEFECTIVE NOSE LANDING GEAR (DOWN UNLOCKED OR NOT DOWN) 1 -- Transfer passengers to the rear, if necessary 2 -- Approach ........Flaps TO IAS = 90 KIAS 3 -- Land with nose--up attitude, keep nose high...
Page 150 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.7 -- EMERGENCY LANDINGS LANDING WITH GEAR UP 1 -- Final approach ........Standard (Flaps LDG, IAS = 80 KIAS) 2 -- ”BLEED VALVE”...
Page 151 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.7 -- EMERGENCY LANDINGS LANDING WITHOUT ELEVATOR CONTROL 1 -- Configuration ... . LANDING GEAR DN - - FLAPS LDG 2 -- Airspeed .
Page 152 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.7 -- EMERGENCY LANDINGS LANDING WITH FLAPS MALFUNCTION For flaps deflections from “UP” to “TO” position : Proceed as for a normal landing, maintaining approach airspeed : -- Weight ± 6250 lbs (2835 kg) .
Page 153 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.7 -- EMERGENCY LANDINGS DITCHING 1 -- Landing gear ......... In heavy swell with light wind, land parallel to the swell (rollers).
Page 154 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 14 Page 3.7.10 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 155 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.8 - - FUEL SYSTEM RED WARNING LIGHT ON (1/2) FUEL PRESS Indicates a fuel pressure drop at ”HP” engine pump inlet 1 -- Remaining fuel ........CHECK 2 -- Tank selector .
Page 156 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.8 -- FUEL SYSTEM RED WARNING LIGHT ON (2/2) FUEL PRESS If pressure remains at 0 and if warning remains on : FUEL PRESS 9 -- Selection of the fullest tank .
Page 157 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.8 -- FUEL SYSTEM AMBER WARNING LIGHT AUX BP ON (Indication is normal if ”AUX BP” fuel switch is in ON position) If ”AUX BP” fuel switch is in AUTO position : 1 -- Reset to .
Page 158 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.8 -- FUEL SYSTEM AMBER WARNING LIGHT FUEL L. LO FUEL R. LO Indicates level drop in the corresponding tank 1 -- Corresponding gage ......CHECK 2 -- Check the other tank has been automatically selected If not :...
Page 159 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.9 - - ELECTRICAL SYSTEM RED WARNING LIGHT BAT OVHT (if Cadmium- -Nickel battery installed) Indicates a battery overheat 1 -- ”SOURCE” selector ........WARNING LIGHT BAT OVHT 2 -- Monitor airplane mains battery voltage...
Page 160 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.9 -- ELECTRICAL SYSTEM AMBER WARNING LIGHT MAIN GEN Indicates that ”GENERATOR” selector has been positioned to OFF or ST--BY, or main generator is cut off 1 -- If necessary .
Page 161 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.9 -- ELECTRICAL SYSTEM AMBER WARNING LIGHT LO VOLT normal functioning on ”MAIN GEN” 1 -- Voltmeter voltage ........CHECK 2 -- If voltage is <...
Page 162 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.9 -- ELECTRICAL SYSTEM AMBER WARNING LIGHT LO VOLT functioning on ”ST- -BY GENERATOR” (after ”MAIN GEN” failure) (1/2) Amber warning lights MAIN GEN LO VOLT with ”GENERATOR” selector on ”ST--BY” 1 -- ”GENERATOR”...
Page 163 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.9 -- ELECTRICAL SYSTEM AMBER WARNING LIGHT LO VOLT functioning on ”ST- -BY GENERATOR” (after ”MAIN GEN” failure) (2/2) 9 -- ”GENERATOR” selector ......If conditions allow : VMC and non icing conditions 10 -- Descend .
Page 164 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved FLAPS (D) STROBE PITOT 1 HTR R.W / S DE ICE INERT SEP AIRFRAME DE ICE ENGINE INDIC 1 : -- torquemeter, propeller & oil press+temperature IGNIT AUX BP PHONE or FUEL SEL PHONE+MKR...
Page 165 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.9 -- ELECTRICAL SYSTEM ”RADIO MASTER” SWITCH FAILURE NOTE : This procedure is not valid for aircraft S/N 1 to 17 if the ”RADIO FAN” circuit breaker is not releasable manually. In case of ”RADIO MASTER”...
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Page 167 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.10 - - PRESSURIZATION AND AIR CONDITIONING RED WARNING LIGHT CAB PRESS 1 -- Pressurization indicator ......CHECK ∆...
Page 168 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.10 -- PRESSURIZATION AND AIR CONDITIONING AMBER WARNING LIGHT BLEED OFF (Normal signal if ”BLEED VALVE” switch is OFF) 1 -- If necessary ........CORRECT 2 -- In case of failure, the airplane is no longer pressurized, nor conditioned...
Page 169 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.10 -- PRESSURIZATION AND AIR CONDITIONING RED WARNING LIGHT BLEED TEMP Indicates overheat of air conditioning pack. Normally this leads to ”BLEED VALVE” cutoff and to amber warning light BLEED OFF illumination Should automatic cutoff occur or not :...
Page 170 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.10 -- PRESSURIZATION AND AIR CONDITIONING RED WARNING LIGHT DOOR Indicates that one of the door latches of the access door and (if installed) of the ”pilot” door has not been correctly locked On ground, check the correct locking, as well as the latches position of the access door and (if installed) of the ”pilot”...
Page 171 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.10 -- PRESSURIZATION AND AIR CONDITIONING AMBER WARNING LIGHT VACUUM LO Suction gage indicator ....... . CHECK Low vacuum may lead to misfunctioning of leading edge deicing, pressurization and gyroscopic vacuum--operated...
Page 172 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.10 -- PRESSURIZATION AND AIR CONDITIONING DEFOG MALFUNCTION If moisture starts to quickly cover the inside of the windscreen with the distributor already positioned on ”DEFOG” : 1 -- ”DEFOG / NORMAL” distributor .
Page 173 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.11 - - LANDING GEAR AND FLAPS LANDING GEAR RETRACTION DISCREPANCY NOTE : Symptoms have to be considered at the end of the sequence. - - Symptoms Red warning light OFF and 1 to 3 green light(s) ON. Steady red warning light ON and 0 to 3 green light(s) ON.
Page 174 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.11 -- LANDING GEAR AND FLAPS LANDING GEAR EXTENSION DISCREPANCY NOTE : Symptoms have to be considered at the end of the sequence. - - Symptoms Red warning light OFF and 1 to 3 green light(s) OFF. Steady red warning light ON and 0 to 3 green light(s) OFF.
Page 175 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.11 -- LANDING GEAR AND FLAPS LANDING GEAR RETRACTION DISCREPANCY NOTE : Symptoms have to be considered at the end of the sequence. A - - Symptoms : Steady red warning light ON and 0 to 3 green light(s) ON.
Page 176 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.11 -- LANDING GEAR AND FLAPS LANDING GEAR EXTENSION DISCREPANCY NOTE : Symptoms have to be considered at the end of the sequence. - - Symptoms Steady red warning light ON and 0 to 3 green light(s) OFF. Red warning light flashing and 0 to 3 green light(s) OFF.
Page 177 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.11 -- LANDING GEAR AND FLAPS EMERGENCY GEAR EXTENSION (1/2) NOTE : This procedure has to be followed in case of any discrepancy or doubt about the gear extension or retraction. Maintain IAS ≤...
Page 178 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.11 -- LANDING GEAR AND FLAPS EMERGENCY GEAR EXTENSION (2/2) If landing gear does not lock (other than 3 green indicator lights illuminated) : 6 -- ”LDG GR” circuit breaker .
Page 179 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.11 -- LANDING GEAR AND FLAPS RED WARNING LIGHT FLAPS Indicates a dissymmetry of flap deflection. This immediately stops the flap motor and prevents further operation of the flaps 1 -- ”FLAPS”...
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Page 181 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.12 - - DEICING SYSTEM LEADING EDGES DEICING FAILURE Symptoms : Failure on one of the two pneumatic deicing pulses : -- Ice on wing outboard sections -- Or ice on wing inboard sections and stabilizers -- One of the two cycling green lights is not lit 1 -- LEAVE icing conditions as soon as possible 2 -- ”AIRFRAME DE ICE”...
Page 182 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.12 -- DEICING SYSTEM INERTIAL SEPARATOR FAILURE Symptoms : -- Warning light is not lit within 30 seconds following ”INERT SEP” switch setting ON -- Neither torque drop, nor increase of ITT observed during maneuver LEAVE icing conditions as soon as possible WINDSHIELD DEICING FAILURE...
Page 183 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.12 -- DEICING SYSTEM WINDSHIELD MISTING OR INTERNAL ICING Symptoms : -- Mist or ice on windshield internal face 1 -- ”CABIN TEMP” selector ......Max HOT 2 -- ”DEFOG / NORMAL”...
Page 184 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.12 -- DEICING SYSTEM AMBER WARNING LIGHT PITOT 1 PITOT 2 STALL HTR Indicates a heating failure of the corresponding probe Icing conditions may alter airspeed indications on the PITOT 1 airspeed indicator 1 -- AVOID icing conditions...
Page 185 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.13 - - MISCELLANEOUS RUNAWAY OF ONE OF THE THREE ELECTRICAL TRIM TABS 1 -- ”AP / DISC TRM INT” push button ..PRESSED AND HOLD The three trim tabs are disconnected and runaway stops 2 -- ”AP / TRIMS MASTER”...
Page 186 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.13 -- MISCELLANEOUS EMERGENCY EXIT USE 1 -- Check that the anti--theft safety pin has been removed 2 -- Lift up the opening handle 3 -- Pull emergency exit assembly toward oneself to release it from its recess 4 -- Put the emergency exit door inside fuselage or throw it away from the fuselage through the opening...
Page 187 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.13 -- MISCELLANEOUS TOTAL COMMUNICATION FAILURE 1 -- Refer to PARTICULAR TRANSPONDER USES procedures 2 -- Apply air traffic control procedures in case of communications failure : -- code 7700 during 1 minute, then -- code 7600 3 -- Try to restore communications by using all possible combinations of the headset, micro and loudspeaker...
Page 188 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.13 -- MISCELLANEOUS PARTICULAR TRANSPONDER USES 1 -- Check transponder mode selector ....ON or ALT 2 -- Codes selector : 7700...
Page 189 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.13 -- MISCELLANEOUS OXYGEN USE (1/2) WARNING SMOKING IS STRICTLY PROHIBITED ANY TIME OXYGEN SYSTEM IS USED. BEFORE USING OXYGEN, REMOVE ANY TRACE OF OIL, GREASE, SOAP AND OTHER FATTY SUBSTANCES (INCLUDING LIPSTICK, MAKE UP, ETC...) WARNING IN CASE GENERATOR FAILS TO ACTIVATE, PULL ON...
Page 190 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.13 -- MISCELLANEOUS OXYGEN USE (2/2) NOTE : Whenever an oxygen generator is activated, warning OXYGEN light, located on the advisory panel, illuminates. The warning light will remain ON as long as the used generator is not replaced AIRSPEED INDICATING SYSTEM FAILURE Symptoms : erroneous indication in flight...
Page 191 T B M SECTION 3 EMERGENCY PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 3.13 -- MISCELLANEOUS FLIGHT INTO SEVERE ICING CONDITIONS Severe icing conditions, particularly freezing rain and freezing drizzle, can be identified by : -- unusually extensive ice accumulation on the airframe and windshield in areas not normally observed to collect ice, -- accumulation of ice on the upper surface of the wing aft of the protected area.
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Page 193 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved SECTION 4 NORMAL PROCEDURES TABLE OF CONTENTS Page GENERAL 4.1.1 ..........AIRSPEEDS FOR NORMAL OPERATION 4.2.1 .
Page 194 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved TABLE OF CONTENTS (Continued) Page 4.4.34 MOTORING FOLLOWED BY AN ENGINE START ....4.4.37 AFTER STARTING ENGINE .
Page 195 EASA Approved 4.1 - - GENERAL This Section provides procedures for the conduct of normal operation of TBM 700 airplane. The first part of this Section lists the normal procedures required as a check list. The amplified procedures are developed in the second part of the Section.
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Page 197 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 4.2 - - AIRSPEEDS FOR NORMAL OPERATION CONDITIONS : - Takeoff weight 6579 lbs (2984 kg) - Landing weight : 6250 lbs (2835 kg) Rotation airspeed (V -- Flaps TO .
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Page 199 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 4.3 - - CHECK- -LIST PROCEDURES PREFLIGHT INSPECTION (See Figure 4.3.1) IMPORTANT * During outside inspection, visually check inspection doors and airplane general condition. * In cold weather, remove even small accumulations of frost, ice or snow from wing, tail and control surfaces.
Page 200 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES PREFLIGHT INSPECTION (Cont’d) Figure 4.3.1 -- PREFLIGHT INSPECTION Rev. 13 Page 4.3.2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 201 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES PREFLIGHT INSPECTION (Cont’d) A - - INSIDE INSPECTIONS Cockpit -- CRASH lever ........1 -- ELECTRIC POWER panel -- ”SOURCE”...
Page 202 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES PREFLIGHT INSPECTION (Cont’d) 12 -- ECS panel -- ”BLEED VALVE” switch ......-- ”CABIN FAN”...
Page 203 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES PREFLIGHT INSPECTION (Cont’d) CAUTION BEFORE SELECTING SOURCE, CHECK : 21 - - ”IGNITION” switch ......AUTO or OFF 22 - - ”STARTER”...
Page 204 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES PREFLIGHT INSPECTION (Cont’d) 31 -- ECS panel -- ”LT TEST” push button (if vapor cycle cooling system installed) ... . PRESS (green lamp ON) 32 -- Flaps...
Page 205 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES PREFLIGHT INSPECTION (Cont’d) 37 -- EXT LIGHTS panel -- ”STROBE” ........-- ”NAV”...
Page 206 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES PREFLIGHT INSPECTION (Cont’d) B - - AIRPLANE OUTSIDE L.H. wing III 1 -- Flap ..........CHECK (Condition / Play) 2 -- Aileron and trim / Spoiler...
Page 207 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES PREFLIGHT INSPECTION (Cont’d) Fuselage forward section IV 1 -- Baggage compartment -- Inside ........CONTROLLED -- Door .
Page 208 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES PREFLIGHT INSPECTION (Cont’d) 10 -- R.H. exhaust stub ....... . CHECK (Condition / No cracks) R.H.
Page 209 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES PREFLIGHT INSPECTION (Cont’d) Fuselage rear section / Empennages VI 1 -- Static pressure ports ..... . . Clean - - CHECK 2 -- Ventral fins .
Page 210 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES BEFORE STARTING ENGINE (1/2) CAUTION ”BLEED VALVE” SWITCH ON “ON” MAY CAUSE OVERTEMPERATURE OR ABNORMAL ACCELERATION AT START CAUTION MAKE SURE THAT ”MAN OVRD” CONTROL IS OFF TO AVOID OVERTEMPERATURE RISKS AT START 1 -- Preflight inspection .
Page 211 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES BEFORE STARTING ENGINE (2/2) 17 -- Radar switch (if installed) ......18 -- ”SOURCE”...
Page 212 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES STARTING ENGINE USING AIRPLANE POWER (1/5) CAUTION BEFORE SELECTING SOURCE, CHECK : 1 - - ”IGNITION” switch ..... . . AUTO or OFF 2 - - ”STARTER”...
Page 213 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES STARTING ENGINE USING AIRPLANE POWER (2/5) 7 -- FUEL panel -- ”AUX BP” switch ........WARNING LIGHT AUX BP ON FUEL PRESS...
Page 214 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES STARTING ENGINE USING AIRPLANE POWER (3/5) 11 -- Condition lever ........HI / IDLE CHECK : Ng 69 % (±...
Page 215 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES STARTING ENGINE USING AIRPLANE POWER (4/5) CAUTION IF ENGINE STAGNATES, INTERRUPT STARTING PROCEDURE : Condition lever ........CUT OFF ”IGNITION”...
Page 216 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES STARTING ENGINE USING AIRPLANE POWER (5/5) 50 % -- ”STARTER” switch ........STARTER WARNING LIGHTS IGNITION...
Page 217 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES STARTING ENGINE USING EXTERNAL POWER (GPU) (1/5) 1 -- GPU ........CONNECTED CAUTION BEFORE SELECTING SOURCE, CHECK :...
Page 218 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES STARTING ENGINE USING EXTERNAL POWER (GPU) (2/5) 8 -- FUEL panel -- ”AUX BP” switch ........WARNING LIGHTS AUX BP ON FUEL PRESS...
Page 219 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES STARTING ENGINE USING EXTERNAL POWER (GPU) (3/5) 11 -- ”SOURCE” selector ........BAT OFF WARNING LIGHT 12 -- Propeller governor lever...
Page 220 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES STARTING ENGINE USING EXTERNAL POWER (GPU) (4/5) CAUTION IF 10 SECONDS AFTER HAVING POSITIONED CONDITION LEVER TO ”LO / IDLE” THERE IS NO IGNITION OR IF DURING IGNITION SEQUENCE, OVERTEMPERATURE INDICATION APPEARS (MAX.
Page 221 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES STARTING ENGINE USING EXTERNAL POWER (GPU) (5/5) ENGINE START panel -- ”IGNITION” switch ........AUTO -- ”STARTER”...
Page 222 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES MOTORING (1/2) CAUTION AFTER ANY STARTING INTERRUPT PROCEDURE : - - WAIT FOR ENGINE TOTAL SHUT- -DOWN - - WAIT AT LEAST 30 SECONDS BEFORE INITIATING A MOTORING 1 -- Engine controls -- ”MAN OVRD”...
Page 223 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES MOTORING (2/2) 3 -- ”IGNITION” switch ........WARNING LIGHT IGNITION To clear fuel and vapor internally trapped :...
Page 224 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES MOTORING FOLLOWED BY AN ENGINE START (1/2) Within starter operating limits (continuous max. 1 minute), it is possible to initiate a starting procedure from a motoring procedure. 1 -- Engine controls -- ”MAN OVRD”...
Page 225 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES MOTORING FOLLOWED BY AN ENGINE START (2/2) 5 -- After 15 seconds : -- ”IGNITION” switch ......AUTO or ON -- Ng .
Page 226 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES AFTER STARTING ENGINE (1/2) 1 -- GYRO INST panel -- All switches ........Pull on the caging knobs when starting the ADI(s).
Page 227 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES AFTER STARTING ENGINE (2/2) 5 -- ”GENERATOR” selector -- On ”MAIN” ....Voltage and current checked when current ≤...
Page 228 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES TAXIING 1 -- ”TAXI” light ......... . 2 -- ”INERT SEP”...
Page 229 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES BEFORE TAKEOFF (1/2) 1 -- Parking brake ........WARNING LIGHT PARK BRAKE 2 -- Condition lever...
Page 230 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES BEFORE TAKEOFF (2/2) 7 -- Advisory panel ........CHECK All warning lights OFF, except...
Page 231 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES TAKEOFF (1/2) WHEN LINED UP CAUTION - - IF HEAVY PRECIPITATION, TURN IGNITION AND INERT SEP - - IF ICING CONDITIONS ARE FORESEEN, REFER TO CHAPTER 4.5, PARAGRAPH ”FLIGHT INTO KNOWN ICING CONDITIONS”...
Page 232 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES TAKEOFF (2/2) 8 -- Brakes ........RELEASED 9 -- Power lever .
Page 233 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES CLIMB 1 -- Power lever ......ADJUST according to engine operation table - - Chapter 5.7 CAUTION...
Page 234 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES CRUISE 1 -- Power lever ......ADJUST according to engine operation table - - Chapter 5.7 CAUTION...
Page 235 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES DESCENT 1 -- Altimeter settings ......COMPLETE 2 -- ECS panel -- Cabin altitude selector...
Page 236 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES BEFORE LANDING Long final 1 -- Altimeters ........CHECK 2 -- Fuel -- Gages...
Page 237 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES LANDING 1 -- Power lever ......... IDLE After wheel touch 2 -- Reverse...
Page 238 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES GO- -AROUND 1 -- Simultaneously -- Power lever ......TRQ = 100 % -- Attitude .
Page 239 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES TOUCH AND GO After wheel touch 1 -- Flaps ..........2 -- Elevator trim .
Page 240 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES SHUT- -DOWN (1/2) 1 -- Parking brake ........WARNING LIGHT PARK BRAKE 2 -- ”TAXI”...
Page 241 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved CHECK--LIST PROCEDURES SHUT- -DOWN (2/2) 14 -- Fuel -- ”AUX BP” switch ........-- ”FUEL SEL”...
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Page 243 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 4.4 - - AMPLIFIED PROCEDURES PREFLIGHT INSPECTION A - - INSIDE INSPECTIONS Cockpit -- CRASH lever ........1 -- ELECTRIC POWER panel -- ”SOURCE”...
Page 244 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES PREFLIGHT INSPECTION (Cont’d) 8 -- Landing gear emergency control Open door of emergency landing gear compartment. -- Lever ........PULLED DOWN -- By--pass selector .
Page 245 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES PREFLIGHT INSPECTION (Cont’d) CAUTION WHEN THE ENGINE IS SHUTDOWN, THE POWER LEVER MUST NOT BE MOVED BEHIND THE FLIGHT IDLE POSITION When engine is shut--off, a lack of hydraulic pressure prevents movement into reverse range.
Page 246 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES PREFLIGHT INSPECTION (Cont’d) 25 -- Voltage ......... . CHECK -- BAT .
Page 247 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES PREFLIGHT INSPECTION (Cont’d) 29 -- Oxygen emergency system ... WARNING LIGHT OXYGEN If not, seek which of the oxygen generators has been activated. The amber strip around each generator becomes black by thermal effect, if the generator has been operated.
Page 248 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES PREFLIGHT INSPECTION (Cont’d) Correct operation of pitot (PITOT 1 and 2) tube heating elements and of stall aural warning system (STALL HTR) is indicated by extinction of corresponding lights on the advisory panel, when control switches are ON.
Page 249 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES PREFLIGHT INSPECTION (Cont’d) Cabin II 1 -- Cabin fire extinguisher (if installed) ....CHECK (Pressure / Attachment) The fire extinguisher is provided with a pressure gage.
Page 250 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES PREFLIGHT INSPECTION (Cont’d) B - - AIRPLANE OUTSIDE The preflight inspection described in Figure 4.3.1 is recommended before each flight. NOTE : If a preflight inspection is performed, just after the engine shut- -off, be careful because the leading edge of engine air inlet, as well as exhaust stubs may be very hot.
Page 251 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES PREFLIGHT INSPECTION (Cont’d) 2 -- Aileron and trim / Spoiler ......CHECK (Condition / Free movement / Deflection) Ensure there are no foreign objects in the spoiler recess.
Page 252 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES PREFLIGHT INSPECTION (Cont’d) 11 -- Wing deicer boots ....... . CHECK (Condition / Attachment) Care must be taken when refuelling the airplane to avoid damaging...
Page 253 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES PREFLIGHT INSPECTION (Cont’d) Fuselage forward section IV 1 -- Baggage compartment -- Inside ........CONTROLLED -- Door .
Page 254 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES PREFLIGHT INSPECTION (Cont’d) 7 -- Air inlets -- Main ..... . No crack - - UNOBSTRUCTED Check for no cracks, which are sometimes put in evidence by traces of soot resulting from exhaust gases.
Page 255 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES PREFLIGHT INSPECTION (Cont’d) R.H. wing V Additional remarks are identical to those of L.H. wing. 1 -- Fuel tank drain (two on each wing) ....DRAIN (Fuel free of water and contamination) 2 -- Main landing gear...
Page 256 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES PREFLIGHT INSPECTION (Cont’d) Fuselage rear section / Empennages VI Check that outside handle of emergency exit is flush with door skin. 1 -- Static pressure ports .
Page 257 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES BEFORE STARTING ENGINE (1/4) Check that the weight and balance are within the correct limits. Brief passengers about use of seat belts and the emergency oxygen system, as well as opening the access door and the emergency exit.
Page 258 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES BEFORE STARTING ENGINE (2/4) 8 -- R.H and L.H. pedals ......ADJUSTED 9 -- Belts and harnesses (Pilot and passengers) .
Page 259 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES BEFORE STARTING ENGINE (3/4) 19 -- ”BAT TEMP TEST” push--button (if installed -- with a Cadmium--Nickel battery) ..PRESS Check illumination of the ”BAT OVHT”...
Page 260 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES BEFORE STARTING ENGINE (4/4) 24 -- Engine instruments ....... CHECK 25 -- ITT TEST .
Page 261 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES STARTING ENGINE USING AIRPLANE POWER (1/6) CAUTION BEFORE SELECTING SOURCE, CHECK : 1 - - ”IGNITION” switch ..... . . AUTO or OFF 2 - - ”STARTER”...
Page 262 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES STARTING ENGINE USING AIRPLANE POWER (2/6) 7 -- FUEL panel -- ”AUX BP” switch ........WARNING LIGHT AUX BP ON FUEL PRESS...
Page 263 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES STARTING ENGINE USING AIRPLANE POWER (3/6) In case of higher temperature and longer time, stop immediately the starting procedure as indicated in the following caution and inform the maintenance department.
Page 264 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES STARTING ENGINE USING AIRPLANE POWER (4/6) -- Ng The start sequence must be timed to ensure starter limits are not exceeded. Lengthy operation of the starter results in excessive temperature of the engine : -- If Ng does not reach 30 % within 30 seconds, after the starter is selected ON, abort the start.
Page 265 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES STARTING ENGINE USING AIRPLANE POWER (5/6) Monitor increase of : -- ITT ....(max.
Page 266 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES STARTING ENGINE USING AIRPLANE POWER (6/6) 13 -- FUEL panel -- ”AUX BP” switch ....... . . AUTO At this time, observing a drop in the fuel pressure is normal.
Page 267 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES STARTING ENGINE USING EXTERNAL POWER (GPU) (1/7) Before connecting GPU, check that its indicated voltage is correct. 1 -- GPU ........CONNECTED CAUTION BEFORE SELECTING SOURCE, CHECK :...
Page 268 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES STARTING ENGINE USING EXTERNAL POWER (GPU) (2/7) -- Propeller governor lever ..... . . MAX RPM -- Condition lever .
Page 269 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES STARTING ENGINE USING EXTERNAL POWER (GPU) (3/7) The absolute limit read on the indicator is 1090°C during the starting sequence (red triangle). However, the ITT limits during the starting sequence are : .
Page 270 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES STARTING ENGINE USING EXTERNAL POWER (GPU) (4/7) CAUTION IF 10 SECONDS AFTER HAVING POSITIONED CONDITION LEVER TO ”LO / IDLE” THERE IS NO IGNITION OR IF DURING IGNITION SEQUENCE, OVERTEMPERATURE INDICATION APPEARS (MAX.
Page 271 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES STARTING ENGINE USING EXTERNAL POWER (GPU) (5/7) CAUTION IF ENGINE STAGNATES, INTERRUPT STARTING PROCEDURE : Condition lever ........CUT OFF ”IGNITION”...
Page 272 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES STARTING ENGINE USING EXTERNAL POWER (GPU) (6/7) Monitor increase of : -- ITT ....(max.
Page 273 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES STARTING ENGINE USING EXTERNAL POWER (GPU) (7/7) This means that ground power receptacle door has been correctly locked. 14 -- Condition lever ........HI / IDLE 15 -- Propeller governor lever .
Page 274 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES MOTORING (1/3) To drain fuel accumulated inside the combustion chamber, a motoring procedure is required following an aborted start. A 15--second dry motoring run is sufficient to clear any fuel pooled in the engine.
Page 275 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES MOTORING (2/3) 2 -- FUEL panel -- Tank selector ........L or R -- ”AUX BP”...
Page 276 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES MOTORING (3/3) 6 -- FUEL panel -- ”AUX BP” switch ........WARNING LIGHTS AUX BP ON FUEL PRESS...
Page 277 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES MOTORING FOLLOWED BY AN ENGINE START (1/3) Amplified procedures stated in starting engine sequences using airplane power or with GPU are also to be applied to hereunder procedure.
Page 278 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES MOTORING FOLLOWED BY AN ENGINE START (2/3) 5 -- After 15 seconds : -- ”IGNITION” switch ......AUTO or ON -- Ng .
Page 279 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES MOTORING FOLLOWED BY AN ENGINE START (3/3) 10 -- FUEL panel -- ”AUX BP” switch ....... . AUTO WARNING LIGHT AUX BP ON...
Page 280 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES AFTER STARTING ENGINE (1/4) 1 -- GYRO INST panel -- All switches ........Pull on the caging knobs when starting the ADI(s).
Page 281 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES AFTER STARTING ENGINE (2/4) -- ”L.WINDSHIELD” switch ......-- ”R.WINDSHIELD”...
Page 282 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES AFTER STARTING ENGINE (3/4) when current ≤ 50 amps : -- on ”ST--BY” ....Voltage and current checked (reset if necessary) If the indicated voltage on the ”ST BY”...
Page 283 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES AFTER STARTING ENGINE (4/4) 9 -- Radar switch (if installed) ......10 -- ”EFIS MASTER”...
Page 284 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES TAXIING (1/2) 1 -- ”TAXI” light ......... . . 2 -- ”INERT SEP”...
Page 285 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES TAXIING (2/2) CAUTION AVOID USING REVERSE DURING TAXIING Operation in the Beta (β) range / reverse is not restricted during ground operations. However, foreign particles (dust, sand, grass, gravel, etc...) may be blown into the air, ingested by the engine (above all if ”INERT SEP”...
Page 286 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES BEFORE TAKEOFF (1/3) 1 -- Parking brake ........WARNING LIGHT PARK BRAKE 2 -- Condition lever...
Page 287 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES BEFORE TAKEOFF (2/3) If there is standing water or other contamination on the runway : -- ”INERT SEP” switch ......Left ON WARNING LIGHT INERT SEP...
Page 288 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES BEFORE TAKEOFF (3/3) 12 -- Trims -- Pitch ........ADJUSTED -- Yaw .
Page 289 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES TAKEOFF (1/3) WHEN LINED UP CAUTION - - IF HEAVY PRECIPITATION, TURN IGNITION AND INERT SEP - - IF ICING CONDITIONS ARE FORESEEN, REFER TO CHAPTER 4.5, PARAGRAPH ”FLIGHT INTO KNOWN ICING CONDITIONS”...
Page 290 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES TAKEOFF (2/3) 6 -- Radar switch (if installed) ..... . . As required 7 -- PROP O’...
Page 291 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES TAKEOFF (3/3) 13 -- Landing gear control ..(IAS < 128 KIAS) ... . At sequence end, check : All warning lights OFF In practice, if preconized attitude is kept, there is no difficulty to maintain a speed <...
Page 292 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Page 4.4.50 (a) Rev. 16 Pre- -MOD70- -021- -32 and Pre- -MOD70- -0640- -32 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 293 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES TAKEOFF (3/3) 13 -- Landing gear control ..(IAS < 128 KIAS) ... During the sequence : -- The red warning light flashes ;...
Page 294 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Page 4.4.50 (b) Rev. 16 Post- -MOD70- -021- -32 or Post- -MOD70- -0640- -32 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 295 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES CLIMB (1/2) 1 -- Power lever ......ADJUST according to engine operation table - - Chapter 5.7 CAUTION...
Page 296 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES CLIMB (2/2) 3 -- ECS panel -- Cabin altitude selector ..Cruise altitude + 1000 feet -- Cabin rate selector .
Page 297 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES CRUISE (1/2) 1 -- Power lever ......ADJUST according to engine operation table - - Chapter 5.7 As indicated in lower part of these tables, reducing propeller RPM is...
Page 298 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES CRUISE (2/2) 3 -- Fuel -- Gages ......... CHECK REGULARLY CHECK : - - consumption...
Page 299 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES DESCENT (1/2) 1 -- Altimeter settings ......COMPLETE 2 -- ECS panel -- Cabin altitude selector...
Page 300 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES DESCENT (2/2) 5 -- Fuel -- Gages ......... CHECK (Quantity / Symmetry) -- Fullest tank...
Page 301 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES BEFORE LANDING (1/2) Long final 1 -- Altimeters ........CHECK 2 -- Fuel -- Gages...
Page 302 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES BEFORE LANDING (2/2) 10 -- 11 -- Approach speed (Flaps LDG) ..... . . 80 KIAS To ensure positive and rapid engine response to throttle movement, it is recommended that a minimum of 10 % torque be maintained on...
Page 303 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES BEFORE LANDING (1/2) Long final 1 -- Altimeters ........CHECK 2 -- Fuel -- Gages...
Page 304 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES BEFORE LANDING (2/2) 7 -- 8 -- Autopilot ..........Autopilot must be disconnected at the latest at 200 ft above the ground or at decision height or before go--around, whichever is the highest.
Page 305 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES LANDING 1 -- Power lever ......... IDLE Avoid three--point landings.
Page 306 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES GO- -AROUND 1 -- Simultaneously -- Power lever ......TRQ = 100 % -- Attitude .
Page 307 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES TOUCH AND GO After wheels touch 1 -- Flaps ..........Check that flaps have well reached the TO position before increasing power.
Page 308 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES AFTER LANDING RUNWAY CLEAR -- AIRPLANE STOPPED 1 -- DE ICE SYSTEM panel -- ”AIRFRAME DE ICE” switch ......-- ”PROP DE ICE”...
Page 309 SECTION 4 T B M NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES SHUT- -DOWN (1/2) 1 -- Parking brake ........WARNING LIGHT PARK BRAKE 2 -- ”TAXI”...
Page 310 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved AMPLIFIED PROCEDURES SHUT- -DOWN (2/2) 13 -- Condition lever ........CUT OFF CAUTION IN CASE OF SHUT- -DOWN ON A CONTAMINATED...
Page 311 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved 4.5 - - PARTICULAR PROCEDURES REMARK : The procedures and procedure elements given in this Chapter ”PARTICULAR PROCEDURES” supplement the normal procedures or complete certain elements of the normal procedures described in Chapter(s) 4.3 and/or 4.4.
Page 312 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES FLIGHT INTO KNOWN ICING CONDITIONS (2/5) Boots are automatically cycling at the optimum time to assure proper ice removal. Correct operation of the system can be checked observing the corresponding green advisory light illumination at each boot inflation impulse.
Page 313 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES FLIGHT INTO KNOWN ICING CONDITIONS (3/5) 2 -- When operating under IMC : -- All ”DE ICE SYSTEM” switches ......-- ”IGNITION”...
Page 314 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES FLIGHT INTO KNOWN ICING CONDITIONS (4/5) NOTE : ”IGNITION” switch may be left ON for a long period. Standby compass indications are altered when windshield deicing system(s) operate(s).
Page 315 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES FLIGHT INTO KNOWN ICING CONDITIONS (5/5) Ice accumulation effects When ice has accumulated on the unprotected surfaces of the airplane, aerodynamic characteristics may be changed. Particularly stall speeds may increase by up to : -- Flaps UP 20 KIAS -- Flaps TO...
Page 316 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES FLIGHT INTO SEVERE ICING CONDITIONS (1/2) THE FOLLOWING WEATHER CONDITIONS MAY BE CONDUCIVE TO SEVERE IN- -FLIGHT ICING : -- Visible rain at temperatures below 0°C ambient air temperature, -- Droplets that splash or splatter on impact at temperatures below 0°C ambient air temperature.
Page 317 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES FLIGHT INTO SEVERE ICING CONDITIONS (2/2) 6 -- Do not extend flaps when holding in icing conditions. Operation with flaps extended can result in a reduced wing angle--of--attack, with the possibility of ice forming on the upper surface further aft on the wing than normal, possibly aft of the protected area.
Page 318 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES FLIGHT UNDER HEAVY PRECIPITATIONS 1 -- ”IGNITION” switch ........This action is intended, in highly improbable case of an engine flame--out further to an important ingestion, to ensure immediate restarting without action of the pilot.
Page 319 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION ON RUNWAYS COVERED WITH MELTING OR NOT TAMPED SNOW (2/2) Before takeoff 1 -- If the runway is long enough, takeoff should be performed with the flaps in the up position.
Page 320 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION COVERED WITH TAMPED SNOW RUNWAYS (1/2) Refer if required to paragraph ”UTILIZATION BY COLD WEATHER AND VERY COLD WEATHER”. Preflight inspection 1 -- Remove any snow or ice from the wings, stabilizers and movable surfaces, landing gear wells and gear doors, as well as flap tracks, actuators and their fairings.
Page 321 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION ON ICY OR COVERED WITH TAMPED SNOW RUNWAYS (2/2) Landing After wheel touch 1 -- Use reverse only if necessary and very progressively by monitoring the airplane behaviour.
Page 322 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION BY COLD WEATHER (- - 0° C TO - - 25° C) AND VERY COLD WEATHER (- - 25° C TO - - 40° C) (1/10) REMARK : The procedures hereafter supplement the normal procedures for the airplane use when operating under temperatures between 0°...
Page 323 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION BY COLD WEATHER (- - 0° C TO - - 25° C) AND VERY COLD WEATHER (- - 25° C TO - - 40° C) (2/10) ENVELOPE 1 The procedures hereafter supplement the normal procedures for the airplane use when operating in the ”envelope 1”...
Page 324 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION BY COLD WEATHER (- - 0° C TO - - 25° C) AND VERY COLD WEATHER (- - 25° C TO - - 40° C) (3/10) Taxiing / Before takeoff / Takeoff 1 -- On ”DE--ICE SYSTEM”...
Page 325 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION BY COLD WEATHER (- - 0° C TO - - 25° C) AND VERY COLD WEATHER (- - 25° C TO - - 40° C) (4/10) ENVELOPE 2 The procedures hereafter supplement or replace the normal procedures for the airplane use when operating in the ”envelope 2”...
Page 326 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION BY COLD WEATHER (- - 0° C TO - - 25° C) AND VERY COLD WEATHER (- - 25° C TO - - 40° C) (5/10) 6 -- Remove chocks and / or release ties from the airplane.
Page 327 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION BY COLD WEATHER (- - 0° C TO - - 25° C) AND VERY COLD WEATHER (- - 25° C TO - - 40° C) (6/10) 3 -- Engine controls -- ”MAN OVRD”...
Page 328 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION BY COLD WEATHER (- - 0° C TO - - 25° C) AND VERY COLD WEATHER (- - 25° C TO - - 40° C) (7/10) 13 % -- Condition lever .
Page 329 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION BY COLD WEATHER (- - 0° C TO - - 25° C) AND VERY COLD WEATHER (- - 25° C TO - - 40° C) (8/10) After starting the engine 1 -- On ”ECS”...
Page 330 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION BY COLD WEATHER (- - 0° C TO - - 25° C) AND VERY COLD WEATHER (- - 25° C TO - - 40° C) (9/10) ENVELOPE 3 The procedures defined for the ”envelope 2”...
Page 331 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION BY COLD WEATHER (- - 0° C TO - - 25° C) AND VERY COLD WEATHER (- - 25° C TO - - 40° C) (10/10) Taxiing / Before takeoff / Takeoff Apply procedures defined for Envelope 1.
Page 332 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES LANDING PROCEDURE WITH STRONG HEADWIND CROSSWIND (1/2) If landing must be performed with strong headwind or crosswind, increase approach speed by the greatest of these 2 following values : WIND DOWN −...
Page 333 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES LANDING PROCEDURE WITH STRONG HEADWIND OR CROSSWIND (2/2) Do not try to stabilize the airplane by pushing down the elevator control just after the touch ; this operation may provide pitch oscillations while increasing the yaw movement to the wind.
Page 334 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES UTILIZATION ON GRASS RUNWAY CAUTION THE SMALL WHEELS OF THE AIRPLANE AND ITS WEIGHT MAY LEAD IT TO SINK IN SOPPY OR LOOSE GROUND Before planning the landing, ensure that the field is hard, smooth and dry enough.
Page 335 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved PARTICULAR PROCEDURES OPERATION IN RVSM CONDITIONS After altitude capture, in altitude hold mode of the autopilot, discrepancy between desired altitude and held altitude must be adjusted using the vertical trim control in order not to exceed ¦...
Page 336 T B M SECTION 4 NORMAL PROCEDURES PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 13 Page 4.5.26 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 337 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK SECTION 5 PERFORMANCE TABLE OF CONTENTS Page ACOUSTIC LIMITATION 5.1.1 ........AIRSPEED CALIBRATION 5.2.1 .
Page 338 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 339 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK SECTION 5 PERFORMANCE TABLE OF CONTENTS Page FLYOVER NOISE LEVEL 5.1.1 ........AIRSPEED CALIBRATION 5.2.1 .
Page 340 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK TABLE OF CONTENTS (Continued) Page 5.11 TIME, CONSUMPTION AND DESCENT DISTANCE 5.11.1 ..5.12 HOLDING TIME 5.12.1 ..........5.13 LANDING DISTANCES 5.13.1 .
Page 341 ICAO, Annex 16, 88 dB(A) 80.4 dB(A) Chapter 10, Appendix 6 TBM 700 airplane has received the noise limitation type certificate Nr N181 dated 31st January 1990 replaced by the Type Certificate Data Sheet EASA.A.010 on 14th July 2004. Rev. 13 Page 5.1.1...
Page 342 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 13 Page 5.1.2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 343 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK EASA Approved 5.1 - - FLYOVER NOISE LEVEL Flyover noise level measured in accordance with 14 CFR Part 36 Appendix F : 77.4 dB (A). NOTE : 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.
Page 344 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Page 5.1.2 Rev. 13 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 345 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK EASA Approved 5.2 - - AIRSPEED CALIBRATION NOTE : Indicated airspeeds (IAS) : instrument error supposed to be null (power configuration for cruise condition flight). FLAPS UP FLAPS TO FLAPS LDG LDG GR UP LDG GR DN LDG GR DN...
Page 346 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK EASA Approved FLAPS UP FLAPS TO FLAPS LDG LDG GR UP LDG GR DN LDG GR DN KIAS KCAS KIAS KCAS KIAS KCAS MPH IAS MPH CAS MPH IAS MPH CAS MPH IAS MPH CAS Figure 5.2.2 -- ALTERNATE STATIC SOURCE (BLEED LO)
Page 347 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK 5.3 - - CABIN PRESSURIZATION ENVELOPE Cabin altitude (feet) 8850 ft cabin 8000 PRESSURIZATION USEFUL 7000 ENVELOPE 6000 5000 ∆ P= 6.2 PSI max 4000 3000 2000 1000 Flight level (FL) Figure 5.3.1 -- CABIN PRESSURIZATION ENVELOPE Rev.
Page 348 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 5.3.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 349 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK 5.4 - - SAT - - IOAT CONVERSIONS NOTE : These indicated temperatures are available for stabilized cruise at normal operating power. ISA -- 20°C ISA -- 10°C ISA + 10°C ISA + 20°C Pressure altitude...
Page 350 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 5.4.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 351 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK EASA Approved 5.5 - - STALL SPEEDS CONFIG. BANK AIR-- FLIGHT 0° 30° 45° 60° PLANE IDLE WEIGHT Flaps KIAS KCAS KIAS KCAS KIAS KCAS KIAS KCAS 4850 lbs (2200 kg) 5512 lbs (2500 kg) 6579 lbs...
Page 352 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK EASA Approved INTENTIONALLY LEFT BLANK Rev. 13 Page 5.5.2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 353 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK 5.6 - - WIND COMPONENTS EXAMPLE : Angle between wind direction and flight path 50 ° Headwind 8 kts Crosswind 10 kts Wind speed 13 kts FLIGHT 25 kt : DEMONSTRATED CROSSWIND PATH 0˚...
Page 354 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 5.6.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 355 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK 5.7 - - ENGINE OPERATION The following tables must be used during normal operation of the airplane. The following conditions are given : -- Np = 2000 RPM, -- BLEED LO. The torque must be set at or below the value corresponding to the local conditions of flight level and temperature.
Page 356 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK ENGINE OPERATION Conditions : Maximum climb power (FL ≤ 200) Landing gear and flaps UP IAS = 130 KIAS -- Np = 2000 RPM -- BLEED LO NOTE : Add 1 % of TRQ for each additional 10 KCAS on climb airspeed T°...
Page 357 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK ENGINE OPERATION Conditions : Maximum climb power (FL 200) ≥ Landing gear and flaps UP IAS = 130 KIAS -- Np = 2000 RPM -- BLEED LO NOTE : Add 1 % of TRQ for each additional 10 KCAS on climb airspeed T°...
Page 358 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK Figure 5.7.2 -- ENGINE OPERATION Conditions : Maximum cruise power (FL 200) ≤ Landing gear and flaps UP Np = 2000 RPM -- BLEED LO NOTE : Use preferably recommended cruise power T°...
Page 359 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK ENGINE OPERATION Conditions : Maximum cruise power (FL 200) ≥ Landing gear and flaps UP Np = 2000 RPM -- BLEED LO NOTE : Use preferably recommended cruise power T° (°C) FLIGHT LEVEL (FL) IOAT -- 65...
Page 360 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK Figure 5.7.3 -- ENGINE OPERATION Conditions : Normal (recommended) cruise power (FL ≤ 200) Landing gear and flaps UP Np = 2000 RPM -- BLEED LO T° (°C) FLIGHT LEVEL (FL) IOAT -- 25 -- 15...
Page 361 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK ENGINE OPERATION Conditions : Normal (recommended) cruise power (FL 200) ≥ Landing gear and flaps UP Np = 2000 RPM -- BLEED LO T° (°C) FLIGHT LEVEL (FL) IOAT -- 65 -- 54 -- 63 -- 52...
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Page 363 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK EASA Approved 5.8 - - TAKEOFF DISTANCES WEIGHT : 5512 lbs (2500 kg) Associated conditions -- Landing gear DN and flaps TO -- 15° of attitude -- TRQ = 100 % -- Np = 2000 RPM -- BLEED LO -- Hard, dry and level runway -- GR = Ground roll (in ft)
Page 364 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK EASA Approved TAKEOFF DISTANCES WEIGHT : 6579 lbs (2984 kg) Associated conditions -- Landing gear DN and flaps TO -- 15° of attitude -- TRQ = 100 % -- Np = 2000 RPM -- BLEED LO -- Hard, dry and level runway -- GR = Ground roll (in ft) -- D...
Page 365 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK EASA Approved 5.9 - - CLIMB PERFORMANCE CLIMB SPEEDS (IAS = 130 KIAS) Conditions : Maximum climb power Landing gear and flaps UP IAS = 130 KIAS -- BLEED LO RATE OF CLIMB (ft/min) Pressure Airplane altitude...
Page 366 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK EASA Approved CLIMB PERFORMANCE CLIMB SPEEDS (IAS = 160 KIAS) Conditions : Maximum climb power Landing gear and flaps UP IAS = 160 KIAS -- BLEED LO RATE OF CLIMB (ft/min) Pressure Airplane altitude...
Page 367 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CLIMB PERFORMANCE TIME, CONSUMPTION AND CLIMB DISTANCE (IAS = 130 KIAS ) Conditions : ISA - 20°C Maximum climb power Landing gear and flaps UP IAS = 130 KIAS -- 2000 RPM -- BLEED LO NOTE : Time, consumption and distance from the 50 ft WEIGHT...
Page 368 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CLIMB PERFORMANCE TIME, CONSUMPTION AND CLIMB DISTANCE (IAS = 130 KIAS) Conditions : Maximum climb power Landing gear and flaps UP IAS = 130 KIAS -- 2000 RPM -- BLEED LO NOTE : Time, consumption and distance from the 50 ft WEIGHT...
Page 369 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CLIMB PERFORMANCE TIME, CONSUMPTION AND CLIMB DISTANCE (IAS = 130 KIAS) Conditions : ISA + 20 ° Maximum climb power Landing gear and flaps UP IAS = 130 KIAS -- 2000 RPM -- BLEED LO NOTE : Time, consumption and distance from the 50 ft WEIGHT...
Page 370 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CLIMB PERFORMANCE TIME, CONSUMPTION AND CLIMB DISTANCE (IAS = 160 KIAS) Conditions : ISA - 20 ° Maximum climb power Landing gear and flaps UP IAS = 160 KIAS up to 20000 ft ; -- 4 KIAS / 2000 ft then 2000 RPM -- BLEED LO NOTE : Time, consumption and distance from the 50 ft...
Page 371 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CLIMB PERFORMANCE TIME, CONSUMPTION AND CLIMB DISTANCE (IAS = 160 KIAS) Conditions : Maximum climb power Landing gear and flaps UP IAS = 160 KIAS up to 20000 ft ; -- 4 KIAS / 2000 ft then 2000 RPM -- BLEED LO NOTE : Time, consumption and distance from the 50 ft...
Page 372 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CLIMB PERFORMANCE TIME, CONSUMPTION AND CLIMB DISTANCE (IAS = 160 KIAS) Conditions : ISA + 20°C Maximum climb power Landing gear and flaps UP IAS = 160 KIAS up to 20000 ft ; -- 4 KIAS / 2000 ft then 2000 RPM -- BLEED LO NOTE : Time, consumption and distance from the 50 ft...
Page 373 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CLIMB PERFORMANCE CLIMB PERFORMANCE AFTER GO- -AROUND Conditions : Maximum climb power Landing gear DN and flaps LDG IAS = 90 KIAS RATE OF CLIMB (ft/min) Pressure Pressure Airplane Airplane altitude weight (feet) -- 35°C...
Page 374 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CLIMB PERFORMANCE CLIMB PERFORMANCE - - FLAPS TO Conditions : Climb maximum power Landing gear UP and flaps TO IAS = 110 KIAS RATE OF CLIMB (ft/min) Pressure Pressure Airplane Airplane altitude weight (feet)
Page 375 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK 5.10 - - CRUISE PERFORMANCE Conditions : ISA Weight 5512 lbs (2500 kg) Flight level (FL) IRCR NOCR MXCR LRCR (KTAS) Figure 5.10.1 -- CRUISE PERFORMANCE Rev. 2 Page 5.10.1 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 376 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Maximum cruise Conditions : ISA - 20°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Use preferably recommended cruise power AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs...
Page 377 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Maximum cruise Conditions : ISA - 10°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Use preferably recommended cruise power AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs...
Page 378 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Maximum cruise Conditions : ISA - 5°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Use preferably recommended cruise power AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs...
Page 379 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Maximum cruise Conditions : ISA Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Use preferably recommended cruise power AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs Pressure...
Page 380 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Maximum cruise Conditions : ISA + 5°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Use preferably recommended cruise power AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs...
Page 381 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Maximum cruise Conditions : ISA + 10°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Use preferably recommended cruise power AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs...
Page 382 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Maximum cruise Conditions : ISA + 20°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Use preferably recommended cruise power AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs...
Page 383 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Normal (recommended) cruise Conditions : ISA - 20°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Power recommended by PRATT & WHITNEY CANADA AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs...
Page 384 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Normal (recommended) cruise Conditions : ISA - 10°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Power recommended by PRATT & WHITNEY CANADA AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs...
Page 385 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Normal (recommended) cruise Conditions : ISA - 5°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Power recommended by PRATT & WHITNEY CANADA AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs...
Page 386 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Normal (recommended) cruise Conditions : ISA Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Power recommended by PRATT & WHITNEY CANADA AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs...
Page 387 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Normal (recommended) cruise Conditions : ISA + 5°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Power recommended by PRATT & WHITNEY CANADA AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs...
Page 388 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Normal (recommended) cruise Conditions : ISA + 10°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Power recommended by PRATT & WHITNEY CANADA AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs...
Page 389 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Normal (recommended) cruise Conditions : ISA + 20°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO NOTE : Power recommended by PRATT & WHITNEY CANADA AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs...
Page 390 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Intermediate cruise Conditions : ISA - 20°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs Pressure IOAT altitude (2200 kg)
Page 391 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Intermediate cruise Conditions : ISA - 10°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs Pressure IOAT altitude (2200 kg)
Page 392 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Intermediate cruise Conditions : ISA - 5°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs Pressure IOAT altitude (2200 kg)
Page 393 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Intermediate cruise Conditions : ISA Landing gear and flaps UP 2000 RPM (*) -- BLEED LO AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs Pressure IOAT altitude (2200 kg) (2500 kg) (2800 kg)
Page 394 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Intermediate cruise Conditions : ISA + 5°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs Pressure IOAT altitude (2200 kg)
Page 395 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Intermediate cruise Conditions : ISA + 10°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs Pressure IOAT altitude (2200 kg)
Page 396 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Intermediate cruise Conditions : ISA + 20°C Landing gear and flaps UP 2000 RPM (*) -- BLEED LO AIRSPEEDS (kt) Fuel flow 4850 lbs 5512 lbs 6173 lbs Pressure IOAT altitude (2200 kg)
Page 397 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Long Range Cruise (5512 lbs - 2500 kg) IOAT : ° C LEGEND : IAS : KIAS Conditions : Landing gear and flaps UP : us gal/h 2000 RPM (*) -- BLEED LO : lbs/h TAS : KTAS Presssure...
Page 398 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK CRUISE PERFORMANCE Long Range Cruise (6173 lbs - 2800 kg) IOAT : ˚C LEGEND : IAS : KIAS Conditions : Landing gear and flaps UP : us gal/h : lbs/h TAS : KTAS 2000 RPM (*) -- BLEED LO Presssure altitude...
Page 399 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK 5.11 - - TIME, CONSUMPTION AND DESCENT DISTANCE Conditions : Power as required to maintain constant Vz Landing gear and flaps UP CAS = 230 KCAS -- 2000 RPM -- BLEED LO Vz = 1500 ft/min Vz = 2000 ft/min Vz = 2500 ft/min...
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Page 401 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK 5.12 - - HOLDING TIME Conditions : Landing gear and flaps UP IAS = 120 KIAS -- 2000 RPM -- BLEED LO 30 % FUEL USED DURING HOLDING TIME Weight 4850 lbs (2200 kg) Weight 5512 lbs (2500 kg) Pressure Pressure...
Page 402 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 5.12.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 403 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK EASA Approved 5.13 - - LANDING DISTANCES WEIGHT : 6250 lbs (2835 kg) Associated conditions Landing gear DN and flaps LDG Approach speed IAS = 80 KIAS Touch--down speed IAS = 65 KIAS Maximum braking without reverse Hard, dry and level runway GR = Ground roll (in ft)
Page 404 T B M SECTION 5 PERFORMANCE PILOT’S OPERATING HANDBOOK EASA Approved LANDING DISTANCES WEIGHT : 5071 lbs (2300 kg) Associated conditions Landing gear DN and flaps LDG Approach speed IAS = 80 KIAS Touch--down speed IAS = 60 KIAS Maximum braking without reverse Hard, dry and level runway GR = Ground roll (in ft) = Landing distance (clear to 50 ft) (in ft)
Page 405 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK SECTION 6 WEIGHT AND BALANCE TABLE OF CONTENTS Page GENERAL 6.1.1 ........... AIRPLANE WEIGHING PROCEDURES 6.2.1 .
Page 406 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 6.0.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 407 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK 6.1 - - GENERAL This section is intended to provide the pilot with the procedure to determine the weight and balance of the airplane. A list of equipment available for this airplane is included at the end of this section.
Page 408 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 6.1.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 409 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK 6.2 - - AIRPLANE WEIGHING PROCEDURES Refer to Maintenance Manual for the procedures to use. NOTE : Weighing carried out at the factory takes into account all equipment installed on the airplane.
Page 410 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 6.2.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 411 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK 6.3 - - BAGGAGE LOADING There are two baggage compartments : -- one in fuselage non pressurized forward section, between firewall and cockpit with maximum baggage capacity of 110 lbs (50 kg). -- the other one is in the rear of the pressurized cabin with maximum baggage capacity of 220 lbs (100 kg).
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Page 413 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK 6.4 - - DETERMINING WEIGHT AND BALANCE GENERAL This section is intended to provide the pilot with the procedure to detemine the weight and balance of the airplane. IT IS THE PILOT’S RESPONSIBILITY TO ENSURE THAT THE AIRPLANE IS PROPERLY LOADED AND THE WEIGHT AND BALANCE LIMITS ARE ADHERED TO.
Page 414 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK 5) Compute Zero Fuel Weight arm (5) and CG (MAC %) (5c) using given formulas. 6) Record the loaded Fuel (6a) and compute associated moment (6b). 7) Compute Ramp Weight (7a) and moment (7b) as sum of Zero Fuel Weight (3a) + loaded Fuel (6a) and moments (3b) + (6b).
Page 415 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK AIRPLANE LOADING FORM (m, kg) - - Valid from S / N 1 to 23, 25, 28, 33 and 35, except airplanes equipped as a retrofit with modification Nr MOD 70- -019- -25 ( Arm (m) −...
Page 416 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK EXAMPLE OF AIRPLANE WEIGHT AND BALANCE REPORT NOTE : Airplane original report shall be kept with the airplane POH. Figure 6.4.1 -- Example of Weight and Balance Report and basic airplane characteristics, in kg and m Page 6.4.4 Rev.
Page 417 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK NOTE : Airplane original report shall be kept with the airplane POH. Figure 6.4.2 -- Example of Weight and Balance Report and basic airplane characteristics, in lb and in Rev.
Page 418 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT AND BALANCE FORM AND DIAGRAM (m, kg) - - Valid from S / N 1 to 23, 25, 28, 33 and 35, except airplanes equipped as a retrofit with modification Nr MOD 70- -019- -25 ( Arm (m) −...
Page 419 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK Figure 6.4.3 -- Weight and Balance diagram Rev. 15 Page 6.4.7 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 420 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT AND BALANCE FORM AND DIAGRAM (m, kg) - - Valid for S / N 24, 26, 27, 29 to 32, 34, 36 to 9999, plus airplanes equipped as a retrofit with modification Nr MOD 70- -019- -25 ( Arm (m) −...
Page 421 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK Figure 6.4.4 -- Weight and Balance diagram Rev. 15 Page 6.4.9 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 422 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT AND BALANCE FORM AND DIAGRAM (in, lbs) - - Valid from S / N 1 to 23, 25, 28, 33 and 35, except airplanes equipped as a retrofit with modification Nr MOD 70- -019- -25 ( Arm (in) −...
Page 423 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK Figure 6.4.5 -- Weight and Balance diagram Rev. 15 Page 6.4.11 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 424 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT AND BALANCE FORM AND DIAGRAM (in, lbs) - - Valid for S / N 24, 26, 27, 29 to 32, 34, 36 to 9999, plus airplanes equipped as a retrofit with modification Nr MOD 70- -019- -25 ( Arm (in) −...
Page 425 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK Figure 6.4.6 -- Weight and Balance diagram Rev. 15 Page 6.4.13 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
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Page 427 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT AND BALANCE SAMPLES (m, kg) - - Valid from S / N 1 to 23, 25, 28, 33 and 35, except airplanes equipped as a retrofit with modification Nr MOD 70- -019- -25 CAUTION LOADING SAMPLES (FIGURE 6.4.7 OR 6.4.8) ARE ONLY GIVEN AS AN EXAMPLE ;...
Page 428 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ( Arm (m) − 4.392 ) Moment = Weight x Arm CG (MAC %) = × 100 1.51 Weight Moment Item (kg) (m.kg) (MAC %) Empty Weight (kg) 1 860 4.633 8 618 Baggage FWD...
Page 429 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK Figure 6.4.7 -- Loading sample Rev. 15 Page 6.4.17 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
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Page 431 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT AND BALANCE SAMPLES (in, lbs) - - Valid for S / N 24, 26, 27, 29 to 32, 34, 36 to 9999, plus airplanes equipped as a retrofit with modification Nr MOD 70- -019- -25 CAUTION LOADING SAMPLES (FIGURE 6.4.7 OR 6.4.8) ARE ONLY...
Page 432 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ( Arm (in) − 172.93 ) Moment = Weight x Arm CG (MAC %) = × 100 59.45 Weight Moment Item (lbs) (in) (in.lbs) (MAC %) Empty Weight (lbs) 4 300 183.1 787 402...
Page 433 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK Figure 6.4.8 -- Weight and Balance diagram Rev. 15 Page 6.4.21 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 434 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK DETERMINING EMPTY AIRPLANE CHARACTERISTICS Empty airplane characteristics (weight and balance) may vary with regard to those indicated on weighing form according to installed optional equipment. List of equipment (paragraph 6.5) contains the standard and optional equipment, as well as their characteristics (weight, arm).
Page 435 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ( do − 172.93 ) CG m.a.c.% = × 100 59.45 Use the above formula to express arm ”d ” in % of mean aerodynamic chord. NOTE : Arm expressed in inches with regard to reference. Front seats : 180.5 in.
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Page 437 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK 6.5 - - LIST OF EQUIPMENT The following list contains standard equipment installed on each airplane and available optional equipment. A separate list of equipment of items installed at the factory in your specific airplane is provided in your airplane file.
Page 438 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 01 - - SPECIFIC OPTIONAL EQUIPMENT 01008 Flight inspection system capability NAVCAL 97.223 231.69...
Page 439 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 21 - - ENVIRONMENTAL SYSTEM 21- -20 - - Distribution Cabin fan AVVC 00244 VETUS...
Page 440 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 0285--21 Ground conditioning fan -- SOCATA 13.911 90.55 Version B (6.310) (2.300) (TBM 700B)
Page 441 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 22 - - AUTO FLIGHT NOTE : KFC 325 autopilot is included in EFIS equipment (ATA 34) AFC air data computer KDC 222...
Page 442 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) Yaw rate gyro KRG 331 HONEYWELL 0.750 171.26 P/N 060--00024--0000 (0.340) (4.350) 22002...
Page 443 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 23 - - COMMUNICATIONS Antenna 16--21B--P3 CHELTON 1.036 192.91 (0.470) 267.72 (4.900 6.800)
Page 444 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) O 23005A COM1--NAV # 1 KX 165--25 KING 151.73 ∆--3.440 without EFIS (∆--1.560) (3.854)
Page 445 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) A 23013B VHF COM antenna 16--41--XX CHELTON 1.036 272.28 under fuselage (0.470) (6.916) A 23013C VHF COM antenna...
Page 446 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 23023 Audio selector and Marker GARMIN 1.609 129.05 GMA 340 (0.730) (3.278) A 23024A COM/NAV/GPS # 1 (B--RNAV)
Page 447 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 24 - - ELECTRICAL POWER 24- -30 - - DC generation Ammeter 12--1200--9L 28 0.309...
Page 448 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) O 24001B Battery with temperature sensor SAFT 82.849 112.20 4076--10 (37.580) (2.850) O 24002A Lead--Acid battery...
Page 449 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 25 - - EQUIPMENT AND FURNISHINGS 25001A Toilets SOCATA 30.055 285.91 (13.633) (7.262)
Page 450 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 25006E Storage box -- Composite SOCATA 16.314 202.76 (7.400) (5.150) 25006F Refreshment cabinet -- Composite SOCATA...
Page 451 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 25021A Coat hanger SOCATA Negligible 25022A Upholstery panels modifications -- SOCATA ∆...
Page 452 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 0174--25 Optional 12 V plugs SOCATA 3.31 195.28 (1.500) (4.960) A 0246--25B Potty seat (Chemical toilets cabinet) DOMETIQUE/ 54.23...
Page 453 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) Seats (6 places with or without oxygen equipment) -- Post--MOD70--019--25 Valid S/N 24, 26, 27, 29 to 32, 34, 36 to 9999 : .
Page 454 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) . Intermediate seats (R.H. and 25.507 218.31 L.H.) (back to flight direction) (11.570) (5.545) (TBM700A)
Page 455 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) . L.H. intermediate seat (back to SOCATA 24.25 218.30 flight direction) T700A2522000 (11.000) (5.545) (TBM700A)
Page 456 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) . Front R.H. seat SOCATA 24.250 180.30 (11.000) (4.580) . L.H. intermediate seat (back to SOCATA 23.148 217.72...
Page 457 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) . L.H. intermediate seat (back to 218.31 flight direction) (5.545) .
Page 458 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 25016B Three--frequency emergency SOCATA locator transmitter (TSO) ELT 97 -- TBM700A 3.638 297.64 (1.650)
Page 459 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 26 - - FIRE PROTECTION 26001A Portable fire extinguisher unit (TBM 700A) FH 15 N AREOFEU...
Page 460 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 27 - - FLIGHT CONTROLS 27- -10 - - Roll control Roll trim actuator 145700.01 LPMI...
Page 461 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 28 - - FUEL SYSTEM 28- -20 - - Fuel supply Electric boost pump 2003--B WELDON...
Page 462 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) Fuel pressure indicator 19--3005 0.309 157.48 or PC99--06 FALGAYRAS (0.140) (4.000) Inboard L.H.
Page 463 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 30 - - ICE AND RAIN PROTECTION Deicer, L.H. elevator horn SOCATA 3.307 403.15...
Page 464 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) Deicer, outboard L.H. wing SOCATA 2.646 173.23 T700A3010012000 (1.200) (4.400) (with radar OPT70 34007A) 30- -40 - - Windshield deicing Windshield heater controller...
Page 465 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 31 - - INDICATING/RECORDING SYSTEMS 31- -20 - - Independent instruments Chronometer M800 (28V)
Page 466 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 32 - - LANDING GEARS 32- -10 - - Main landing gear L.H.
Page 467 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 0342--52 Lower main landing gear doors SOCATA 6.614 204.33 (R.H. and L.H.) (3.000) (5.190) 32- -35 - - Hydraulic generation...
Page 468 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 0408--32 Nose tire 5.00--5--10PR GOODYEAR 6.834 89.57 (3.100) (2.275) Nose tire 5.00x5--10--120TL AVIATOR 5.600...
Page 469 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 33 - - LIGHTS 33- -10 - - Instrument panel lighting L.H.
Page 470 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) Cont’d -- L.H. navigation light assy WHELEN 0.507 185.04 A600 PR D28 (0.230) (4.700) R.H.
Page 471 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34 - - NAVIGATION 34036A COM--NAV KX 165 -- SINGLE KING 1.301 151.57...
Page 472 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) Vertical speed indicator 3” UNITED 1.213 157.48 7060 C.118 INSTRUMENTS (0.550) (4.000)
Page 473 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -13 - - Outside temperature Outside air temperature indicator DAVTRON 0.265 157.48...
Page 474 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -24 - - ADI and standby horizon ADI flight director KI 256 KING 3.307...
Page 475 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -25 - - Radio magnetic indication RMI 1 KI 229 KING (See ATA 34--54)
Page 476 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34020E RMI 1 KNI 582 HONEYWELL 7.738 214.45 (L.H. instrument panel) (3.510) (5.447) EFIS coupled...
Page 477 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) O 34001C EFIS (EFS 40 + AP KFC 325) : KING -- with DME KDI 574...
Page 478 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34041A Stormscope WX 950 4.700 191.85 (2.130) (4.873) 34056A Stormscope WX 500 4.938 232.28...
Page 479 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34008F Graphic weather radar RDS 82 VP KING 33.510 162.68 EFIS coupled, with KNS 81 (15.200)
Page 480 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -43 - - Radioaltimeter 34010A Radioaltimeter KRA 10A KING 5.291 325.98...
Page 481 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) Cont’d . Antennas (Qty 2) DM 19--2--1 DORNE & 0.40 182.09 MARGOLIN...
Page 482 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) Cont’d . Antennas (Qty 2) DM 19--2--1 DORNE & 0.40 182.09 MARGOLIN...
Page 483 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34059B SKYWATCH HP Traffic advisory 12.720 151.18 system SKY 899 (5.770) (3.840) EFIS and TAS coupled...
Page 484 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34061C TAS + TAWS system KMH 880 HONEYWELL 15.65 158.42 (with indicator on MFD KMD 850 or (7.10)
Page 485 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) VHF GS--NAV antenna DORNE & 3.307 401.57 DM N4--17N MARGOLIN (1.500) (10.200)
Page 486 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) A 34021G Transponder # 2 KT 76C+ HONEYWELL 3.175 150.59 (interfaced with encoding (1.440)
Page 487 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -54 - - Automatic Direction Finder (ADF) ADF (basic) : -- Receiver KR 87 KING...
Page 488 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34055A ADF SC+ : -- Receiver KR87/Indicator KI227 HONEYWELL 3.902 157.48 P/N 066--01072--0014...
Page 489 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -56 - - LORAN- -C 34005A LORAN--C KLN 88 KING 12.566 168.11...
Page 490 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -60 - - Flight management computing 34- -61 - - Moving map display system 34042B Moving map display ARGUS...
Page 491 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 35 - - OXYGEN Generator 117024--02 PURITAN 0.948 180.31 (0.430) (4.580) 209.84...
Page 492 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 37 - - VACUUM Air ejector valve 19E17--5A LUCAS 0.661 116.14 (0.300)
Page 493 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 52 - - DOORS 52002A ”Pilot” door SOCATA 44.092 171.26 (TBM700B) (20.000)
Page 494 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 56 - - WINDOWS 56001A Deiced R.H. windshield ∆ 1.764 158.27 (∆...
Page 495 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 57 - - WINGS 57001A Utilization on runways covered SOCATA 200.00 ∆--7.716...
Page 496 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 61 - - PROPELLER 61- -10 - - Propeller assembly Propeller (4--blade) HARTZELL 153.220...
Page 497 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 71 - - POWER PLANT Turboprop engine PT6 A--64 P &...
Page 498 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 77 - - ENGINE INDICATING Compressor turbine QPL (AIRCRAFT 0.981 108.27 tacho--generator (Ng)
Page 499 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) Flowmeter 90 12 00 : -- Indicator 912080--38 SHADIN 0.930 143.70 or 912080--38A...
Page 500 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 79 - - LUBRICATION 79- -20 - - Distribution Oil cooler L8538233 LORI...
Page 501 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK 6.5 - - LIST OF EQUIPMENT The following list contains standard equipment installed on each airplane and available optional equipment. A separate list of equipment of items installed at the factory in your specific airplane is provided in your airplane file.
Page 502 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 01 - - SPECIFIC OPTIONAL EQUIPMENT S 01004A Brazil certification markings SOCATA 01008 Flight inspection system capability...
Page 503 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 21 - - ENVIRONMENTAL SYSTEM 21- -20 - - Distribution Cabin fan AVVC 00244 VETUS...
Page 504 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 0285--21 Ground conditioning fan -- SOCATA 13.911 90.55 Version B (6.310) (2.300) (TBM 700B)
Page 505 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 22 - - AUTO FLIGHT NOTE : KFC 325 autopilot is included in EFIS equipment (ATA 34) AFC air data computer KDC 222...
Page 506 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) Yaw rate gyro KRG 331 HONEYWELL 0.750 171.26 P/N 060--00024--0000 (0.340) (4.350) 22002...
Page 507 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 23 - - COMMUNICATIONS Antenna 16--21B--P3 CHELTON 1.036 192.91 (0.470) 267.72 (4.900 6.800)
Page 508 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) O 23005A COM1--NAV # 1 KX 165--25 KING 151.73 ∆--3.440 without EFIS (∆--1.560) (3.854)
Page 509 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) A 23013B VHF COM antenna 16--41--XX CHELTON 1.036 272.28 under fuselage (0.470) (6.916) A 23013C VHF COM antenna...
Page 510 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 23023 Audio selector and Marker GARMIN 1.609 129.05 GMA 340 (0.730) (3.278) A 23024A COM/NAV/GPS # 1 (B--RNAV)
Page 511 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 24 - - ELECTRICAL POWER 24- -30 - - DC generation Ammeter 12--1200--9L 28 0.309...
Page 512 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) O 24001B Battery with temperature sensor SAFT 82.849 112.20 4076--10 (37.580) (2.850) O 24002A Lead--Acid battery...
Page 513 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 25 - - EQUIPMENT AND FURNISHINGS 25001A Toilets SOCATA 30.055 285.91 (13.633) (7.262)
Page 514 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 25006E Storage box -- Composite SOCATA 16.314 202.76 (7.400) (5.150) 25006F Refreshment cabinet -- Composite SOCATA...
Page 515 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 25021A Coat hanger SOCATA Negligible 25022A Upholstery panels modifications -- SOCATA ∆...
Page 516 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 0174--25 Optional 12 V plugs SOCATA 3.31 195.28 (1.500) (4.960) A 0246--25B Potty seat (Chemical toilets cabinet) DOMETIQUE/ 54.23...
Page 517 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) Seats (6 places with or without oxygen equipment) -- Post--MOD70--019--25 Valid S/N 24, 26, 27, 29 to 32, 34, 36 to 9999 : .
Page 518 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) . Intermediate seats (R.H. and 25.507 218.31 L.H.) (back to flight direction) (11.570) (5.545) (TBM700A)
Page 519 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) . L.H. intermediate seat (back to SOCATA 24.25 218.30 flight direction) T700A2522000 (11.000) (5.545) (TBM700A)
Page 520 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) . Front R.H. seat SOCATA 24.250 180.30 (11.000) (4.580) . L.H. intermediate seat (back to SOCATA 23.148 217.72...
Page 521 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) . L.H. intermediate seat (back to 218.31 flight direction) (5.545) .
Page 522 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 25016B Three--frequency emergency SOCATA locator transmitter (TSO) ELT 97 -- TBM700A 3.638 297.64 (1.650)
Page 523 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 26 - - FIRE PROTECTION 26001A Portable fire extinguisher unit (TBM 700A) FH 15 N AREOFEU...
Page 524 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 27 - - FLIGHT CONTROLS 27- -10 - - Roll control Roll trim actuator 145700.01 LPMI...
Page 525 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 28 - - FUEL SYSTEM 28- -20 - - Fuel supply Electric boost pump 2003--B WELDON...
Page 526 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) Fuel pressure indicator 19--3005 0.309 157.48 or PC99--06 FALGAYRAS (0.140) (4.000) Inboard L.H.
Page 527 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 30 - - ICE AND RAIN PROTECTION Deicer, L.H. elevator horn SOCATA 3.307 403.15...
Page 528 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) Deicer, outboard L.H. wing SOCATA 2.646 173.23 T700A3010012000 (1.200) (4.400) (with radar OPT70 34007A) 30- -40 - - Windshield deicing Windshield heater controller...
Page 529 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD (S) ITEM EQUIPMENT per unit OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 31 - - INDICATING/RECORDING SYSTEMS 31- -20 - - Independent instruments Chronometer M800 (28V)
Page 530 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 32 - - LANDING GEARS 32- -10 - - Main landing gear L.H.
Page 531 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 0342--52 Lower main landing gear doors SOCATA 6.614 204.33 (R.H. and L.H.) (3.000) (5.190) 32- -35 - - Hydraulic generation...
Page 532 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 0408--32 Nose tire 5.00--5--10PR GOODYEAR 6.834 89.57 (3.100) (2.275) Nose tire 5.00x5--10--120TL AVIATOR 5.600...
Page 533 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) 33 - - LIGHTS 33- -10 - - Instrument panel lighting L.H.
Page 534 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK WEIGHT REQUIRED (R) OR STANDARD ITEM EQUIPMENT per unit (S) OR OPTIONAL (A or O) OPT70 SUPPLIER EQUIPMENT (kg) Cont’d -- L.H. navigation light assy WHELEN 0.507 185.04 A600 PR D28 (0.230) (4.700) R.H.
Page 535 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34 - - NAVIGATION 34036A COM--NAV KX 165 -- SINGLE KING 1.301 151.57...
Page 536 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) Vertical speed indicator 3” UNITED 1.213 157.48 7060 C.118 INSTRUMENTS (0.550) (4.000)
Page 537 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -13 - - Outside temperature Outside air temperature indicator DAVTRON 0.265 157.48...
Page 538 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -24 - - ADI and standby horizon ADI flight director KI 256 KING 3.307...
Page 539 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -25 - - Radio magnetic indication RMI 1 KI 229 KING (See ATA 34--54)
Page 540 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34020E RMI 1 KNI 582 HONEYWELL 7.738 214.45 (L.H. instrument panel) (3.510) (5.447) EFIS coupled...
Page 541 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) O 34001C EFIS (EFS 40 + AP KFC 325) : KING -- with DME KDI 574...
Page 542 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34041A Stormscope WX 950 4.700 191.85 (2.130) (4.873) 34056A Stormscope WX 500 4.938 232.28...
Page 543 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34008F Graphic weather radar RDS 82 VP KING 33.510 162.68 EFIS coupled, with KNS 81 (15.200)
Page 544 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -43 - - Radioaltimeter 34010A Radioaltimeter KRA 10A KING 5.291 325.98...
Page 545 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) Cont’d . Antennas (Qty 2) DM 19--2--1 DORNE & 0.40 182.09 MARGOLIN...
Page 546 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) Cont’d . Antennas (Qty 2) DM 19--2--1 DORNE & 0.40 182.09 MARGOLIN...
Page 547 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34059B SKYWATCH HP Traffic advisory 12.720 151.18 system SKY 899 (5.770) (3.840) EFIS and TAS coupled...
Page 548 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34061C TAS + TAWS system KMH 880 HONEYWELL 15.65 158.42 (with indicator on MFD KMD 850 or (7.10)
Page 549 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) VHF GS--NAV antenna DORNE & 3.307 401.57 DM N4--17N MARGOLIN (1.500) (10.200)
Page 550 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) A 34021G Transponder # 2 KT 76C+ HONEYWELL 3.175 150.59 (interfaced with encoding (1.440)
Page 551 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -54 - - Automatic Direction Finder (ADF) ADF (basic) : -- Receiver KR 87 KING...
Page 552 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34055A ADF SC+ : -- Receiver KR87/Indicator KI227 HONEYWELL 3.902 157.48 P/N 066--01072--0014...
Page 553 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -56 - - LORAN- -C 34005A LORAN--C KLN 88 KING 12.566 168.11...
Page 554 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 34- -60 - - Flight management computing 34- -61 - - Moving map display system 34042B Moving map display ARGUS...
Page 555 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 35 - - OXYGEN Generator 117024--02 PURITAN 0.948 180.31 (0.430) (4.580) 209.84...
Page 556 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 37 - - VACUUM Air ejector valve 19E17--5A LUCAS 0.661 116.14 (0.300)
Page 557 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 52 - - DOORS 52002A ”Pilot” door SOCATA 44.092 171.26 (TBM700B) (20.000)
Page 558 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 56 - - WINDOWS 56001A Deiced R.H. windshield ∆ 1.764 158.27 (∆...
Page 559 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 57 - - WINGS 57001A Utilization on runways covered SOCATA 200.00 ∆--7.716...
Page 560 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 61 - - PROPELLER 61- -10 - - Propeller assembly Propeller (4--blade) HARTZELL 153.220...
Page 561 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 71 - - POWER PLANT Turboprop engine PT6 A--64 P &...
Page 562 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 77 - - ENGINE INDICATING Compressor turbine QPL (AIRCRAFT 0.981 108.27 tacho--generator (Ng)
Page 563 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) Flowmeter 90 12 00 : -- Indicator 912080--38 SHADIN 0.930 143.70 or 912080--38A...
Page 564 T B M SECTION 6 WEIGHT AND BALANCE PILOT’S OPERATING HANDBOOK ITEM WEIGHT REQUIRED (R) OR STANDARD (S) OPT70 EQUIPMENT per unit OR OPTIONAL (A or O) SUPPLIER EQUIPMENT MOD70 (kg) 79 - - LUBRICATION 79- -20 - - Distribution Oil cooler L8538233 LORI...
Page 565 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK SECTION 7 DESCRIPTION TABLE OF CONTENTS Page GENERAL 7.1.1 ..........AIRFRAME 7.2.1 .
Page 566 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK TABLE OF CONTENTS (Continued) Page POWERPLANT 7.6.1 ..........7.6.1 TURBOPROP ENGINE OPERATION .
Page 567 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK TABLE OF CONTENTS (Continued) Page AIR CONDITIONING AND PRESSURIZATION 7.9.1 ... . 7.9.1 AIR CONDITIONING ..........7.9.5 PRESSURIZATION .
Page 568 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 7.0.4 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 569 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.1 - - GENERAL This Section provides description and operation of the TBM 700 airplane and its systems. Some of the equipment described herein is optional and may not be installed in the airplane. Details of other optional systems and equipment are presented in Section 9 ”Supplements”...
Page 570 T B M SECTION 0 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 7.1.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 571 SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.2 - - AIRFRAME The TBM 700 is a six / seven--place, low wing airplane. The structure is a semi--monocoque all--metal construction and is equipped with a retractable tricycle landing gear. TBM700A : The pressurized cabin is equipped, on the left side of fuselage, with a two--piece door comprising integrated stairs allowing pilot and passengers boarding.
Page 572 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.2.1 -- CABIN ARRANGEMENT Rev. 13 Page 7.2.2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 573 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK WINGS The wings are monocoque, bi--spar structures. Main spars of each wing are linked to the fuselage by two integral attach fittings. Each wing contains a main landing gear well and sealed casings forming the fuel tank. The wing leading edge is equipped with a deicing system.
Page 574 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Wings characteristics : Area ......... 193.75 sq.
Page 575 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Geared motor 2) Internal actuator 3) Intermediate bearings 4) Wing flap 5) External actuator 6) Rods 7) Position indicator 8) Control selector Figure 7.2.2 (1/2) -- WING FLAPS Rev. 11 Page 7.2.5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 576 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.2.2 (2/2) -- WING FLAPS Page 7.2.6 Rev. 7 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 577 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK EMPENNAGES Empennages are composite structures. The horizontal empennage consists of a horizontal stabilizer (PHF), control surfaces and elevator trim tabs ; the vertical empennage consists of a vertical stabilizer, the rudder and the rudder trim tab.
Page 578 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 7.2.8 Rev. 7 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 579 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.3 - - ACCOMODATIONS INSTRUMENT PANEL (Figure 7.3.1) The instrument panel contains instruments and controls necessary for flight monitoring. The typical instrument panel consists of all standard equipment, as well as additional optional equipment. Upper panel (Figure 7.3.2) The upper panel located at the top part of the windshield, contains electrical generation control panels, engine starting and ancillary electrical systems.
Page 580 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Central pedestal (Figure 7.3.6) The central pedestal under the radio rack, comprises position indicators and trim tabs controls, flaps, engine controls and fuel tank selector. Circuit breakers panel (Figures 7.3.7 and 7.8.2) Circuit breakers for all electrical equipment supplied by bus bars are located on a separate panel installed on the left side of cockpit, near the pilot or on right side when the airplane is equipped with a ”pilot”...
Page 581 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK The system uses : -- the stall warning horn, -- the VMO alarm, -- AP alarms, -- the landing gear control unit, -- the flap geared motor, -- (if installed) the radar altimeter aural warning. Aural warning box The aural warning box consists of a box including logic circuits, which create the signals heard in the aural warning loud--speaker.
Page 582 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Upper panel (Figures 7.3.2 and 7.3.2A) The upper panel includes following elements : -- the alarm loud--speaker (landing gear up with flaps extended and / or idle, stall), -- the altitude preselection indicating buzzer, -- the autopilot disconnection indicating buzzer, -- the VMO alarm buzzer, -- the ”HORN TEST”...
Page 583 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK The ”HORN TEST” knob allows to test the correct operation of aural warnings : -- Set the ”SOURCE” selector to ”BAT” or to ”GPU”. -- Push and hold the ”HORN TEST” knob : .
Page 584 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 7.3.2D Rev. 6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 585 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.1 -- INSTRUMENT PANEL ASSEMBLY (Typical arrangement) Rev. 9 Page 7.3.3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 586 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) L. H. side upper panel postlight 2) Buzzers (AP, landing gear not extended and V alarms) 3) Loud--speakers (radio and stall warning horn) 4) Cockpit floodlights (instrument panel emergency lighting) 5) R.
Page 587 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.2 (2/2) -- UPPER PANEL AND COCKPIT OVERHEAD PANEL Typical arrangement -- Valid S / N 1 to 23, 25, 28, 33 and 35, except airplanes equipped as a retrofit with modification Nr MOD 70--019--25 Rev.
Page 588 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) L.H. instrument panel emergency lighting 2) Buzzers (AP, landing gear not extended and V alarms) 3) Loud--speakers (radio and stall warning horn) 4) R.H. instrument panel emergency lighting 5) Cockpit floodlight switches (rheostats) 6) R.
Page 589 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.2A (2/2) -- UPPER PANEL AND COCKPIT OVERHEAD PANEL Typical arrangement -- Valid S / N 24, 26, 27, 29 to 32, 34, 36 to 9999, plus airplanes equipped as a retrofit with modification Nr MOD 70--019--25 Rev.
Page 590 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 23) Landing gear configuration 1) ”DE SYSTEM” panel control panel postlight (Figure 7.5.1) 2) OAT indicator 24) Chronometer 3) Turn coordinator 25) Oxygen mask microphone 4) VOR / ILS 2 switch (Figure 7.10.1) 5) Suction indicator 26) Parking brake control 6) Airspeed indicator...
Page 591 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.3 (2/2) -- LEFT INSTRUMENT PANEL (Typical arrangement) Rev. 13 Page 7.3.7 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 592 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Stand--by compass 2) AP mode controller (see Section 9) 3) Advisory panel (Figure 7.3.8) 4) KMA selection box 5) VHF 1 6) RNAV 7) VHF 2 / VOR 2 8) ADF 9) ATC 10) DME 11) Cabin interior lighting rheostats and switches (Figure 7.8.7)
Page 593 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.4 (2/2) -- CENTRAL INSTRUMENT PANEL (Typical arrangement) Rev. 5 Page 7.3.9 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 594 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) ”FUEL” check and control panel (fuel pressure and quantity indicators, ”FUEL SEL” and ”AUX BP” switches) (Figure 7.7.3) 2) ”GYRO mode” indicator 3) Emergency beacon switch (not valid for UK) 4) Altimeter 2 5) Battery temperature indicator (if installed) (Figure 7.8.4) 6) Adjustable air outlet...
Page 595 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.5 (2/2) -- RIGHT INSTRUMENT PANEL (Typical arrangement) Rev. 3 Page 7.3.11 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 596 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Trim tabs indicators 2) Flaps position indicator 3) Propeller governor lever 4) Power lever 5) Flaps control 6) Condition lever 7) Levers friction adjustment 8) Emergency fuel control 9) Manual fuel tank selector (Figure 7.7.2) 10) Roll trim tab control 11) Pitch trim tab control 12) Lock for access door to landing gear emergency pump (Figure 7.5.2)
Page 597 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.6 (2/2) -- PEDESTAL CONSOLE (Typical arrangement) Rev. 2 Page 7.3.13 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 598 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.7 -- CIRCUIT BREAKERS PANEL -- Without ”pilot” door Page 7.3.14 Rev. 7 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 599 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.7A -- CIRCUIT BREAKERS PANEL -- With ”pilot” door Rev. 7 Page 7.3.15 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 600 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK MASTER General warning WARNING upon illumination of red warning light MASTER General warning CAUTION upon illumination of amber warning light Inter turbine temperature ≥ 800°C OIL PRESS Engine oil low pressure ≤ 4.1 bar (60 psi) STARTER Starter generator running (flashing) IGNITION...
Page 601 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.8 (2/2) -- ADVISORY PANEL AND GENERAL ALARMS WARNING LIGHTS Rev. 6 Page 7.3.17 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 602 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK DOORS, WINDOWS AND EMERGENCY EXIT Cabin access door (Figure 7.3.9) The cabin two--piece access door (crew and passengers), located on the left side of fuselage aft of the wings, opens outside. Stairs are incorporated in the lower door.
Page 603 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.9 -- CABIN ACCESS DOOR Rev. 7 TBM 700A - - Door equipped with one cable Page 7.3.19 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 604 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK DOORS, WINDOWS AND EMERGENCY EXIT Cabin access door (Figure 7.3.9A) The cabin two--piece access door (crew and passengers), located on the left side of fuselage aft of the wings, opens outside. Stairs are incorporated in the lower door.
Page 605 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.9A -- CABIN ACCESS DOOR Rev. 8 TBM 700A - - Door equipped with two cables Page 7.3.19B PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 606 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK DOORS, WINDOWS AND EMERGENCY EXIT Cabin access door (Figure 7.3.9B) The cabin one--piece access door, located on the left side of fuselage aft of the wings, opens outside. The retractable stairs and hand rail make boarding easier.
Page 607 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.9B -- CABIN ACCESS DOOR Rev. 9 TBM 700B Page 7.3.19D PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 608 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK CAUTION BEFORE OPENING ACCESS DOOR, MAKE SURE DOOR DEFLECTION AREA IS CLEAR To open door from inside the cabin, unlock the handle by pressing on knob located on its left side, pull the handle toward inside and move it upwards. Open the door by pushing it upwards.
Page 609 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Cockpit access door (Figure 7.3.9C) The cockpit access door, so--called ”pilot” door, (if installed) located on the left side of fuselage forward of the wings, opens outside. Retractable footstep makes boarding easier. WARNING AS THE ”PILOT”...
Page 610 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.9C -- COCKPIT ACCESS DOOR (”PILOT” DOOR) Page 7.3.19G TBM 700B Rev. 9 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 611 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK CAUTION RETRACT FOOTSTEP BEFORE CLOSING ACCESS DOOR Fold and tilt footstep upwards. 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.
Page 612 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK FWD baggage compartment door The FWD baggage compartment door is located on the airplane left side between the firewall and the front pressure bulkhead. It is hinged at the top. It is maintained in the up position by a compensation rod.
Page 613 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.10 -- EMERGENCY EXIT Rev. 11 Page 7.3.21 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 614 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK SEATS, BELTS AND HARNESSES Cockpit seats (Figure 7.3.11) L.H. and R.H. front seats are mounted on rails attached to the structure. Longitudinal position, height and back--rest tilting of each seat can be adjusted and the arm--rest is hinged.
Page 615 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK SEATS, BELTS AND HARNESSES Cockpit seats (Figure 7.3.11A) L.H. and R.H. front seats are mounted on rails attached to the structure. Longitudinal position, height and back--rest tilting of each seat can be adjusted and the arm--rest is hinged.
Page 616 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK SEATS, BELTS AND HARNESSES Cockpit seats (Figure 7.3.11B) L.H. and R.H. front seats are mounted on rails attached to the structure. Longitudinal position, height and back--rest tilting of each seat can be adjusted and the arm--rest is hinged.
Page 617 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK BAGGAGE COMPARTMENTS There are two baggage compartments : An AFT compartment located in the pressurized cabin between rear passenger seats and rear pressure bulkhead. A FWD compartment (non--pressurized) located between firewall and fwd pressure bulkhead.
Page 618 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Front passenger’s seat 2) L. H. pilot’s seat 3) R. H. intermediate passenger’s seat (back to flight direction) 4) L. H. intermediate passenger’s seat (back to flight direction) 5) R. H. rear passenger’s seat 6) L.
Page 619 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK (*) Oxygen masks (2) drawer in variant of R.H. rear seat Figure 7.3.11 (2/2) -- SEATS Valid S / N 1 to 23, 25, 28, 33 and 35, except airplanes equipped as a retrofit with modification Nr MOD 70--019--25 Rev.
Page 620 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Front passenger’s seat 2) L. H. pilot’s seat 3) R. H. intermediate passenger’s seat (back to flight direction) 4) L. H. intermediate passenger’s seat (back to flight direction) 5) R. H. rear passenger’s seat Rear bench 6) L.
Page 621 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK (*) Variant from S / N 68 except S / N 72, 73, 74 and 75 Figure 7.3.11A (2/2) -- SEATS Valid S / N 24, 26, 27, 29 to 32, 34, 36 to 9999, plus airplanes equipped as a retrofit with modification Nr MOD 70--019--25 Rev.
Page 622 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Front passenger’s seat 2) L. H. pilot’s seat 3) R. H. intermediate passenger’s seat (back to flight direction) 4) L. H. intermediate passenger’s seat (back to flight direction) 5) R. H. rear passenger’s seat Rear bench 6) L.
Page 623 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.11B (2/2) -- SEATS Rev. 7 TBM 700B Page 7.3.29 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 624 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.3.12 -- FRONT OR REAR SEAT BELT (with movable straps) AND HARNESSES Page 7.3.30 Rev. 7 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 625 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.4 - - FLIGHT CONTROLS Flight controls consist of roll, pitch and rudder controls, as well as roll trim tab, pitch trim tab and rudder trim tab controls. NOTE : During airplane parking, it is recommended to lock flight controls (see Figure 8.6.2) ROLL (Figure 7.4.1) The roll control is activated by an assembly of rods and cables which links...
Page 626 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Pedestal assembly 2) Control wheels 3) Fuselage roll lever 4) Spoiler 5) Aileron 6) Aileron control in wing 7) Spoiler control Figure 7.4.1 (1/2) -- ROLL Page 7.4.2 Rev. 11 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 627 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.4.1 (2/2) -- ROLL Rev. 5 Page 7.4.3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 628 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Roll trim tab 2) Aileron 3) Adjustable rods 4) Actuator 5) Trim tab control wiring 6) Aileron trim tab position indicator 7) Trim switch on pedestal console Figure 7.4.2 (1/2) -- LATERAL TRIM Page 7.4.4 Rev.
Page 629 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.4.2 (2/2) -- LATERAL TRIM Rev. 2 Page 7.4.5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 630 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 7.4.6 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 631 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK ELEVATOR (Figure 7.4.3) Both elevators are activated simultaneously by the same control. Each control surface is hinged at three points to the rear part of horizontal stabilizer. The control wheel controls the two elevators through rods, bearings and bellcranks.
Page 632 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Control wheel assembly 2) Elevators 3) Lever assembly, fuselage rear part 4) Elevator bellcrank 5) Rod with presseal connection 6) Lever assembly under floor 7) Pedestal assembly 8) Actuator Figure 7.4.3 (1/2) -- ELEVATOR Page 7.4.8 Rev.
Page 633 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.4.3 (2/2) -- ELEVATOR Rev. 5 Page 7.4.9 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 634 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Cables 2) Pulleys 3) Pitch trim tabs 4) Actuating rods 5) Actuator 6) Pitch trim tab position indicator 7) Pitch trim manual control wheel 8) Pitch trim electrical control Figure 7.4.4 (1/2) -- PITCH TRIM Rev.
Page 635 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.4.4 (2/2) -- PITCH TRIM Rev. 5 Page 7.4.11 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 636 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 7.4.12 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 637 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK RUDDER (Figure 7.4.5) The rudder is hinged on three fittings attached to the vertical stabilizer rear spar. The rudder pedals / rudder linkage is ensured through cables and a rod. Pilot and R.H. station rudder pedal positions are adjustable at each station. The rudder pedal adjustment mechanism (for piloting comfort purposes) includes a manual control located against the external bulkhead beneath the instrument panel and a locking device on the rudder pedals.
Page 638 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Roll / rudder combination bellcrank installation 2) Rudder pedals assembly 3) Control cables 4) Pulleys 5) Rudder lever assembly 6) Rod 7) Rudder 8) Nose gear steering rod Figure 7.4.5 (1/2) -- RUDDER Page 7.4.14 Rev.
Page 639 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.4.5 (2/2) -- RUDDER Rev. 2 Page 7.4.15 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 640 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Trim switch on control wheel 2) Actuator 3) Rudder trim tab 4) Rods 5) Rudder trim control wiring 6) Rudder trim tab position indicator Figure 7.4.6 (1/2) -- RUDDER TRIM Page 7.4.16 Rev.
Page 641 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.4.6 (2/2) -- RUDDER TRIM Rev. 5 Page 7.4.17 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 642 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 7.4.18 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 643 SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.5 - - LANDING GEAR The TBM 700 is equipped with electro--hydraulically actuated, fully retractable tricycle landing gear. Each landing gear is equipped with one wheel and an oil--air shock absorber integrated in the strut.
Page 644 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK HYDRAULIC PRESSURE Hydraulic pressure required for landing gear operation is accomplished : -- during normal operation, by an electro--hydraulic generator with integrated reservoir, -- during emergency extension operation by a hand pump supplied with an auxiliary reservoir.
Page 645 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Red warning light (LDG GR) 2) Green indicator light (LDG GR) 3) Landing gear control selector 4) Test switch 5) Test knobs Figure 7.5.1 -- CONTROL PANEL AND LANDING GEAR INDICATING Rev.
Page 646 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK SAFETY Safety switch (landing gear retraction) : A safety switch installed on each main landing gear prevents, by detecting shock strut compression, landing gear accidental retraction when airplane is on ground. Landing gear horn : Landing gear horn is controlled by power lever and / or flaps.
Page 647 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.5.2 -- EMERGENCY LANDING GEAR EXTENSION CONTROL Rev. 13 Page 7.5.5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 648 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK GROUND MANEUVERS Nose gear steering control (Figures 7.5.3 and 7.5.4) Nose gear steering control is combined with rudder pedals and is fitted with a shimmy damper. When one of rudder pedals is fully pushed, nose wheel swivels about 20°.
Page 649 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.5.3 -- MINIMUM TURN DIAMETER (Full rudder pedals travel without using differential braking) Rev. 14 Page 7.5.7 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 650 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.5.4 -- MINIMUM TURN DIAMETER (Full rudder pedals travel by using differential braking) Page 7.5.8 Rev. 11 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 651 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK BRAKE SYSTEM (Figure 7.5.5) Airplane is equipped with a hydraulically actuated disc braking system installed on the main landing gear wheels. Each toe brake at L.H. and R.H. stations is equipped with a master cylinder which sends hydraulic pressure to the corresponding disc brake : L.H.
Page 652 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Reservoir 2) Vent 3) R.H. station master cylinders 4) Parking brake control knob 5) Parking brake valve 6) Drain 7) Pilot’s station master cylinders 8) L.H. brake assembly 9) R.H. brake assembly Figure 7.5.5 (1/2) -- BRAKE SYSTEM Page 7.5.10 Rev.
Page 653 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.5.5 (2/2) -- BRAKE SYSTEM Rev. 6 Page 7.5.11 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 654 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.5.6 -- PARKING BRAKE Page 7.5.12 Rev. 6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 655 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.6 - - POWERPLANT TURBOPROP ENGINE OPERATION (Figure 7.6.1) The PRATT & WHITNEY CANADA turboprop engine (PT6A--64 type) is a free turbine engine developing thermodynamic power of 1580 SHP, derated to 700 SHP. Intake air enters engine through an annular casing and is then ducted toward compressor.
Page 656 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Propeller governor 2) Exhaust stub 3) Axial compressors 4) Accessory gearbox 5) FCU Fuel control unit 6) Oil to fuel heater 7) Compressor stubshaft 8) Air intake 9) Centrifugal impeller 10) Combustion chamber 11) Compressor turbine 12) Power turbine 1st stage...
Page 657 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.6.1 (2/2) -- POWER PLANT Rev. 2 Page 7.6.3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 658 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK ENGINE CONTROLS (LEVERS) (Figure 7.6.2) Engine operation requires use of four levers located on pedestal console in cabin : -- power lever (Item 2), and its detent for reverse (Item 6) -- propeller governor lever (Item 1), -- condition lever (Item 3), -- ”MAN OVRD”...
Page 659 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Power control lever The power control lever is linked to fuel control unit. It modulates engine power from full reverse to takeoff. Engine running, the power control lever rearward displacement, past the lock using the detent, allows to control : -- the engine power in the Beta range from idle to maximum reverse, -- the Beta valve to select the propeller pitch in reverse.
Page 660 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Post--MOD70--0256--76 The fuel condition lever has a ”HI / IDLE” locked position. Change from idle ”HI / IDLE” to ”LO / IDLE” position is only possible after having overridden the idle gate. To override idle gate, raise lever and move it rearwards.
Page 661 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Engine fire detection test knob (if installed) 2) Torque indicator 3) ”PROP O’SPEED TEST” knob 4) Propeller indicator 5) ITT indicator 6) ITT test knob 7) Ng indicator 8) Oil pressure and temperature indicator 9) Fuel flow indicator Figure 7.6.3 -- ENGINE INSTRUMENTS...
Page 662 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Fuel flow totalizer (FLOW) is a digital display instrument which indicates : -- quantity of fuel consumed since beginning of flight, -- instantaneous consumption, -- remaining flight time depending on fuel quantity. NOTE : Each instrument is provided with marks indicating utilization limits.
Page 663 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK ENGINE LUBRICATION Engine oil is in a tank incorporated into the power plant. It ensures lubrication and engine cooling. A cooler located on left side in engine compartment maintains oil temperature within limits. Oil flow into the cooler is metered by a thermostatic valve.
Page 664 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Starter function Starting system consists of ”STARTER” switch located on ”ENGINE START” panel, starter generator, ”STARTER” warning light in advisory panel and ignition circuit (Refer to Paragraph ”Ignition function”). Starting procedure is manual. Setting ”STARTER” switch to ”ON” connects the starter generator which drives power plant .
Page 665 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.6.4 -- ENGINE STARTING Rev. 5 Page 7.6.11 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 666 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK EXHAUST SYSTEM Exhaust gases are evacuated through exhaust stubs located on sides of engine cowlings. ENGINE ACCESSORIES All engine driven accessories [except power turbine tacho--generator (Np) and propeller governor] are installed on accessory gearbox located rearwards of engine.
Page 667 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Torque transmitter Torque transmitter is attached on the torque limiter, it measures torque produced by the power turbine by comparing oil pressures (reduction gear and power turbine) and converts pressure difference into a voltage which is applied to torquemeter.
Page 668 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK PROPELLER Airplane is equipped with an all--metal, four--bladed, constant--speed and full--feathering propeller. Regulation Propeller governor located on engine maintains rotation speed selected by pilot with propeller governor lever. Regulation is obtained through propeller blade pitch variation : counterweights drive propeller blades toward high pitch (low RPM) whereas oil pressure delivered by governor drives back blades toward low pitch (high RPM).
Page 669 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.7 - - FUEL SYSTEM (Figure 7.7.1) The fuel system comprises fuel tanks, fuel unit, selectors (manual and automatic), electric and mechanical boost pumps, engine fuel system, gaging installation, monitoring installation and drains. FUEL TANKS Fuel tanks are formed by sealed casings in each wing.
Page 670 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Flow divider 2) Flowmeter 3) Collector tank 4) Fuel regulator 5) High pressure pump (HP) 6) Oil to fuel heater 7) Low pressure switch 8) Pressure transmitter 9) Fuel jet 10) Main mechanical boost pump 11) Electric boost pump 12) Fuel filter...
Page 671 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.7.1 (2/2) -- FUEL SYSTEM Rev. 5 Page 7.7.3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 672 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK AUTOMATIC TANK SELECTOR (Figures 7.7.2 and 7.7.3) Automatic tank selection allows, without pilot’s intervention, feeding the engine from one tank to the other in predetermined sequences. These sequences depend on airplane configuration (ground, in--flight, fuel low level warning lights illuminated).
Page 673 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK NOTE : The manual selector is driven by the fuel unit and is positioned on ”R ” or ”L” mark corresponding to the tank selected by the sequencer. Therefore, the pilot continuously knows the tank which is operating. Test for system proper operation ”SHIFT”...
Page 674 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.7.2 -- MANUAL SELECTOR OF FUEL TANKS Page 7.7.6 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 675 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.7.3 -- FUEL CONTROL PANEL Valid from S / N 1 to 5 Rev. 2 Page 7.7.7 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 676 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 7.7.8 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 677 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.7.3A -- FUEL CONTROL PANEL Valid from S / N 6 Rev. 2 Page 7.7.9 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 678 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK MAIN MECHANICAL BOOST PUMP The mechanical boost pump is attached to accessory gearbox and supplies fuel necessary for engine operation. ENGINE FUEL SYSTEM The engine fuel system consists of a fuel regulator, pumps, filters, a fuel divider and fuel nozzles.
Page 679 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK FUEL MONITORING INSTALLATION (Figure 7.7.3) Monitoring installation comprises pressure indicator and warning lights grouped on advisory panel. Pressure indicator is attached on ”FUEL” panel ; it indicates fuel pressure at main booster pump outlet. Indications provided by illumination of warning lights on advisory panel : -- ”FUEL OFF”...
Page 680 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK FUEL SYSTEM DRAINING AND CLOGGING INDICATOR (Figure 7.7.4) The fuel system comprises five drain points, a drain on the filter bowl, two drain valves on each tank, located on wing lower surface, on wing root side. These drains allow draining water or sediments contained in fuel.
Page 681 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.7.4 (2/2) -- FUEL SYSTEM DRAINING POINTS AND CLOGGING INDICATOR Rev. 13 Valid from S/N 1 to 92 Page 7.7.13 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 682 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 7.7.14 Rev. 5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 683 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK FUEL SYSTEM DRAINING AND CLOGGING INDICATOR (Figure 7.7.4A) The fuel system comprises five drain points, a drain on the filter bowl, two drain valves on each tank, located on wing lower surface, one at wing root and the other past main landing gear well.
Page 684 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Lighting switch 2) Mirror door 3) Clogging indicator 4) Central access door 5) Filter drain 6) Tank drain 7) Drain bowl Figure 7.7.4A (1/2) -- FUEL SYSTEM DRAINING POINTS AND CLOGGING INDICATOR Page 7.7.16 Valid from S/N 93 to 9999...
Page 685 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.7.4A (2/2) -- FUEL SYSTEM DRAINING POINTS AND CLOGGING INDICATOR Rev. 11 Valid from S/N 93 to 9999 Page 7.7.17 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 686 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 7.7.18 Rev. 5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 687 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.8 - - ELECTRICAL SYSTEM (Figures 7.8.1 and 7.8.5) The airplane is fitted with a direct--current electrical system rated to 28 volts with negative pole at ground. Airplane mains supply is obtained from various power supplies : -- an engine driven starter generator -- a stand--by generator driven by the engine through a belt -- a battery located in engine compartment...
Page 688 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK STAND- -BY GENERATOR Stand--by generator supplies a 28--volt stand--by direct current which may be used in case of main generator failure. Generator connection with main bus bar is controlled through ”GENERATOR” selector set to ”ST--BY”, it will be effective when connection conditions are met.
Page 689 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK DISTRIBUTION Airplane electrical systems are connected to ”BUS” bars and protected by circuit breakers located on L.H. side panel, near the pilot (See Figures 7.8.3, 7.8.3A and 7.8.3B) or on R.H. side panel, if ”pilot” door installed (See Figure 7.8.3C).
Page 690 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.8.1 -- ELECTRICAL DIAGRAM Rev. 13 Page 7.8.4 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 691 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK FLAPS (D) STROBE PITOT 1 HTR R.W / S DE ICE INERT SEP AIRFRAME DE ICE ENGINE INDIC 1 : -- torquemeter, propeller & oil press+temperature IGNIT AUX BP PHONE or FUEL SEL PHONE+MKR CABIN TEMP...
Page 692 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK AP / TRIMS AP & trims general protec. ADVISORY 1 Visual warn. protec. RUD TRIM Rudder trim protec. ADVISORY 2 Visual warn. protec. AIL TRIM Aileron trim protec. AUDIO Audio warnings protec. PITCH TRIM Pitch trim protec.
Page 693 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK (*) ”Pull--off” type circuit breaker in variant Figure 7.8.3 (2/2) -- CIRCUIT BREAKER PANEL (Typical arrangement) Rev. 13 TBM 700A from S/N 1 to 10 Page 7.8.7 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 694 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK AP / TRIMS AP & trims general protec. ADVISORY 1 Visual warn. protec. RUD TRIM Rudder trim protec. ADVISORY 2 Visual warn. protec. AIL TRIM Aileron trim protec. AUDIO Audio warnings protec. PITCH TRIM Pitch trim protec.
Page 695 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK (*) Circuit breaker which cannot be pulled off up to S / N 17 NOTE 1 : If ADF 2 is installed, its circuit breaker is installed on a free location, HSI RMI becomes HSI and ADF becomes ADF 1 RMI.
Page 696 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK AP / TRIMS AP & trims general protec. FUEL GAGE 1 L.H gage protec. RUD TRIM Rudder trim protec. FUEL GAGE 2 R.H gage protec. AIL TRIM Aileron trim protec. FUEL SEL Timer protec.
Page 697 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK NOTE 1 : If an additional equipment is installed, its circuit breaker is installed on a free location. Figure 7.8.3B (2/2) -- CIRCUIT BREAKER PANEL (Typical arrangement) Rev. 8 TBM 700B without ”pilot” door Page 7.8.9B PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 698 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK AP / TRIMS AP & trims general protec. L LDG L.H. landing light protec. RUD TRIM Rudder trim protec. TAXI Taxi light protec. AIL TRIM Aileron trim protec. R LDG R.H. landing light protec. PITCH TRIM Pitch trim protec.
Page 699 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK NOTE 1 : If an additional equipment is installed, its circuit breaker is installed on a free location. Figure 7.8.3C (2/2) -- CIRCUIT BREAKER PANEL (Typical arrangement) Rev. 9 TBM 700B with ”pilot” door Page 7.8.9D PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 700 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INDICATING (Figure 7.8.4) Electrical system indicating consists of a voltmeter and an ammeter located on the upper panel, as well as warning lights grouped on advisory panel. The voltmeter indicates the voltage with generator connected to main bus bar.
Page 701 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK PROTECTION - - SAFETY (Figure 7.8.5) The electrical power center provides systems protection in case of : -- overvoltage coming from the starter generator, the stand--by generator or the ground power receptacle -- short--circuit in starter generator feeder -- starter generator undervoltage In case of disconnection of starter generator or stand--by generator following...
Page 702 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Ammeter 2) Voltmeter 3) General flashing red and amber warning lights 4) Electric system warning lights on the ”ADVISORY PANEL” 5) Battery temperature indicator (if installed) 6) ”BAT TEMP TEST” push--button (if installed) Figure 7.8.4 (1/2) -- INDICATING Page 7.8.12 Rev.
Page 703 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.8.4 (2/2) -- INDICATING Rev. 6 Page 7.8.13 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 704 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) ”MAIN” reset knob 2) ”ST--BY” reset knob 3) Crash lever 4) ”SOURCE” selector 5) ”GENERATOR” selector Figure 7.8.5 (1/2) -- ELECTRICAL CONTROL Page 7.8.14 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 705 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.8.5 (2/2) -- ELECTRICAL CONTROL Rev. 2 Page 7.8.15 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 706 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK EXTERIOR LIGHTING (Figure 7.8.6) The airplane is equipped with two navigation lights, two strobe lights, two landing lights, a taxi light, a wing leading edge icing inspection light. A ”LTS TEST” test--knob located above lights switches allows checking proper operation of warning lights ;...
Page 707 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Leading edge icing inspection light The leading edge icing inspection light is installed on fuselage L.H. side, its beam illuminates the wing leading edge. It is controlled by the ”ICE LIGHT” switch installed on ”DE--ICE SYSTEM”...
Page 708 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) L.H. landing light switch 2) Test knob (test light integrated to switches) 3) Taxi light switch 4) R.H. landing light switch 5) Navigation lights switch 6) Strobe lights switch 7) (Free) Figure 7.8.6 (1/2) -- EXTERNAL LIGHTING CONTROLS Page 7.8.18 Rev.
Page 709 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.8.6 (2/2) -- EXTERNAL LIGHTING CONTROLS Rev. 2 Page 7.8.19 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 710 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTERIOR LIGHTING (Figure 7.8.7) Interior lighting consists of access, cabin, instrument panel, instruments, baggage compartments and emergency lighting. Access lighting Access lighting consists of FWD dome light, rear baggage compartment, R.H. rear light and access door. ”ACCESS” switch on ”INT LIGHTS” panel and the switch located near access door are two--way switches type and control these 3 lights.
Page 711 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Emergency lighting Emergency lighting consists of two floodlights located on the upper duct above front seats. It illuminates instrument panel assembly in case of visor lighting and / or instrument integrated lighting failure. The rheostat located near R.H.
Page 712 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTERIOR LIGHTING (Figure 7.8.7) Interior lighting consists of access, cabin, instrument panel, instruments, baggage compartments and emergency lighting. Access lighting Access lighting consists of two floodlights located on the ceiling upholstering (one at the level of the access door, the other at the level of the storage cabinet) and the L.H.
Page 713 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Emergency lighting Emergency lighting consists of two swiveling floodlights located on the upper duct above front seats. It illuminates instrument panel assembly in case of visor lighting and / or instrument integrated lighting failure. The rheostat located near R.H.
Page 714 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Instrument lighting switch (rheostat) 2) Instrument panel lighting switch (rheostat) 3) Cabin lighting switch (rear seats reading light) 4) Access door, rear baggage compartment and FWD dome light (two--way switch with access door switch) lighting controls 5) Emergency lighting switch (rheostat) Figure 7.8.7 (1/2) -- INTERNAL LIGHTING CONTROLS Page 7.8.22...
Page 715 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.8.7 (2/2) -- INTERNAL LIGHTING CONTROLS Rev. 13 Page 7.8.23 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 716 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 7.8.24 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 717 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.9 - - AIR CONDITIONING AND PRESSURIZATION AIR CONDITIONING (Figure 7.9.1) Air conditioning system includes a flow--pressure regulation system, temperature regulation and cooling system, control and check systems and distribution. Air necessary for conditioning is picked up from the engine. A two--setting level valve regulates pressure and bleed hot air flow and may be also used as shutoff valve.
Page 718 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Overheat switch 2) Cooling turbine 3) Hot air -- cold air mixer 4) Water separator 5) Temperature control valve 6) Pressure regulator of temperature control valve 7) Check--valve 8) Temperature control sensor 9) Cabin emergency air inlet 10) Defogging outlets 11) Adjustable air outlets...
Page 719 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.9.1 (2/2) -- AIR CONDITIONING Rev. 5 Page 7.9.3 Valid S/N 1 to 23, 25, 28, 33 and 35 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 720 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Control and check (Figure 7.9.3) Air conditioning system controls are located on ”ECS” panel, warning lights are grouped on advisory panel. Conditioning occurs when ”BLEED VALVE” switch is set to ”ON” ; this leads to opening of pressure regulation valve and switches off ”BLEED OFF”...
Page 721 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.9 - - AIR CONDITIONING AND PRESSURIZATION AIR CONDITIONING (Figure 7.9.1A) Air conditioning system includes a flow--pressure regulation system, temperature regulation and cooling system, control and check systems and distribution. Air necessary for conditioning is picked up from the engine. A two--setting level valve regulates pressure and bleed hot air flow and may be also used as shutoff valve.
Page 722 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Overheat switch 2) Cooling turbine 3) Hot air -- cold air mixer 4) Water separator 5) Temperature control valve 6) Pressure regulator of temperature control valve 7) Check--valve 8) Temperature control sensor 9) Cabin emergency air inlet 10) Defogging outlets 11) Adjustable air outlets...
Page 723 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.9.1A (2/2) -- AIR CONDITIONING Valid S/N 24, 26, 27, 29 to 32, Rev. 5 Page 7.9.4C 34, 36 to 85, 87, 90 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 724 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Control and check (Figure 7.9.3) Air conditioning system controls are located on ”ECS” panel, warning lights are grouped on advisory panel. Conditioning occurs when ”BLEED VALVE” switch is set to ”ON” ; this leads to opening of pressure regulation valve and switches off ”BLEED OFF”...
Page 725 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.9 - - AIR CONDITIONING AND PRESSURIZATION AIR CONDITIONING (Figure 7.9.1B) Air conditioning system includes a flow--pressure regulation system, temperature regulation and cooling system, control and check systems and distribution. Air necessary for conditioning is picked up from the engine. A two--setting level valve regulates pressure and bleed hot air flow and may be also used as shutoff valve.
Page 726 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Overheat switch 2) Cooling turbine 3) Hot air -- cold air mixer 4) Water separator 5) Temperature control valve 6) Pressure regulator of temperature control valve 7) Check--valve 8) Temperature control sensor 9) Cabin emergency air inlet 10) Defogging outlets 11) Adjustable air outlets...
Page 727 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.9.1B (2/2) -- AIR CONDITIONING Rev. 5 Valid S/N 86, 88, 89, 91 to 9999 Page 7.9.4G PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 728 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Control and check (Figure 7.9.3) Air conditioning system controls are located on ”ECS” panel, warning lights are grouped on advisory panel. Conditioning occurs when ”BLEED VALVE” switch is set to ”ON” ; this leads to opening of pressure regulation valve and switches off ”BLEED OFF”...
Page 729 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK PRESSURIZATION (Figures 7.9.2 and 7.9.3) Pressurization system maintains the pressure corresponding to an altitude compatible with passengers’ safety and comfort inside the cabin. The system uses the air conditioning system to pressurize the cabin and the vacuum generation system for check and safety.
Page 730 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Check valve 2) Cabin--atmosphere ∆P microswitch 3) Advisory panel 4) Outflow valve 5) Safety valve 6) Depressurization valve 7) Landing gear switch (airplane on ground) 8) Pressure controller 9) Cabin altitude warn switch 10) Compensation tank Figure 7.9.2 (1/2) -- PRESSURIZATION Page 7.9.6...
Page 731 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.9.2 (2/2) -- PRESSURIZATION Rev. 9 Page 7.9.7 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 732 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) ”BLEED VALVE” switch -- ON/OFF 2) ”BLEED VALVE” switch -- HI/LO 3) ”CABIN FAN” switch 4) ”DUMP” switch 5) ”CABIN TEMP” selector 6) ”DEFOG / NORMAL” distributor 7) Cabin rate selector 8) Cabin altitude selector 9) Three--position indicator (cabin altitude, cabin climb speed and differential pressure)
Page 733 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.9.3 (2/2) -- ”ECS” CONTROL AND CHECK PANEL Rev. 13 Page 7.9.9 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 734 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 7.9.10 Rev. 5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 735 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.10 - - EMERGENCY OXYGEN SYSTEM (Figure 7.10.1) Emergency oxygen system must be used following a pressurization system failure at an altitude between 12000 and 30000 ft. The three emergency oxygen systems provide enough chemical oxygen for six persons during a descent from 30000 to 12000 ft and below.
Page 736 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Generator 2) Supply tubes 3) Masks 4) Drawer 5) Microswitch 6) Dimpled support 7) Microphone switch Figure 7.10.1 (1/2) -- EMERGENCY OXYGEN SYSTEM Page 7.10.2 Rev. 11 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 737 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK (*) Variant Figure 7.10.1 (2/2) -- EMERGENCY OXYGEN SYSTEM Valid S/N 1 to 23, 25, 28, 33 and 35, except airplanes equipped as a retrofit with Rev. 5 Page 7.10.3 modification Nr MOD 70- -019- -25 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 738 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INDICATING When the ”SOURCE” selector is set to ”BAT” or ”GPU”, as soon as an oxygen generator is activated, the ”OXYGEN” warning light located on the advisory panel illuminates. The warning light remains illuminated as long as used generator is not replaced.
Page 739 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.10.1A (2/2) -- EMERGENCY OXYGEN SYSTEM Valid S/N 24, 26, 27, 29 to 32, 34, 36 to 9999, plus airplanes equipped as a retrofit with Rev. 5 Page 7.10.5 modification Nr MOD 70- -019- -25 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 740 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 7.10.6 Rev. 5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 741 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.11 - - AIR DATA SYSTEM AND INSTRUMENTS (Figure 7.11.1) Airplane air data system consists of : -- two separate static pressure systems supplying the altimeters, airspeed and vertical speed indicators. They also provide a static pressure reference to the ∆P cabin and to the Autopilot system Air Data Computer (ADC).
Page 742 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Pitot Nr 1 2) Pitot Nr 2 3) Pitot Nr 2 dynamic drain 4) Pitot Nr 1 dynamic drain 5) V detector 6) Static drain 7) Emergency static drain 8) Static drain 9) FWD pressure bulkhead 10) Airspeed indicator Nr 1 11) Encoding altimeter Nr 1...
Page 743 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.11.1 (2/2) -- AIR DATA SYSTEM Rev. 5 Page 7.11.3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 744 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Alternate static source The alternate static port located in the rear fuselage supplies a system routed to the switching valve (normal / alternate) in order to replace static system 1 and also supplies the V warning.
Page 745 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.12 - - VACUUM SYSTEM AND INSTRUMENTS (Figure 7.12.1) The airplane is fitted with a vacuum system providing the suction necessary to operate the stand--by attitude indicator, the cabin pressurization and the leading edge deicing.
Page 746 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) Pressure regulator 2) Ejector 3) Valve 4) Regulating and relief valve 5) Pressure switch 6) Failure warning light (Figure 7.3.8) Figure 7.12.1 (1/2) -- VACUUM SYSTEM Page 7.12.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 747 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.12.1 (2/2) -- VACUUM SYSTEM Rev. 2 Page 7.12.3 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 748 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.12.2 (1/2) -- GYROSCOPIC INSTRUMENTS CONTROL (Variants according to the type of installation) Page 7.12.4 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 749 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK GYROSCOPIC INSTRUMENTS CONTROL (Figure 7.12.2) Gyroscopic instruments : electrical attitude gyros, HSI, RMI, ADI, etc... are controlled by switches located on instrument panel upper strip. SUCTION GAGE The suction gage is calibrated in inches of mercury and indicates the suction available for operation of the attitude indicator.
Page 750 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.12.2 (2/2) -- GYROSCOPIC INSTRUMENTS CONTROL (Variants according to the type of installation) Page 7.12.6 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 751 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.13 - - ICE PROTECTION EQUIPMENT (Figure 7.13.1) Ice protection equipment is as follows : -- Pneumatic deice system for inboard, central and outboard wing and for stabilizers : ”AIRFRAME DE--ICE” -- Propeller electrical deice system : ”PROP DE--ICE”...
Page 752 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK PROPELLER DEICING Propeller deicing is accomplished through electrical heating of blade roots. This system operates cyclically and alternately on two opposite blades at the same time. Each cycle is 180 seconds long. The system operation is correct when green warning light located above ”PROP DE ICE”...
Page 753 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK HEATING OF PITOTS AND STALL WARNING SENSOR (”PITOT 1 HTR” AND ”PITOT 2 & STALL HTR”) The two pitots, which supply airspeed indicators and the stall warning sensor are electrically heated. This deice equipment must be used even during flight into non--icing conditions ;...
Page 754 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Figure 7.13.1 -- DEICING CONTROL AND CHECK PANEL Page 7.13.4 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 755 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.14 - - RADIO MASTER AND GROUND COMMUNICATION (Figure 7.14.1) The electrical supply of radio communication and radio navigation equipment assembly is controlled by the ”RADIO MASTER” switch located on the ”INT LIGHTS”...
Page 756 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 1) ”RADIO MASTER” switch 2) ”GND CLR” (ground clearance) ground communication indicator Figure 7.14.1 -- RADIO MASTER AND GROUND COMMUNICATION Rev. 13 Page 7.14.2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 757 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK 7.15 - - MISCELLANEOUS EQUIPMENT STALL WARNING SYSTEM The airplane is equipped with an electrically deiced stall sensor in the leading edge of the right wing. This sensor fitted with a vane is electrically connected to an audible warning.
Page 758 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK CABIN FIRE EXTINGUISHER (if installed) The fire extinguisher is located on the pilot’s seat L.H. side. It is attached on the floor by means of a quick--disconnect support. A pressure gage allows checking the fire extinguisher condition.
Page 759 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK ELT 90, 91, 96, 97, JE2, JE2NG Operation of the emergency locator transmitter is obtained as follows : -- from the instrument panel by setting ”ELT” remote control switch to ON or position (locator transmitter...
Page 760 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK Reset after an inadvertent activation ELT 90 (EUROCAE) -- ELT 91 (TSO) 1) Set ELT switch to ”MAN/RESET” a) The keeps transmitting emergency or remote control switch to ”MAN”. signal. b) On remote control, the ”XMIT ALERT”...
Page 761 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK ELT KANNAD 406 AF On ”ON/ARMED/RESET--TEST” remote control switch, press on “RESET--TEST” or set locator transmitter switch to “OFF”, then to “ARM”. Rev. 13 Page 7.15.5 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 762 T B M SECTION 7 DESCRIPTION PILOT’S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Rev. 13 Page 7.15.6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 763 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE SECTION 8 HANDLING, SERVICING AND MAINTENANCE TABLE OF CONTENTS Page GENERAL 8.1.1 ........... . IDENTIFICATION PLATE 8.2.1 .
Page 764 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE TABLE OF CONTENTS (Continued) Page AIRPLANE CLEANING AND CARE 8.8.1 ......8.8.1 WINDSHIELD AND WINDOWS .
Page 765 8.1 - - GENERAL This section contains the procedures recommended by the manufacturer for the proper ground handling and routine care and servicing of TBM 700 airplane. Also included in this section are the inspection and maintenance requirements which must be followed if your airplane is to retain its performance and dependability.
Page 766 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE INTENTIONALLY LEFT BLANK Page 8.1.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 767 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE 8.2 - - IDENTIFICATION PLATE Any correspondence regarding your airplane should include its serial number. This number together with the model number, type certificate number and production certificate number are stamped on the identification plate attached to the left side of the fuselage beneath the horizontal stabilizer.
Page 768 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE INTENTIONALLY LEFT BLANK Page 8.2.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 769 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE 8.3 - - PUBLICATIONS When the airplane is delivered from the factory, it is supplied with a Pilot’s Operating Handbook and supplemental data covering optional equipment installed in the airplane (refer to Section 9 “Supplements” and to pilot’s guides).
Page 770 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE INTENTIONALLY LEFT BLANK Page 8.3.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 771 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE 8.4 - - INSPECTION PERIODS Refer to regulations in force in the certification country for information concerning preventive maintenance to be carried out. A maintenance Manual must be obtained prior to performing any preventive maintenance to make sure that proper procedures are followed.
Page 772 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE INTENTIONALLY LEFT BLANK Page 8.4.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 773 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE 8.5 - - ALTERATIONS OR REPAIRS It is essential that the Airworthiness authorities be contacted prior to any alterations or repairs on the airplane to make sure that airworthiness of the airplane is not violated.
Page 774 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE INTENTIONALLY LEFT BLANK Page 8.5.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 775 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE 8.6 - - GROUND HANDLING CAUTION ONLY MOVE OR TOW THE AIRPLANE WITH SOMEONE IN THE COCKPIT TOWING CAUTION USING THE PROPELLER FOR GROUND HANDLING COULD RESULT IN SERIOUS DAMAGE, ESPECIALLY IF PRESSURE OR PULL IS EXERTED ON BLADE TIPS The airplane should be moved on the ground with a towing bar and a suitable vehicle in order not to damage the nose gear steering mechanism.
Page 776 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE Figure 8.6.1 -- TURNING ANGLE LIMITS Page 8.6.2 Rev. 2 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 777 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE NOTE : Do not use solar screens or shields installed on the aircraft inside, or leave sun visors down against windshield when aircraft on ground. The reflected heat from these items causes a temperature increase which accelerates the crack growth or crazing and may cause the formation of bubbles in the inner layer of multilayer windshields.
Page 778 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE Figure 8.6.2 -- CONTROL LOCK DEVICE Page 8.6.4 Rev. 11 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 779 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE FLYABLE STORAGE Airplanes placed in storage for a maximum of 28 days are considered in flyable storage. Storage from 0 to 7 days : -- Engine : according to Maintenance Manual P & W -- C Airplane fueling : -- Keep fuel tanks full to minimize condensation in the tanks.
Page 780 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE INTENTIONALLY LEFT BLANK Page 8.6.6 Rev. 9 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 781 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE 8.7 - - SERVICING MAINTENANCE In addition to the preflight inspection (refer to Section 4, ”Normal Procedures”), servicing, inspection and test requirements for the airplane are detailed in the Maintenance Manual. Maintenance Manual outlines all items which require servicing, inspection or testing or overhaul.
Page 782 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE Oil level check : To avoid overfilling of oil tank, and high oil consumption, an oil level check is recommended within 30 minutes after engine shutdown. Ideal interval is 15 to 20 minutes.
Page 783 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE CAUTION DURING FUELING OPERATIONS, TAKE CARE NOT TO DAMAGE PNEUMATIC DEICER BOOTS LOCATED ON WING LEADING EDGE. THE USE OF AVIATION GASOLINE (AVGAS) MUST BE RESTRICTED TO EMERGENCIES ONLY. AVGAS WILL NOT BE USED FOR MORE THAN 150 CUMULATIVE HOURS DURING ANY PERIOD BETWEEN ENGINE OVERHAUL WARNING...
Page 784 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE Fuel additives Fuel used must contain an anti--ice additive conforming to MIL--I--27686 or MIL--I--85470 specification. Strict adherence to recommended preflight draining instructions as called for in Section 4 will eliminate any free water accumulations from the tank sumps. While small amounts of water may still remain emulsified in the gasoline, it will normally be consumed and go unnoticed in the operation of the engine.
Page 785 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE CAUTION DO NOT PERMIT THE CONCENTRATE OF EGME OR DIEGME TO COME IN CONTACT WITH THE AIRPLANE FINISH OR FUEL TANK MIXING OF THE EGME OR DIEGME WITH THE FUEL IS EXTREMELY IMPORTANT.
Page 786 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE Figure 8.7.3 -- ADDITIVE MIXING RATIO (EGME or DIEGME) Page 8.7.6 Rev. 8 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
Page 787 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE LANDING GEAR Nose gear tire : 5.00--5 6 PR -- Inflating pressure : 98 psi (6.7 bars) * Main gear tires : 18 5.5 8 PR -- Inflating pressure : 125 psi (8.6 bars) * Nose gear shock absorber : Fill with hydraulic fluid AIR 3520 B (MIL.H5606E) ;...
Page 788 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE OXYGEN Indicating When the ”SOURCE” selector is set to ”BAT” or ”GPU”, as soon as an oxygen generator is activated, the ”OXYGEN” warning light located on the advisory panel illuminates.
Page 789 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE 8.8 - - AIRPLANE CLEANING AND CARE WINDSHIELD AND WINDOWS The windshield and windows should be cleaned with an airplane windshield cleaner. NOTE : Refer to the Maintenance Manual for products and procedures to apply. Apply the cleaner sparingly with soft cloths and rub with moderate pressure until all dirt, oil scum and bug stains are removed.
Page 790 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE PAINTED SURFACES Refer to Maintenance Manual for the products and procedures to apply. PROPELLER CARE Preflight inspection of propeller blades for nicks and cleaning them occasionally with a cloth soaked with soapy water to clean off grass and bug stains will assure long blade life.
Page 791 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE 8.9 - - UTILIZATION BY COLD WEATHER (- - 0°C TO - - 25°C) OR VERY COLD WEATHER (- - 25°C TO - - 40°C) If a landing is foreseen by cold or very cold weather or in case of airplane prolonged operation in such conditions, it is recommended to prepare the airplane as follows : 1 -- Smear with silicone grease the seals of the door and engine...
Page 792 T B M SECTION 8 HANDLING, SERVICING PILOT’S OPERATING HANDBOOK AND MAINTENANCE INTENTIONALLY LEFT BLANK Page 8.9.2 Rev. 6 PIM - DO NOT USE FOR FLIGHT OPERATIONS...
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Page 875 T B M SUPPLEMENT 6 ”BFG” STORMSCOPE SUPPLEMENT ”BFG” WX- -500 OR WX- -950 OR WX- -1000 OR 1000+ OR 1000E STORMSCOPE TABLE OF CONTENTS Page -- GENERAL ........9.6.2 -- LIMITATIONS .
Page 876 T B M SUPPLEMENT 6 ”BFG” STORMSCOPE SECTION 1 GENERAL This supplement supplies information to the pilot about limitations, normal and emergency procedures when the optional ”BFG” WX--500 or WX--950 or WX--1000 or 1000+ or 1000E stormscope is installed on the TBM airplane. The stormscope must be used within limits of this supplement.
Page 877 T B M SUPPLEMENT 6 ”BFG” STORMSCOPE -- The Stormscope ”BFG” Pilot’s Handbook, Series II, No. 75--0299--7690--1 (WX--1000 or 1000+ or 1000E), -- The WX--950 Pilot’s guide, Series II, No. 009--10951--001, -- The WX--500 Pilot’s guide, Series II, No. 009--11501--001 and the ”GARMIN”...
Page 878 T B M SUPPLEMENT 6 ”BFG” STORMSCOPE SECTION 4 NORMAL PROCEDURES Normal operating procedures of the ”BFG” stormscope are outlined in : -- the Pilot’s Handbook, Series II, No. 75--0299--7690--1 at its last revision for ”BFG” stormscope model WX--1000 or 1000+ or 1000E -- the WX--950 Pilot’s Guide, Series II, No.
Page 879 T B M SUPPLEMENT 6 ”BFG” STORMSCOPE SECTION 6 WEIGHT AND BALANCE Informations hereafter supplement the ones given for the standard airplane in Section 6 ”Weight and balance” of the basic Pilot’s Operating Handbook. WEIGHT EQUIPMENT per unit OPTIONAL EQUIPMENT SUPPLIER (kg) 34 - - NAVIGATION...
Page 880 T B M SUPPLEMENT 6 ”BFG” STORMSCOPE WEIGHT EQUIPMENT per unit OPTIONAL EQUIPMENT SUPPLIER (kg) Stormscope WX--500 4.94 232.28 -- shared with the GNS 530 GPS or with (2.240) (5.900) the KMD 850 or GMX 200 MFD (OPT 70 34056A) Stormscope WX--500 4.94...
Page 881 T B M SUPPLEMENT 6 ”BFG” STORMSCOPE SECTION 7 DESCRIPTION The ”BFG” (Series II) stormscope, weather mapping system provides a visual screen readout of the electrical discharges associated with thunderstorms. This information with proper interpretation, will allow the pilot to detect severe thunderstorm activity. A series of green dots or of strike points will be displayed on the screen to indicate the electrical discharge areas.
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