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Tbm 930 Pilot's Information Manual

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Tbm 930 Pilot's Information Manual TBM 930 Airplane equipped with MOD70--0476--00 PILOT'S INFORMATION MANUAL P/N T00.DMJPIPYEE0 - EDITION 0 - REVISION 1 CAUTION THIS INFORMATION MANUAL IS A NON-OFFICIAL COPY OF THE PILOT'S OPERATING HANDBOOK AND MAY BE USED FOR GENERAL INFORMATION PURPOSES ONLY. IT IS NOT KEPT CURRENT AND THEREFORE CANNOT BE USED AS A SUBSTITUTE FOR AIRWORTHINESS AUTHORITIES APPROVED MANUAL WHICH IS THE ONLY ONE INTENDED FOR OPERATION OF THE AIRPLANE. The content of this document is the property of SOCATA S.A.S. 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 writing from the owners of the Copyright. Information in this document is subject to change without notice. © 2015 - 2016 - SOCATA S.A.S All rights reserved SOCATA S.A.S Customer support 65921 TARBES CEDEX 9 FRANCE Printed in FRANCE SECTION 0 PILOT'S OPERATING HANDBOOK SOCATA MODIFICATIONS - INDEX NOTE The standardized name for SOCATA modifications is : MOD70-XXXX-XX MOD70 No. SUBJECT CLASSIF. 70-0258-00D Traffic Advisory System GARMIN GTS820 minor Installation 70-0322-00 Evolution of wing tips, tail cone and lights Major 70-0323-71 Propulsion efficiency improvement Major 70-0324-00 Modified pedestal and Single Lever Power Major Control Assy 70-0325-21 Automatic altitude cabin selection Major 70-0357-71 Takeoff and landing at 850 shp - Increase of Major takeoff power 70-0374-25 Servicing plugs minor 70-0379-23 Capability for future integration of the CPDLC minor (Controller Pilot Data Link Communication) antenna 70-0401-92 Illuminated pushbuttons minor 70-0423-34A Safe flight lift transducer and AoA computer minor installation 70-0430-34 Radome with reduced honeycomb structure minor 70-0437-25B ARTEX ELT 1000 Emergency locator transmitter minor 70-0449-11B Interior paint - Authorization to apply Paint P58 minor 70-0450-76 Single lever power control HA1210003 Amdt A minor 70-0455-31 Lightweight Flight Data Recorder (ADRS CARS) minor 70-0457-92 HMI – Panels equipped for G3000 dashboard minor 70-0458-23B A68a- GDL 69A SXM - XM Generation 4 minor 70-0459-46C Flight stream 210 installation (GARMIN) minor 70-0463-92 Unique PL45 push test button minor Edition 0 - December 31, 2015 Page 0.6A Rev. 1 SECTION 0 PILOT'S OPERATING HANDBOOK MOD70 No. SUBJECT CLASSIF. 70-0464-53 G3000 Instrument panel : Definition and minor mechanical installation 70-0465-53 G3000 Anti-glare shield : Definition and minor mechanical installation 70-0466-53 Dashboard fasteners - Modification of the minor fasteners of the fittings 70-0467-21 G3000 HAD – HAD Mechanical adaptation for minor G3000 dashboard 70-0468-32 G3000 pilot door TBM parking brakes – Parking minor brakes mechanical adaptation for G3000 70-0469-32 G3000 large door TBM parking brakes – Parking minor brakes mechanical adaptation for G3000 70-0471-34A Airspeedsyst. –mechanical adaptation toG3000 minor 70-0476-00 G3000 Integrated Flight Deck Major 70-0476-00C G3000 integrated Flight deck - Major Version C : Software for ESP/USP function 70-0476-00D G3000 integrated Flight deck - minor Version D : Software for radar function 70-0476-00E G3000 integrated Flight deck - minor Version E : Software for HF receiver function 70-0476-00F G3000 integrated Flight deck - minor VersionF:SDcardforaudioalertvolumefunction 70-0476-00G G3000 integrated Flight deck - minor Version G : Software for PDF viewer, Flight Stream 210 functions and for GTX345 transponder limited compatibility 70-0477-00 Printed circuit U60 minor 70-0484-53 Modification of the upper fittings of the dashboard minor 70-0485-11 Modification of oxygen switch placards Major 70-0487-23 Bose A20 Headset P/N 324843-3040 minor 70-0488-27 ESP Software unlock card minor 70-0495-92 Cabin electrical harness for 7Y9Y aircraft - design minor and installation Page 0.6B Edition 0 - December 31, 2015 Rev. 1 SECTION 0 PILOT'S OPERATING HANDBOOK MOD70 No. SUBJECT CLASSIF. 70-0498-57 Improvement of lift transducer integration minor 70-0499-30 Modification for lift transducer capability minor 70-0500-25 2016 interior - 2016 carbon finish minor 70-0504-11 Passengers A/C control label minor 70-0513-70 Introduction of HTS engine oil per P&WC minor SB14001 70-0518-23 Time delay relay K21B minor 70-0521-21 Motor brushes for B12 fan minor 70-0524-21 ITS reliability improvement minor 70-0525-28 Fuel hose : new lower pressure switch location minor 70-0528-34 New manufacturing process of pitot probe minor bracket 70-0532-92 PL1 panel structure minor 70-0534-33 Backlighted cabin air contioning control minor 70-0537-21 Modification of BTSW (S210) and BLEED switch minor (S80) electrical wiring on TBM930 70-0538-24 Capability to connect a battery charger minor 70-0540-24 Alternator interference alternator minor 70-0545-46 PDF viewer installation (GARMIN) minor 70-0552-92 Wiring for GAS CAS messages on GX000 minor 70-0554-25 1” back of the pilot seat minor NOTE Optional modifications are integrated in the list of equipment - refer to the list of equipment available in SOCATA Report reference NAV No. 34/90-RJ-App 4, located at the end of this POH. Edition 0 - December 31, 2015 Page 0.6C Rev. 1 SECTION 0 PILOT'S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 0.6D Edition 0 - December 31, 2015 Rev. 1 SECTION 0 PILOT'S OPERATING HANDBOOK TABLE OF CONTENTS SECTION GENERAL 1 LIMITATIONS 2 EMERGENCY PROCEDURES 3 NORMAL PROCEDURES 4 PERFORMANCE 5 WEIGHT AND BALANCE 6 DESCRIPTION 7 AIRPLANE HANDLING, SERVICING AND 8 MAINTENANCE SUPPLEMENTS 9 Edition 0 - December 31, 2015 Page 0.7 Rev. 0 SECTION 1 GENERAL PILOT'S OPERATING HANDBOOK SECTION 1 GENERAL TABLE OF CONTENTS 1.1 - GENERAL ............................................. 1.1.1 1.2 - THREEVIEWDRAWING ................................. 1.2.1 1.3 - DESCRIPTIVEDATA .................................... 1.3.1 ENGINE ............................................. 1.3.1 PROPELLER ........................................ 1.3.1 FUEL ............................................... 1.3.2 ENGINE OIL ......................................... 1.3.3 MAXIMUM CERTIFICATED WEIGHTS .................. 1.3.3 STANDARD AIRPLANE WEIGHTS ..................... 1.3.3 CABIN AND ENTRY DIMENSIONS ..................... 1.3.4 SPECIFIC LOADINGS ................................. 1.3.4 1.4 - ABBREVIATIONS AND TERMINOLOGY ................... 1.4.1 METEOROLOGICAL TERMINOLOGY ................... 1.4.1 GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS . 1.4.1.. POWER TERMINOLOGY .............................. 1.4.2 AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY ........................... 1.4.2 WEIGHT AND BALANCE TERMINOLOGY ............... 1.4.2 GENERAL ABBREVIATIONS .......................... 1.4.4 RADIO - NAVIGATION ABBREVIATIONS ................ 1.4.7 1.5 - CONVERSIONFACTORS ................................ 1.5.1 1.6 - PRESSURE AND STANDARD ATMOSPHERE .............. 1.6.1 STANDARD ATMOSPHERE ........................... 1.6.1 PRESSURE CONVERSION TABLE ..................... 1.6.2 Edition 0 - December 31, 2015 Page 1.0.1 Rev. 0 SECTION 1 GENERAL PILOT'S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 1.0.2 Edition 0 - December 31, 2015 Rev. 0 SECTION 1 GENERAL PILOT'S OPERATING HANDBOOK 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 airplane. It also contains supplemental data supplied by the manufacturer. The ”GARMIN” G3000 Integrated Flight Deck Pilot's Guide, No. 190-02046-00, or any later version as applicable, must be permanently kept in the airplane with the Pilot's Operating Handbook. The Pilot's Guide for the MD302 Standby Attitude Module P/N 9017846 Rev. E or any later version as applicable, must be permanently kept in the airplane with the Pilot's Operating Handbook. Section 1 provides basic data and information of general interest. It also contains definitions or explanations of abbreviations and terminology commonly used. The general for complex optional systems are given in Section 9, ”Supplements” of the Pilot's Operating Handbook. The installed ADS-B OUT system has been shown to meet the equipment requirements of 14 CFR 91.227. PART 135 OPERATIONS For14CFR 135operations, TBMaircraft alternativesource ofelectric powerisableto supply 150 percent of the electrical loads of all required instruments and equipment for safe emergency operation of the aircraft for at least 1 hour. Electrical load shedding procedure provided in Section 3 of this POH must be followed in order to meet the requirements of that Paragraph under 14 CFR 135.163(f)(2). Edition 0 - December 31, 2015 Page 1.1.1 Rev. 1 SECTION 1 GENERAL PILOT'S OPERATING HANDBOOK INTENTIONALLY LEFT BLANK Page 1.1.2 Edition 0 - December 31, 2015 Rev. 0 SECTION 1 GENERAL PILOT'S OPERATING HANDBOOK 1.2 - THREE VIEW DRAWING * Airplane on level field with fully extended FWD shock-absorber Figure 1.2.1 (1/2) - THREE VIEW DRAWING Edition 0 - December 31, 2015 Page 1.2.1 Rev. 1 SECTION 1 GENERAL PILOT'S OPERATING HANDBOOK Figure 1.2.1 (2/2) - THREE VIEW DRAWING Page 1.2.2 Edition 0 - December 31, 2015 Rev. 0 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 - 66D Engine type : Free turbine, reverse flow and 2 turbine sections Compressor type : 4 axial stages 1 centrifugal stage Combustion chamber type : Annular Turbine type : 1 gas generator turbine stage 2 power turbines stages Horsepower rating and propeller speed : 850 SHP at 2000 RPM PROPELLER Number of propellers : 1 Propeller manufacturer : HARTZELL Propeller model number : HC-E5N-3C / NC8834K Number of blades : 5 Propeller diameter : Minimum : 90 inches (2.286 m) Maximum : 91 inches (2.311 m) Propeller type : Adjustable constant speed, with feathering and hydraulic control reverse Propeller blade setting at 30 inches station Low pitch : 19.5° Feathering : 85° Maximum reverse : - 9° Propeller governor : 8210.007 WOODWARD Edition 0 - December 31, 2015 Page 1.3.1 Rev.
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