DOCSLIB.ORG

Tbm 930 Pilot's Information Manual

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text

Load more

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.
Recommended publications
  • Forerunner®‎ 55 Owner's Manual

    Forerunner®‎ 55 Owner's Manual

    FORERUNNER® 55 Owner’s Manual © 2021 Garmin Ltd. or its subsidiaries All rights reserved. Under the copyright laws, this manual may not be copied, in whole or in part, without the written consent of Garmin. Garmin reserves the right to change or improve its products and to make changes in the content of this manual without obligation to notify any person or organization of such changes or improvements. Go to www.garmin.com for current updates and supplemental information concerning the use of this product. Garmin®, the Garmin logo, ANT+®, Auto Lap®, Auto Pause®, Edge®, and Forerunner® are trademarks of Garmin Ltd. or its subsidiaries, registered in the USA and other countries. Body Battery™, Connect IQ™, Firstbeat Analytics™, Garmin Connect™, Garmin Express™, Garmin Index™, Garmin Move IQ™, and TrueUp™ are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin. Android™ is a trademark of Google Inc. Apple®, iPhone®, and Mac® are trademarks of Apple Inc., registered in the U.S. and other countries. The BLUETOOTH® word mark and logos are owned by the Bluetooth SIG, Inc. and any use of such marks by Garmin is under license. The Cooper Institute®, as well as any related trademarks, are the property of The Cooper Institute. iOS® is a registered trademark of Cisco Systems, Inc. used under license by Apple Inc. Windows® and Windows NT® are registered trademarks of Microsoft Corporation in the United States and other countries. Zwift™ is a trademark of Zwift, Inc. Other trademarks and trade names are those of their respective owners.
  • Wing Root & Landing Gear Door Seal Replacement

    Wing Root & Landing Gear Door Seal Replacement

    Wing Root & Landing Gear Door Seal Replacement One of the oldest original components remaining on my Baron (and likely other members planes) was surely the stiff and ragged wing root seal. In researching this component I learned that the wing root and tail seals were installed on the wings and tails before the marriage to the airframe. What lies below the top skin of the wing and tail is a length of rubber “finger” (Figure 1) as an integral part of the seal. Figure 1 This “finger” holds the seal in place and was likely glued at the factory, grabbing the backside of the wing and tail skin. With time and age these original rubber seals have taken quite a beating. With an extended winter annual downtime this year I chose to tackle this really tedious project while waiting for other components that were out for overhaul. A word of caution, this is as tedious as it gets if you choose to dig out the finger from below the top surface skins using the very narrow gap between the skin and the fuselage. Here is a pirep from a Bonanza A36 owner on how he tackled his seal replacement: “I cut the majority of the old seal off using razor blade, leaving a small lip sticking above the wing. I then used a small pick bent at a 90 degree angle, with about a 3/8" 'hook' on the end. Using the hook, I stuck it under the wing skin, between the skin and the old rubber wing seal lip under the skin, and forced it along the chord of the wing.
  • MANUAL REVISION TRANSMITTAL Manual 146 (61-00-46) Propeller Owner's Manual and Logbook

    MANUAL REVISION TRANSMITTAL Manual 146 (61-00-46) Propeller Owner's Manual and Logbook

    HARTZELL PROPELLER INC. One Propeller Place Piqua, Ohio 45356-2634 U.S.A. Telephone: 937.778.4200 Fax: 937.778.4391 MANUAL REVISION TRANSMITTAL Manual 146 (61-00-46) Propeller Owner's Manual and Logbook REVISION 3 dated June 2012 Attached is a copy of Revision 3 to Hartzell Propeller Inc. Manual 146. Page Control Chart for Revision 3: Remove Insert Page No. Page No. COVER AND INSIDE COVER COVER AND INSIDE COVER REVISION HIGHLIGHTS REVISION HIGHLIGHTS pages 5 and 6 pages 5 and 6 SERVICE DOCUMENTS LIST SERVICE DOCUMENTS LIST pages 11 and 12 pages 11 and 12 LIST OF EFFECTIVE PAGES LIST OF EFFECTIVE PAGES pages 15 and 16 pages 15 and 16 TABLE OF CONTENTS TABLE OF CONTENTS pages 17 thru 24 pages 17 thru 26 INTRODUCTION INTRODUCTION pages 1-1 thru 1-14 pages 1-1 thru 1-16 DESCRIPTION AND DESCRIPTION AND OPERATION OPERATION pages 2-1 thru 2-20 pages 2-1 thru 2-24 INSTALLATION AND INSTALLATION AND REMOVAL REMOVAL pages 3-1 thru 3-22 pages 3-1 thru 3-24 TESTING AND TESTING AND TROUBLESHOOTING TROUBLESHOOTING pages 4-1 thru 4-10 pages 4-1 thru 4-10 continued on next page Page Control Chart for Revision 3 (continued): Remove Insert Page No. Page No. INSPECTION AND INSPECTION AND CHECK CHECK pages 5-1 thru 5-24 pages 5-1 thru 5-26 MAINTENANCE MAINTENANCE PRACTICES PRACTICES pages 6-1 thru 6-36 pages 6-1 thru 6-38 DE-ICE SYSTEMS DE-ICE SYSTEMS pages 7-1 thru 7-6 pages 7-1 thru 7-6 NOTE 1: When the manual revision has been inserted in the manual, record the information required on the Record of Revisions page in this manual.
  • Gpsbabel Documentation Gpsbabel Documentation Table of Contents

    Gpsbabel Documentation Gpsbabel Documentation Table of Contents

    GPSBabel Documentation GPSBabel Documentation Table of Contents Introduction to GPSBabel ................................................................................................... xx The Problem: Too many incompatible GPS file formats ................................................... xx The Solution ............................................................................................................ xx 1. Getting or Building GPSBabel .......................................................................................... 1 Downloading - the easy way. ....................................................................................... 1 Building from source. .................................................................................................. 1 2. Usage ........................................................................................................................... 3 Invocation ................................................................................................................. 3 Suboptions ................................................................................................................ 4 Advanced Usage ........................................................................................................ 4 Route and Track Modes .............................................................................................. 5 Working with predefined options .................................................................................. 6 Realtime tracking ......................................................................................................
  • 2018 Annual Report

    2018 Annual Report

    2018 ANNUAL REPORT LETTER FROM THE CEO DEAR SHAREHOLDER, Garmin delivered solid financial results in 2018, our third consecutive year of consolidated revenue and profit growth. Our success was driven by strong performance by four of our five reportable segments, which reported double-digit revenue growth. The year offered much to celebrate, including the opening of our new manufacturing facility in Olathe, Kansas, which more than doubled our North American manufacturing capacity. This investment reinforces Garmin's continued commitment to our customers, associates, shareholders and community. We also shipped nearly 15 million units during the year and more than 205 million units since inception, including more than 1 million certified aviation products. We not only expanded our physical footprint but also our product lines and market presence by entering new product categories. Growth in the Aviation segment was driven by the ADS-B equipage mandate, new products and aircraft certifications, while growth in Outdoor and Fitness segments was driven by wearable product categories. The Marine segment grew at a faster rate than the market because of game-changing innovations and market share gains. While we continue to see a decline of the PND market size, our share of the market remains strong. We are very pleased with our accomplishments in 2018 and are optimistic about what we can achieve in the coming year. In 2019, Garmin will celebrate its 30th anniversary. As we reflect on how far we've come and the growth of our business, it is just as exciting to think about the possibilities that lie before us.
  • Automated Generic Parameterized Design of Aircraft Fairing and Windshield

    Automated Generic Parameterized Design of Aircraft Fairing and Windshield

    Automated generic parameterized design of aircraft fairing and windshield Vijaykumar Govindharajan Aakash Narender Singh LIU-IEI-TEK-A-12/01271-SE Department of Management and Engineering Division of Flumes Department of Management and Engineering SE-581 83 Linköping, Sweden i ii Upphovsrätt Detta dokument hålls tillgängligt på Internet – eller dess framtida ersättare – under 25 år från publiceringsdatum under förutsättning att inga extraordinära omständigheter uppstår. Tillgång till dokumentet innebär tillstånd för var och en att läsa, ladda ner, skriva ut enstaka kopior för enskilt bruk och att använda det oförändrat för ickekommersiell forskning och för undervisning. Överföring av upphovsrätten vid en senare tidpunkt kan inte upphäva detta tillstånd. All annan användning av dokumentet kräver upphovsmannens medgivande. För att garantera äktheten, säkerheten och tillgängligheten finns lösningar av teknisk och administrativ art. Upphovsmannens ideella rätt innefattar rätt att bli nämnd som upphovsman i den omfattning som god sed kräver vid användning av dokumentet på ovan beskrivna sätt samt skydd mot att dokumentet ändras eller presenteras i sådan form eller i sådant sammanhang som är kränkande för upphovsmannens litterära eller konstnärliga anseende eller egenart. För ytterligare information om Linköping University Electronic Press se förlagets hemsida http://www.ep.liu.se/. Copyright The publishers will keep this document online on the Internet – or its possible replacement – for a period of 25 years starting from the date of publication barring exceptional circumstances. The online availability of the document implies permanent permission for anyone to read, to download, or to print out single copies for his/her own use and to use it unchanged for non-commercial research and educational purpose.
  • Lighting up to 7 Times Brighter Than Other LED Landing Lights!

    Lighting up to 7 Times Brighter Than Other LED Landing Lights!

    Lighting FAA-PMA Approved AeroLEDs Lighting Increase safety and reduce operating cost! See the Difference... Lighting Know the Difference... • Increased safety • Direct replacement • Up to 80% reduced power consumption • Long life - over 50,000 hours! • Lighter weight - no heavy power supply - save up to 3 lbs • Reduced drag • Zero maintenance • 10x more efficient than incandescent! Increased Safety AeroLED lights allow you to comply with the latest FAA recommendations (Operation Lights On) regarding extended use of taxi, landing, and anti-collision lights without fear of reduced light performance or life. They all feature optimized light color (6500k sunlight equivalent) for proven superior air-to-air recognition. The landing and taxi lights also feature an optional pulsed recognition light mode. Reduced Power Consumption High efficiency LED lights use less than 1/3 the power of halogen bulbs. They significantly reduce the load on the electrical system and they won't dim due to low voltage, typical of low RPM final approaches when you need them most! Postition lights aerodynamic design results in less drag than original equipment! Longer Life - Zero Maintenance All AeroLED products are designed to be a "lifetime buy". They last over 50,000 hours when properly installed and do not degrade with on/off cycles. They are extremely rugged and hardened against all kinds of electrical damage, shock, and vibration. Up to 7 times brighter than other LED landing lights! PAR36 Landing Light Comparison Measured Brightness at 50 Ft. Manufacturer Intensity
  • Android (Operating System) 1 Android (Operating System)

    Android (Operating System) 1 Android (Operating System)

    Android (operating system) 1 Android (operating system) Android Home screen displayed by Samsung Nexus S with Google running Android 2.3 "Gingerbread" Company / developer Google Inc., Open Handset Alliance [1] Programmed in C (core), C++ (some third-party libraries), Java (UI) Working state Current [2] Source model Free and open source software (3.0 is currently in closed development) Initial release 21 October 2008 Latest stable release Tablets: [3] 3.0.1 (Honeycomb) Phones: [3] 2.3.3 (Gingerbread) / 24 February 2011 [4] Supported platforms ARM, MIPS, Power, x86 Kernel type Monolithic, modified Linux kernel Default user interface Graphical [5] License Apache 2.0, Linux kernel patches are under GPL v2 Official website [www.android.com www.android.com] Android is a software stack for mobile devices that includes an operating system, middleware and key applications.[6] [7] Google Inc. purchased the initial developer of the software, Android Inc., in 2005.[8] Android's mobile operating system is based on a modified version of the Linux kernel. Google and other members of the Open Handset Alliance collaborated on Android's development and release.[9] [10] The Android Open Source Project (AOSP) is tasked with the maintenance and further development of Android.[11] The Android operating system is the world's best-selling Smartphone platform.[12] [13] Android has a large community of developers writing applications ("apps") that extend the functionality of the devices. There are currently over 150,000 apps available for Android.[14] [15] Android Market is the online app store run by Google, though apps can also be downloaded from third-party sites.
  • Propeller Operation and Malfunctions Basic Familiarization for Flight Crews

    Propeller Operation and Malfunctions Basic Familiarization for Flight Crews

    PROPELLER OPERATION AND MALFUNCTIONS BASIC FAMILIARIZATION FOR FLIGHT CREWS INTRODUCTION The following is basic material to help pilots understand how the propellers on turbine engines work, and how they sometimes fail. Some of these failures and malfunctions cannot be duplicated well in the simulator, which can cause recognition difficulties when they happen in actual operation. This text is not meant to replace other instructional texts. However, completion of the material can provide pilots with additional understanding of turbopropeller operation and the handling of malfunctions. GENERAL PROPELLER PRINCIPLES Propeller and engine system designs vary widely. They range from wood propellers on reciprocating engines to fully reversing and feathering constant- speed propellers on turbine engines. Each of these propulsion systems has the similar basic function of producing thrust to propel the airplane, but with different control and operational requirements. Since the full range of combinations is too broad to cover fully in this summary, it will focus on a typical system for transport category airplanes - the constant speed, feathering and reversing propellers on turbine engines. Major propeller components The propeller consists of several blades held in place by a central hub. The propeller hub holds the blades in place and is connected to the engine through a propeller drive shaft and a gearbox. There is also a control system for the propeller, which will be discussed later. Modern propellers on large turboprop airplanes typically have 4 to 6 blades. Other components typically include: The spinner, which creates aerodynamic streamlining over the propeller hub. The bulkhead, which allows the spinner to be attached to the rest of the propeller.
  • 2020 Jeep® Compass

    2020 Jeep® Compass

    2020 JEEP® COMPASS SELECT STANDARD FEATURES NEW Ventilated Leather-Trimmed Seats — Available on Trailhawk® and Limited models NEW Driver’s Seat Memory — Available on Trailhawk and Limited models NEW Alpine® Premium Speakers — Available on Latitude, Trailhawk and Limited models NEW Power Eight-Way Passenger Seat with Power Four-Way Lumbar Adjuster Jeep Active Drive 4x4 Systems — 4x4 models Jeep Active Drive Low 4x4 System with Hill Descent Control — Trailhawk models Selec-Terrain® Traction Management System with up to Five Modes — 4x4 models 60/40 Split-Folding Rear Seats and Center Armrest with Cup Holders Air Conditioning with Dual-Zone Automatic Temperature Controls Apple CarPlayTM(16) iPhone® Integration and Android AutoTM(9) Smartphone Compatible Daytime Running Lamp System Driver Information Display in 3.5-inch Black-and-White or 7-inch Full-Color Display Full-Length Front Floor Console with Sliding Armrest in Soft Vinyl and Cup Holders Height-Adjustable Load Floor with up to Three-Position Adjustment Integrated Voice Command with Bluetooth® Media Hub with USB Port and Auxiliary Input Jack; 2nd USB Port on Back of Center Console Power Front Windows, One-Touch Up and Down Power-Heated, Power-Adjusting and Manual-Folding Side Mirrors Quad-Halogen Headlamps with Off-Time Delay Remote Keyless/Illuminated Entry with Push-Button Start Steering Wheel with Mounted Audio and Cruise Controls Two 12-Volt and Available 115-Volt Outlets Uconnect® 7-inch or 8.4-inch Touchscreen Display Radios SAFETY & SECURITY Adaptive Cruise Control with Stop
  • Fuel Tank Maintenance & Safety

    Fuel Tank Maintenance & Safety

    Slide 1 Fuel Tank Maintenance & Safety This fuel tank safety course will deal with inspections and preventions required to identify ignition sources of the design. The reason for concern about Fuel Tank Safety The proposal stemmed from the July 1995 TWA Flight 800 explosion over the Atlantic. The Boeing 747 broke apart after takeoff from New York, killing all 230 people aboard. Investigators believe a wiring problem triggered a spark that ignited fuel vapors in the jet's center tank. In November 15, 2005 US airlines and aircraft manufacturers would have to equip more than 3,200 passenger jets with safety systems to reduce the potential of fuel tank fire or explosions, according to a Federal Aviation Administration Maintenance training for the technicians is one of those safety features. The maintenance of ignition prevention is necessary for the inherent safety and reliability of an aircraft’s fuel tank system. The aircraft cannot be operated indefinitely with the failure of an ignition prevention feature. The failure will have a direct adverse effect on operational safety. The Fuel Tank Safety program will prevent catastrophic failure and allow safe flight and landing of the aircraft without serious or fatal injury to the occupants. This fuel tank safety course will deal with inspections and preventions required to identify ignition sources of the design. The failure of any of these design sources may not immediately result in an unsafe condition, but it may warrant certain maintenance to support continued airworthiness. Note: A large percentage of the work involved in properly inspecting and modifying airplane fuel tanks and their systems this must be done in the inside of the tanks.
  • Bell 429 Product Specifications

    Bell 429 Product Specifications

    BELL 429 SPECIFICATIONS BELL 429 SPECIFICATIONS Publisher’s Notice The information herein is general in nature and may vary with conditions. Individuals using this information must exercise their independent judgment in evaluating product selection and determining product appropriateness for their particular purpose and requirements. For performance data and operating limitations for any specific mission, reference must be made to the approved flight manual. Bell Helicopter Textron Inc. makes no representations or warranties, either expressed or implied, including without limitation any warranties of merchantability or fitness for a particular purpose with respect to the information set forth herein or the product(s) and service(s) to which the information refers. Accordingly, Bell Helicopter Textron Inc. will not be responsible for damages (of any kind or nature, including incidental, direct, indirect, or consequential damages) resulting from the use of or reliance on this information. Bell Helicopter Textron Inc. reserves the right to change product designs and specifications without notice. © 2019 Bell Helicopter Textron Inc. All registered trademarks are the property of their respective owners. FEBRUARY 2019 © 2019 Bell Helicopter Textron Inc. Specifications subject to change without notice. i BELL 429 SPECIFICATIONS Table of Contents Bell 429 ..................................................................................................................................1 Bell 429 Specification Summary (U.S. Units) ........................................................................4