Aircraft Technical Resources List Updated April 2021

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Aircraft Technical Resources List Updated April 2021 Aircraft Technical Resources List Updated April 2021 Below is a list compiled by ABS’ Technical Advisors of facilities known to provide the indicated services. Inclusion on this list does not imply endorsement of a particular resource or preference of that resource over others. Lack of appearance on the list does not imply a recommendation against a particular resource or location. See the Shops and Mechanics Recommendations page (from Members Only at www.bonanza.org) for ABS member reviews of maintenance providers, and to post your own reviews. Please review your experience with providers on this list. Additional sources may also be found in display and classified advertising in ABS Magazine. Please contact ABS at [email protected] if you know of additional resources to add to this list. Air conditioner Conversion to R-134 API Memphis 888-274-2497 Steinbach & Associates 254-751-7420Steinbach & Associates Aftermarket a/c installations Air Center www.aircenterinc.com Aircraft Systems www.ftaaviation.com Keith Products www.keithproducts.com New style A/C Systems 615-587-3492 Alternator Exchange/overhaul Accessories, Inc. 800-926-0707 Executive Accessories, Inc. 954-493-9262 Aircraft Electrical Components 530-221-4397 Aerotech 800-634-0190 Autopilot Tacair autopilot repairs Modern Avionics and Maintenance 216-267-3998 or 216-702-7069 KFC 200 troubleshooting, repairs Windward Aviation 800-846-8668 and parts Island Aviation 904-261-3730 Autopilot Central 918-836-6418 Lowe Aviation 478-788-3491 Battery STC to relocate battery box forward Aviation Research Systems 503-668-4542 of firewall D’Shannon Aviation www.d-shannon-aviation.com Hammock Aviation 972-875-4279 Battery box relocation installation Air Mod 513-732-6688 Kalamazoo Aircraft 210-381-0790 Cargo net Replacement cargo net Cameron Interiors 630-584-9366 CHT indicator CHT indicator troubleshooting/rebuild Instrument Rebuild 360-683-6245 Thermocouple probe source Instrument Technology 800-229-9078 Technical resources list. Inclusion or exclusion from this list does not imply endorsement or recommendation. 1 AirParts of Lock Haven 570-748-0823 Replacement gauge light bulbs Kelly 800-835-1054 Century 800-733-0116 Air Capital 316-942-8668 Instrument Technology 800-229-9078 Lewis engine Co. probe replacement Avstat 888-287-8283 O'Halloran Aviation 580-832-3803 Clock Digital clock source Aircraft Spruce 800-329-3020 Astrotech clock repair Transicoil 800-323-7115 Control locks Throw-over style control locks White 800-821-7733 Dodson 800-255-0034 1984 and later 36, 58 style RAPID 888-727-4344 Avstat 888-287-8283 Select 800-318-0010 Arrell 805-604-0439 Control surface reskin Control surface reskin shops Biggs 405-258-2965 Deason Aircraft Service 913-755-4107 Hampton 479-394-5290 STC’d aluminum elevator skins SRS 877-364-8003 Guidance for preparing magnesium FAA Advisory Circular AC43-4a chapters 4 and 6. Cowl flaps Electric cowl flap motor repair/rebuild Aircraft Accessories of Oklahoma 800-255-9924 Aircraft Systems 815-399-0225 Crossroads 972-239-0263 B & S 316-264-2397 Manual cowl flaps for early Barons Aero Crafters www.aero-crafters.com 800-628-2567 Cowlings and nacelles Replacement nacelle fairings Globe Fiberglass 800-899-2707 Knots2U LTD 262-763-5100 Doors Source of inflatable door seal Performance Aero 800-200-3141 Cabin door hinge replacements Crossroads 972-239-0263 Biggs 405-258-2965 Hampton 479-394-5290 DBM 314-406-1389 Replacement door locks Aviation Research Systems 503-668-4542. Technical resources list. Inclusion or exclusion from this list does not imply endorsement or recommendation. 2 Dual control yoke Dual control yoke rentals Cygnet 805-528-2376 Air Mech 580-832-3803 CruiseAir 760-789-8020 Garhawk 800-686-9887 Woodland Aviation 800-442-1333 Lawson Barber 559-675-0183 Kevin Andrews 317-519-3596 Gallagher Aviation 833-425-5288 (check availability at https://www.gallagheraviationllc.com/beech-dual-yoke-rental.html) Replacement (new) dual yoke Cygnet 805-528-2376 Electric trim Pitch trim switch parts Elliott Beechcraft 309-799-3183 ELT ELT repair Merl 203-237-8811 CIR replacement ELT battery Merl 203-237-8811 Encoding altimeter Rebuilding Kelly 800-835-1054 Century 800-733-0116 Engine upgrade STCs IO-470C to –N conversion Powermasters 918-299-0269 Machen conversion Machen 800-426-5085 Al Hoover Equipment list Original factory equipment list for Beech tech support 800-625-7043, ext. 4 menu item 1 a specific serial number airplane E-series engines Overhaul and accessory drive O/H Poplar Grove 800-397-8181 Cruiseair Aviation 760-789-8020 E-series experienced CFIs Craig Bailey, Poplar Grove, IL [email protected] Jack Oliphant, Fort Collins, CO [email protected] Bill Hale, Fort Collins, CO [email protected] Ron Timmermans, Ft Worth, TX [email protected] STC’d electric auxiliary pump for James 918-786-4506 E-225 Bonanzas STC to convert PS5C carburetor D&G Supply 269-684-4440 www.dgsupply.com to fuel injection (E-185/E-225) Firewall Firewall sealing putty Aircraft Spruce 877-477-7823 p/n FWCAULK Technical resources list. Inclusion or exclusion from this list does not imply endorsement or recommendation. 3 Flaps Flap motor overhaul Kelly Aerospace (Aero Electric) 316-943-6100 Aircraft Systems 815-399-0225 George’s Electric 916-922-4277 Flap position indicators repair Instrument Rebuild 360-683-6245 Fuel caps Gabb fuel caps source Performance Aero 800-200-3141 Select 800-318-0010 Arrell 805-604-0439 Avitat 888-287-8283 Locking fuel caps Aviation Research Systems 503-668-4542 Fuel indicators Circuit board repair John Birks 309-686-0614 Sender unit repair John Wolfe 440-942-0083 Air Parts of Lock Haven 570-748-0823 Stewart-Warner and Rochester repairs Instrument Rebuild 360-683-6245 Fuel injection system Simmonds system repairs Central Cylinder 402.451.6468 www.centralcylinder.com (only FAA authorized repair; no parts available) Fuel pump Overhaul Dukes electric fuel pump Aircraft Systems 815-399-0225 Dukes 818-998-2527 CJ Aviation 800-227-5772 Fuel selector Overhaul fuel selector valve Hagerstown Aircraft 301-797-8106 Cruiseair 760-789-8020 The Aviation group 770-486-1666 Fuel tanks 58P/58TC wet wing tip repair Hampton Industries 479-394-5290 Baron 55 wingtip fuel tanks Colemill 615-226-4256 ABS CD-ROM June 2000 pg. 6278 Glareshield Replacement glareshield Dennis Ashby 800-945-7668 Aircraft Spruce 800-861-3192 Glove box Cardboard replacement glove box Air Mod 513-732-6688 Aviation Research Systems 503-668-45 Crossroads Aviation 972-239-0263 Half-size (AOPA 2001 V35B) box Air Mod 513-732-6688 Technical resources list. Inclusion or exclusion from this list does not imply endorsement or recommendation. 9 58P glove box Elliott Beechcraft 309-799-3183 Air Mod 513-732-6688 Ice protection Float repairs for anti-ice fluid tank John Wolfe and Co 440-942-0083 Baron fuselage ice protection plates Sky Harbour 519-524-2165 www.skyharbour.com SRS Aviation 877-364-8003 Windshield “hot plate” repairs Aircraft Window Repairs 310-212-7139 Ignition Bendix ignition system switches Aircraft Spruce and Specialty 877-477-7823 Replacement ignition switch key Elliott Beechcraft 309-799-3183 STC modification of H35 and earlier Mark Givans 916-344-4729 [email protected] ignition switch Inspections See Shops and Mechanics Recommendations on the ABS website Instruments Source of rebuilt flight instruments Air Capital Instruments 316-942-8668 Century Instruments 800-733-0116 Kelly Instruments 800-835-1054 Rebuilt 2-in-one CHT/EGT gauge Air Capital Instruments 316-942-8668 Kelly 800-835-1054 Quad City Instruments 309-507-1280. ABS discount Rebuilt instrument air gauge Century 800-733-0116 Kelly 800-835-1054 Midcontinent 316-630-0101 Instrument Air Vacuum pump conversion STC Airwolf 800-326-1534, www.airwolf.com) Standby instrument air pump Rapco 800-527-2726 Intercooler A36TC/B36TC intercooler STC Turbo Plus 800-742-4202 Gary Main, Main Turbo 800-847-8815 Jacks Source of Beech jacks 561-467-2040 or 626-401-9727 Meyers Jacks at Wag Aero 800-558-6868 Landing gear Landing gear advisory system P2 Engineering 888-921-8359 Strut overhaul Delta Strut 559-662-0421 Landing gear motor rebuild Aero Accessories 800-926-0701 Aircraft Systems 815-399-0225 George’s Electric 916-922-4277 Cruiseair 760-789-8020 Technical resources list. Inclusion or exclusion from this list does not imply endorsement or recommendation. 10 Lift leg oversize bushings installation Texas Air Service 800-313-6506 The Aviation Group (770-486-1666) Lights and beacons Custom glareshield/panel lights www.aeroenhancement.com Grimes beacon rebuild Avlite at 805-239-4037 Strobe light rebuild Avlite at 805-239-4037 Loadmeters Loadmeter rebuild Air Capital 316-942-8668 Century 316-683-7571 Kelly 800-835-1054 Locks Replacement door locks Aviation Research Systems 503-668 4542 Magnetos Magneto service, repair and overhaul Executive Accessories, Inc. 954-493-9262 Quality Aircraft Accessories 800-255-9924 Eagle Magnetos 386-235-3152 OAT gauge Replacement OAT gauge Avstat 888-287-8283 Oil Analysis Oil analysis labs Blackstone Labs 260 744-2380 Howard Fenton, SECOND OilPINION 918-492-5844, Aviation Labs 800-256-6876 Oil temperature New oil temperature sending unit Crossroads Aviation 972-239-0263 Aircraft Spruce 800-861-3192 Panel upgrade Instrument panel upgrades Air Mod 513-732-6688 Aviation Research Systems 503-668-4542 D'Shannon Aviation 612-404-9000, 800-291-7616 John Whimpee 251-433-0831 Midwest Aviation 502-744-8600 Paint Paint shops: See Shops and Mechanics Recommendations on the ABS website Original paint schemes Paint numbers (no pictures): Beech 800-625-7043 x4 Larry Ball books (black and white) ABS Store Factory “Matterhorn White” Sterling Lacquer 314-776-4450 used by Beech Pilot’s Operating Handbook New POH Beech 800-796-2665, 316-676-3238 Reprints www.esscoaircraft.com Technical resources list.
Recommended publications
  • Thrush Aircraft, Inc
    THRUSH AIRCRAFT, INC. P.O. Box 3149 Albany, GA 31706-3149 Phone (229) 883-1440 Fax (229) 439-9790 CUSTOM KIT CUSTOM KIT No. CK-AG-40 Rev. A Date: 12/8/06 WING SPAR UPGRADE The wing spars of most early Thrush models are the subject of FAA Airworthiness Directives (most recently FAA AD 2006-07-15) which require periodic inspection of the lower wing spar caps at the splice block attach holes for fatigue cracks. This Custom Kit is an acceptable way to replace the lower spar caps, but it does more than this for the aircraft owner. It brings the spars up to the best fatigue capability that is compatible with the existing wings. This upgrade includes not only the lower spar caps that have the first two splice holes cold expanded, but it also includes new inboard webs and doublers as well as the “big butterfly” and lower splice plate. When a set of wings is rebuilt according to this Custom Kit, it will gain the initial inspection interval of a “Group 4” airplane while retaining the spar fatigue life of its current group. The inspection intervals between initial inspection and spar fatigue life limit will be the larger inspection intervals currently used for Group 4 and 5 airplanes. The upgraded wing will be as strong as or, in many cases, stronger than the original. Note that this upgrade is for both wings. If the airplane has one relatively young spar cap and it is not replaced, the inspection intervals will be based on that spar, not the new one.
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  • March 2018 5
    The Mooney Flyer y The Official Online Magazine for the Mooney Community www.TheMooneyFlyer.com March 2018 5 The Mooney Flyer Volume 7 Number 3 March 2018 Features Editors Mooney Fuel Tank Leaking – Magnetos & Hot Props Phil Corman ReSeal or Patch Jim Price writes about “Must Know” Jim Price We identify different types of leaks… information for safety with Hot Props different sources… and how to Contributing Writers determine the correct resolution. Bruce Jaeger Noorduyn Norseman C/N427 CF-GYY Blind Announcements Bob Kromer submitted by Mike Alain Tom Rouch Is the practice of Blind Broadcasts on Paul Loewen An interesting restoration by the CTAF appropriate? Jim Price answers Montreal Aviation Museum the question Geoff Lee Linda Corman Evolution of Mooney Summit EMPOA Annual Meeting Mike Elliott asked Neil Cohen to write June 14: Aschaffenburg / EDFC in To Subscribe his thoughts on the evolution of the Germany Click Here Mooney Summit. To Advertise Click Here In Every Issue To Submit an Article Click Here From the Editor Appraise Your Mooney’s Value Latest Mooney Service Bulletins If you love The Mooney Flyer and Mooney Mail – Feedback from Flyer readers. want to keep it Ask the Top Gun healthy, just click Upcoming Fly-Ins on the “Donate” button. Have You Heard? – Relevant GA news & links for the month Mooney CFIs – Across America Product Review – ARTEX ELT 4000 Click Here to Subscribe Click Here For Back Issues Page 2 The Mooney Flyer Volume 7 Number 3 March 2018 Mooney Quiz I often communicate with John Hillard, an amazing Mooniac from Down Under.
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  • Chapter 3-Deicing /Anti-Icing Fluids
    When in Doubt... Small and Large Aircraft Aircraft Critical Surface Contamination Training For Aircrew and Groundcrew Seventh Edition December 2004 2 When in Doubt…TP 10643E How to Use This Manual This manual has been organized and written in chapter and summary format. Each chapter deals with certain topics that are reviewed in a summary at the end of the chapter. The manual is divided into two parts: Part 1-for aircrew and groundcrew; Part 2-additional information for ground crew. The final chapter contains questions that any operator may utilize for their ground icing program examination. The references for each question are listed to assist with answers. The Holdover Tables (HOT) included in the appendix are solely for the use with the examination questions and must not be used for operations. Contact Transport Canada from the addresses located later in this document for the latest HOT. Warnings These are used throughout this manual and are items, which will result in: damage to equipment, personal injury and/or loss of life if not carefully followed. Cautions These are used throughout this manual and are items, which may result in: damage to equipment, personal injury or loss of life if not carefully followed. Notes These are items that are intended to further explain details and clarify by amplifying important information. Should Implies that it is advisable to follow the suggested activity, process or practice. Must Implies that the suggested activity, process or practice needs to be followed because there are significant safety
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  • Aircraft Survivability
    AIRCRAFT published by the Joint Aircraft 18FALL ISSUE Survivability Program Office SURVIVABILITY Onward to Higher Precision: Ballistic Stopping System Shows COVART 7.0 Superior Multiple-Hit Performance page 8 for CV-22 Osprey page 24 The HH-60W LFT&E Program: An Update Autonomous Self-Sealing Fuel page 12 Containment Systems: The Next Step in Fuel Tank Survivability Aircraft Survivability – The Korean page 28 War page 17 Aircraft Survivability is published three times a year by the Joint Aircraft Survivability Program TABLE OF CONTENTS Office (JASPO), chartered by the U.S. Army Aviation & Missile Command, U.S. Air Force Life Cycle Management Center, and U.S. Navy Naval Air Systems Command. 4 NEWS NOTES by Dale Atkinson 6 JCAT CORNER By Lt. Col. Andrew Roberts, CW5 Scott Brusuelas, and CDR Jay Kiser 8 ONWARD TO HIGHER PRECISION: COVART 7.0 by Rodney Stewart The last 45 years have brought great advances in the realms of computing and aircraft design. In terms of computing, we have seen the advent of desktop computing, the Internet, smartphones, cyber security, and a host of other advances that previous generations had hardly anticipated. Likewise, we have seen development and deployment of increasingly complex and technologically advanced aircraft, starting with systems such as the A-10 and F-16 in the 1970s and progressing up to the recently developed F-35 and KC-46 aircraft. The pace of progress has JAS Program Office been rapid since 1973; and, amazingly, COVART has remained a viable tool for performing ballistic 735 S. Courthouse Road vulnerability studies on aircraft all this time.
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  • US Airways Flight 1549
    Docket No. SA-532 Exhibit No. 6-A NATIONAL TRANSPORTATION SAFETY BOARD Washington, D.C. Survival Factors Group Chairman’s Factual Report (186 Pages) NATIONAL TRANSPORTATION SAFETY BOARD Office of Aviation Safety Washington, DC 20594 SURVIVAL FACTORS GROUP CHAIRMAN’S FACTUAL REPORT May 22, 2009 I. ACCIDENT Operator : US Airways, Inc. Airplane : Airbus A320-214 [N106US] MSN 1044 Location : Weehawken, NJ Date : January 15, 2009 Time : 1527 eastern standard time1 NTSB # : DCA09MA026 II. SURVIVAL FACTORS GROUP2 Group Chairman : Jason T. Fedok National Transportation Safety Board Washington, DC Member : David Lefrancq Airbus Toulouse, France Member : Barrington Johnson Association of Flight Attendants Charlotte, NC Member : Dr. Didier Delaitre Bureau d’Enquetes et d’Analyses Paris, France Member : Mark James Federal Aviation Administration Kansas City, MO Member : Brenda Pitts Federal Aviation Administration Garden City, NJ 1 All times are reported in eastern standard time unless otherwise noted. 2 Not all group members were present for all activities. 1 Member : John Shelden Federal Aviation Administration Renton, WA Member : Bob Hemphill US Airways, Inc. Phoenix, AZ III. SUMMARY On January 15, 2009, about 1527 eastern standard time (EST), US Airways flight 1549, an Airbus A320-214, registration N106US, suffered bird ingestion into both engines, lost engine thrust, and landed in the Hudson River following take off from New York City's LaGuardia Airport (LGA). The scheduled, domestic passenger flight, operated under the provisions of Title 14 CFR Part 121, was en route to Charlotte Douglas International Airport (CLT) in Charlotte, North Carolina. The 150 passengers and 5 crewmembers evacuated the airplane successfully. One flight attendant and four passengers were seriously injured.
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  • A Study of Transport Airplane Crash Resistant
    DOT/FAA/AR-01/76 A Study of Helicopter Crash- Office of Aviation Research Washington, D.C. 20591 Resistant Fuel Systems February 2002 Final Report This document is available to the U.S. public through the National Technical Information Service (NTIS), Springfield, Virginia 22161. U.S. Department of Transportation Federal Aviation Administration NOTICE This document is disseminated under the sponsorship of the U.S. Department of Transportation in the interest of information exchange. The United States Government assumes no liability for the contents or use thereof. The United States Government does not endorse products or manufacturers. Trade or manufacturer's names appear herein solely because they are considered essential to the objective of this report. This document does not constitute FAA certification policy. Consult your local FAA aircraft certification office as to its use. This report is available at the Federal Aviation Administration William J. Hughes Technical Center's Full-Text Technical Reports page: actlibrary.tc.faa.gov in Adobe Acrobat portable document format (PDF). Technical Report Documentation Page 1. Report No. 2. Government Accession No. 3. Recipient's Catalog No. DOT/FAA/AR-01/76 4. Title and Subtitle 5. Report Date A STUDY OF HELICOPTER CRASH-RESISTANT FUEL SYSTEMS February 2002 6. Performing Organization Code 7. Author(s) 8. Performing Organization Report No. S.H. Robertson, N.B. Johnson, D.S. Hall and I.J. Rimson RA-FAA-01-130 9. Performing Organization Name and Address 10. Work Unit No. (TRAIS) Robertson Aviation, L.L.C. 1024 East Vista Del Cerro Drive Tempe, AZ 85281 11. Contract or Grant No.
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  • Airframe & Aircraft Components By
    Airframe & Aircraft Components (According to the Syllabus Prescribed by Director General of Civil Aviation, Govt. of India) FIRST EDITION AIRFRAME & AIRCRAFT COMPONENTS Prepared by L.N.V.M. Society Group of Institutes * School of Aeronautics ( Approved by Director General of Civil Aviation, Govt. of India) * School of Engineering & Technology ( Approved by Director General of Civil Aviation, Govt. of India) Compiled by Sheo Singh Published By L.N.V.M. Society Group of Institutes H-974, Palam Extn., Part-1, Sec-7, Dwarka, New Delhi-77 Published By L.N.V.M. Society Group of Institutes, Palam Extn., Part-1, Sec.-7, Dwarka, New Delhi - 77 First Edition 2007 All rights reserved; no part of this publication may be reproduced, stored in a retrieval system or transmitted in any form or by any means, electronic, mechanical, photocopying, recording or otherwise, without the prior written permission of the publishers. Type Setting Sushma Cover Designed by Abdul Aziz Printed at Graphic Syndicate, Naraina, New Delhi. Dedicated To Shri Laxmi Narain Verma [ Who Lived An Honest Life ] Preface This book is intended as an introductory text on “Airframe and Aircraft Components” which is an essential part of General Engineering and Maintenance Practices of DGCA license examination, BAMEL, Paper-II. It is intended that this book will provide basic information on principle, fundamentals and technical procedures in the subject matter areas relating to the “Airframe and Aircraft Components”. The written text is supplemented with large number of suitable diagrams for reinforcing the key aspects. I acknowledge with thanks the contribution of the faculty and staff of L.N.V.M.
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  • Structural Certification of the F-16 Block 52+ Aircraft 29 November 2005 2005 USAF Aircraft Structural Integrity Program Conference
    Structural Certification of the F-16 Block 52+ Aircraft 29 November 2005 2005 USAF Aircraft Structural Integrity Program Conference Robert J. Burt Director and Deputy F-35 Structural Development and Integrity Lockheed Martin Aeronautics Company Fort Worth © 2005 LOCKHEED MARTIN CORPORATION Lockheed Martin Aeronautics Company Structural Certification of the F-16 Block 52+ Aircraft Abstract This presentation will describe in some detail the process followed by Lockheed Martin Aeronautics – Fort Worth for the structural certification of the new production F-16 Block 52+ aircraft for foreign military sales (FMS). The F-16 Block 52+ aircraft are structurally upgraded from the USAF Block 50/52 aircraft due to carriage of the fuselage shoulder mounted conformal fuel tanks and due to the addition of numerous advanced systems. The structural requirements and their methods of verification are set forth in the program contract and subsequent program documents such as the weapon system specification and air vehicle specification. Every USAF and FMS F-16 has an Aircraft Structural Integrity Program (ASIP) based upon program contractual requirement and tailored to MIL-STD-1530B Aircraft Structural Integrity Program. An ASIP Master Plan has been written for the Block 52+ aircraft which has been coordinated with and approved by the USAF F-16 System Group. This ASIP Master Plan states in specific terms how all the tasking outlined in the “five pillars” is accomplished. An overall design process will be discussed in depth pointing out how all historical structural analysis, structural test and field information has been used in the structural design of the Block 52+ aircraft.
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  • Bombardier Global Express - Fuel System
    Bombardier Global Express - Fuel System INTRODUCTION This chapter describes the fuel system for the Global Express aircraft. Fuel is contained in a wet wing box structure, which is sealed to form the three main separate wing tanks, and a smaller quantity of fuel is carried in a separate aft fuselage tank. The tanks are vented to atmosphere and slightly pressurized by an air scoop located on the lower surface of each wing. A scavenge pump purges fuel from the vent lines and a climb vent, located in each main wing tank, provides ventilation when the airplane is in a nose up attitude. Each engine is supplied with fuel from its respective feed tank which contains two alternating current or AC primary pumps, and one Direct Current (DC) backup (or Aux) electrical boost pump. The transfer system maintains the feed tanks full during all attitudes, and provides automatic transfer of fuel from the center tank and aft tank to the main wing tanks. Lateral balance between left and right main tanks is controlled automatically by the Fuel Management and Quantity Gauging Computer (FMQGC), or manually through switch selections in the flight compartment. Page 1 Bombardier Global Express - Fuel System Feed Tanks DC Pumps (start, emergency and wing transfer) AC Motor Pumps* (transfer) AC Motor Pumps (transfer) GX_11_001 AFT Tank* Center Tank Engine Driven Pumps AC Motor Pumps (engine feed) Main Wing Tank Note *Not on Global 5000 Flight deck control is provided on the overhead panel, and fuel quantity and warnings are displayed on EICAS. A single point pressure refuel/defuel adapter is provided which is connected to a manifold containing shutoff valves.
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  • Airplane Flying Handbook (FAA-H-8083-3B) Chapter 2
    Chapter 2 Ground Operations Introduction All pilots must ensure that they place a strong emphasis on ground operations as this is where safe flight begins and ends. At no time should a pilot hastily consider ground operations without proper and effective thoroughness. This phase of flight provides the first opportunity for a pilot to safely assess the various factors of flight operations including the regulatory requirements, an evaluation of the airplane’s condition, and the pilot’s readiness for their pilot in command (PIC) responsibilities. 2-1 Flying an airplane presents many new responsibilities that are not required for other forms of transportation. Focus is often overly placed on the flying portion itself with less emphasis placed on ground operations; it must be stressed that a pilot should allow themselves adequate time to properly prepare for flight and maintain effective situational awareness at all times until the airplane is safely and securely returned to its tie-down or hangar. This chapter covers the essential elements for the regulatory basis of flight including an airplane’s airworthiness requirements, important inspection items when conducting a Figure 2-2. A visual inspection of the aircraft before flight is an preflight visual inspection, managing risk and resources, and important step in mitigating airplane flight hazards. proper and effective airplane surface movements including the use of the Airplane Flight Manual/Pilot’s Operating Handbook (AFM/POH) and airplane checklists. be kept accurate and secure but available for inspection. Airplane logbooks are not required, nor is it advisable, to be Preflight Assessment of the Aircraft kept in the airplane.
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  • FAA Safety Briefing January/February 2020 Volume 60/Number 1
    November/DecemberJanuary/February 2020 2019 Know Your Aircraft Federal Aviation 8 NoA VerySurprises Long Title for One of the20 FeatureThe Wing’s Title24 Give of One Me Feature a Brake ... Administration 10KeepingStories Control Could Possiblyof Go in thisthe SpaceThing 16 Storyand Maybe Goes Here a Tire and a Avionics and Automation Strut TooJanuary / February 2020 1 ABOUT THIS ISSUE ... U.S. Department of Transportation Federal Aviation Administration ISSN: 1057-9648 FAA Safety Briefing January/February 2020 Volume 60/Number 1 Elaine L. Chao Secretary of Transportation The January/February 2020 issue of FAA Safety Steve Dickson Administrator Briefing focuses on how to better “Know Your Aircraft.” Ali Bahrami Associate Administrator for Aviation Safety Feature articles cover each major section of an Executive Director, Flight Standards Service Rick Domingo aircraft, highlighting the many design, performance Editor Susan Parson and structural variations you’ll likely see and how Tom Hoffmann Managing Editor they affect your flying. We’ll also take a fresh look at James Williams Associate Editor / Photo Editor Jennifer Caron Copy Editor / Quality Assurance Lead understanding aircraft energy management. Paul Cianciolo Associate Editor / Social Media John Mitrione Art Director Published six times a year, FAA Safety Briefing, formerly Contact information FAA Aviation News, promotes aviation safety by discussing current The magazine is available on the internet at: technical, regulatory, and procedural aspects affecting the safe www.faa.gov/news/safety_briefing operation and maintenance of aircraft. Although based on current FAA policy and rule interpretations, all material is advisory or Comments or questions should be directed to the staff by: informational in nature and should not be construed to have • Emailing: [email protected] regulatory effect.
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  • February 2019 $10.00
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