DOCSLIB.ORG

AC 00-2.13 Appendix 3

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
AC 00-2.13 Appendix 3 6/15/00 AC 00-2.13 Appendix 3 APPENDIX 3 NUMERICAL LIST OF ADVISORY CIRCULARS Important Notice This Advisory Circular Checklist, AC 00-2, is no longer sent automatically to addresses on free advisory circular mailing lists. Persons not now receiving AC 00-2 but who wish to receive it must specifically request to be placed on the AC 00-2 mailing list (see par. 5 for ordering information). Up to ten copies may be sent to any one address. Persons receiving this edition of AC 00-2 need not request AC 00-2 mailing list service as they have already been transferred to the new list. Q 00-7D (9/20/82) (ANN-130) General State and Regional Disaster Airlift Informs the aviation community of the (SARDA) Planning establishment and content of the United (9/15/98) (ADA-20) States (US). National Aviation Standard for Subject No. 00 Provides officials with guidance to access the Very High Frequency Omnidirectional and utilize a broad range of aviation Radio Range (VOR)/Distance Measuring 00-1.1 resources within the state, when needed to Equipment(DME)/Tactical Air Navigation Government Aircraft Operations support civil emergency operations. (TACAN) Systems. (4/19/95) (AFS -220) Provides guidance on whether particular 00-24B 00-33B government aircraft operations are public Thunderstorms Nickel-Cadmium Battery Operational, aircraft or civil aircraft operations under the (1/20/83) (AFS -400) Maintenance, and Overhaul Practices new statutory definition of “public Describes the hazards of thunderstorms to (7/9/97) (AFS -400) aircraft.” This AC contains FAA’s intended aviation and offers guidance to help prevent Provides guidelines for more reliable nickel- application of key terms in the new accidents caused by thunderstorms. cadmium battery operation through proper statutory definition . For operations that operational and maintenance practices, and have lost public aircraft status under the 00-25 has been reissued to include reconditioning new law, information is provided on Forming and Operating a Flying Club information. bringing those operations into compliance (3/24/69) (AFS -800) with FAA safety regulations for civil Provides preliminary information that will 00-34A aircraft and provides information on assist anyone or any group of people Aircraft Ground Handling and Servicing applying for an exemption. interested in forming and operating a flying (7/29/74) (AFS -340) club. Contains information and guidance for the Q 00-2.13 servicing and ground handling of aircraft. Advisory Circular Checklist 00-30B (6/15/00) (APF-100) Atmospheric Turbulence Avoidance 00-41B Transmits the revised checklist of current 9/9/97 (AFS -400) FAA Quality Control System FAA advisory circulars as of Describes to pilots, aircrew members, Certification Program June 15, 2000. dispatchers, and other operations personnel (10/10/89) (ASU-430) the various types of clear air turbulence Describes the Federal Aviation 00-6A (CAT) and some of the weather patterns Administration (FAA) Quality Control Aviation Weather associated with it. Also included are “Rules System Certification Program and the (3/3/75) (AFS -400) of Thumb” for avoiding or minimizing CAT mechanics of implementation. It is intended Provides an up-to-date and expanded text encounters. for guidance and information only. for pilots and other flight operations personnel whose interest in meteorology is 00-31A 00-44II primarily in its application to flying. United States (US). National Aviation Status of the Federal Aviation SN 050- 007-00283-1. Standard for the VOR/DME/TAC Regulations $8.50 Supt. Docs. Systems (4/97) (AGC-200) A3-1 AC 00-2.13 6/15/00 Appendix 3 This circular sets forth the current Describes a system for the voluntary helicopters and tiltrotor aircraft into publication status of Federal Aviation accreditation of civil aircraft parts disaster relief planning efforts. Regulations (FARs), any Changes issued to distributors on the basis of voluntary date, and provides a price list, and ordering industry oversight and provides information Q 00-60 instructions. that may be used for developing North American Free Trade Agreement accreditation programs. The FAA believes and Specialty AIR Services Operations 00-45D such programs will assist in alleviating lack (11/9/99) AFS -805) Aviation Weather Services of documentation and will improve Provides information for aircraft operators (2/7/95) (AFS -400) traceability. from the United States who plan to conduct Supplements AC 00-6A, Aviation Weather, specialty air services (SAS) operations in in that it explains the weather service in 00-57 Canada or Mexico in accordance with the general and the use and interpretation of Hazardous Mountain Winds and Their North American Free Trade Agreement. It reports, forecasts, weather maps, and Visual Indicators (9/10/97) (AND-720) also provides information for aircraft prognostic charts in detail. Assists pilots involved in aviation operators from Canada or Mexico who plan SN 050-007-01082-6 operations to diagnose the potential for to conduct SAS operations in the U.S. $12.00 Supt. Docs. severe wind events in the vicinity of SN 050-007-01281-1 mountainous areas. It provides information $2.50 Supt. Docs. 00-46D on preflight planning techniques and on in- Aviation Safety Reporting Program flight evaluation strategies for avoiding (2/26/97) (ASY-300) destructive turbulence and loss of aircraft Procedural Describes the Federal Aviation control. Pilots, dispatchers, air traffic Administration’s Aviation Safety Reporting controllers, and other who must deal with Subject No. 10 program which utilizes the National weather phenomena and the routing of Aeronautics and Space Administration aircraft will benefit from the information 11-2A (NASA) as a third party to receive and contained in this advisory circular. Notice of Proposed Rulemaking analyze Aviation Safety Reports. This Distribution System cooperative safety reporting program 00-58 (7/26/84) (ABC-100) invites users of the National Aviation Voluntary Disclosure Reporting Provides the public with information System to report to NASA actual or Program (5/4/98) (AFS -350) relative to participation in the FAA potential discrepancies and deficiencies Replaces AC 120-56. Provides information rulemaking process and explains the involving the safety of aviation operations. and guidance that may be used by certificate availability of the Notices. holders, production approval holders, 00-54 indirect air carriers, and foreign air carriers 13-1 Pilot Windshear Guide disclosing apparent violations to the FAA Aviation Safety Inspector Work Site (11/25/88) (AFS -200) of regulations in 14 CFR parts 21, 107, 108, Access Communicates key windshear information 109, 121, 125, 129 (security program (12/28/95) (AFS -120/AFS -300) relevant to flightcrews. Appendix 1 of this violations only), 133, 135, 137, 141, 142, Explains the requirement and use of FAA advisory circular is the Pilot Windshear 145, & 147 under the self-disclosure Form 8000-39, Aviation Safety Inspector Guide, which is only one section of the program. The procedures outlined in this Identification Card, and its relation to the two-volume Windshear Training Aid. AC can be applied to all of the above. The Aviation Safety Credential, FAA Form procedures and practices outlined in this 110A. This AC is issued primarily to 00-55 AC cannot be applied to those who are acquaint airport authorities and the airport Announcement of availability: FAA required to report failures, malfunctions and security personnel with the FAA Form Order 8130.21A, Procedures for defects under 14 CFR part 21.3 and do not 8000-39 and the aviation safety inspector’s Completion and Use of FAA Form 8130, make those reports in the timeframe need to be in restricted areas of the airport Airworthiness Approval Tag required by the regulation. to perform official FAA business. (1/19/94) (AIR-200) Announces availability of subject order. Q 00-59 Integrating Helicopter and Tiltrotor Aircraft 00-56 Assets Into Disaster Relief Planning Voluntary Industry Distributor (11/98) (AND-710) Subject No. 20 Accreditation Program Provides guidance to state and local (9/5/96) (AFS -350) emergency relief planners on integrating 20-18A A3-2 6/15/00 AC 00-2.13 Appendix 3 Qualification Testing of Turbo-jet from faulty engine exhaust systems or cabin Outlines acceptable methods, but not the Engine Thrust Reversers heaters of the exhaust gas heat exchanger only methods, for measuring cabin interior (3/16/66) (ANE- 100) type. emergency illumination on transport Discusses the requirements for the airplanes, and provides information as to qualification of thrust reversers and sets 20-33B suitable measuring instruments. forth an acceptable means of compliance Technical Information Regarding Civil with the tests prescribed in Federal Aeronautics Manuals 1, 3, 4a,4b, 5, 6, 7, 20-40 Aviation Regulations, Part 33, then run 8, 9, 13 and 14 Placards for Battery-Excited Alternators under nonstandard ambient air conditions. (5/1/75) (AIR-100) Installed in Light Aircraft Advises the public that policy information (8/11/65) (ACE-100) 20-24B contained in the subject Civil Aeronautics Sets forth an acceptable means of Qualification of Fuels, Lubricants, and Manuals may be used in conjunction with complying with placarding rules in Federal Additives specific sections of the Federal Aviation Aviation Regulations 23 and 27 with (12/20/85) (ANE-110) Regulations. respect to battery excited alternator Provides acceptable procedures for installations. approving the qualification of fuels, 20-34D lubricants, and additives for use in Prevention of Retractable Landing Gear 20-41A certificated aircraft engines. Failures Substitute Technical Standard Order (8/8/80) (AFS -340) (TSO) Aircraft Equipment 20-27D Updates statistical information related to (4/5/77) (AIR- 120) Certification and Operation of landing accidents involving aircraft with Sets forth an acceptable means for Amateur-Built Aircraft retractable landing gear and suggests complying with rules governing aircraft (6/22/90) (AIR-230) procedures to minimize those accidents.
Load more

Recommended publications
  • Airport Rules and Regulations, Rev
    AIRPORT RULES and REGULATIONS AVI-POL-506 – DAL Airport Rules and Regulations, Rev. 2 (10/15/17) PURPOSE: The purpose of this manual is to publish Rules and Regulations for airport- approved operating procedures, terminal, safety and security requirements at in affect at Dallas Love Field. Nothing in these Rules and Regulations shall limit or constrain the legitimate authority of the Airport Director or designee. SCOPE: Dallas Love Field is owned and operated by the City of Dallas, Texas. These Airport Rules and Regulations apply to all airport employees (including City staff), tenant organizations, airlines and governmental organizations that work at, conduct business at, lease property, or otherwise have access to Dallas Love Field. They are put in place, to ensure that employees performing their jobs contribute to the Dallas Love Field goal of providing a safe and efficient airport. Chapter 5, of the Dallas City Code contains current City of Dallas Ordinances pertaining to Aircraft and Airports. Only the pertinent portions of the Chapter are included in these Rules and Regulations. AVI-POL-506 – DAL Airport Rules and Regulations Rev 2 - 10/15/17 Page ii Rules of Interpretation and Construction Wherever these Rules and Regulations refer to “applicable law,” such term shall refer to all present and future federal, state and local statutes, ordinances and regulations and City ordinances applicable to the Person or the Airport or the use thereof and judicial or administrative interpretations thereof, as amended from time to time, including but not limited to Transportation Security Regulations and Security Directives issued from time to time by DHS or TSA, Federal Regulations and Advisory Circulars issued from time to time by the FAA, these Rules and Regulations, Notices to Airmen (“NOTAMs”) and Airport Directives issued by the Department of Aviation from time to time and directions issued by the Air Traffic Control Tower.
    [Show full text]
  • Low Temperature Environment Operations of Turboengines
    0 Qo B n Y n 1c AGARD 2 ADVISORY GROUP FOR AEROSPACE RESEARCH & DEVELOPMENT 3 7 RUE ANCELLE 92200 NEUILLY SUR SEINE FRANCE AGARD CONFERENCE PROCEEDINGS 480 Low Temperature Environment Operations of Turboengines (Design and User's Problems) Fonctionnement des Turborkacteurs en Environnement Basse Tempkrature (Problkmes Pos& aux Concepteurs et aux Utilisateurs) processed I /by 'IMs ..................signed-...............date .............. NOT FOR DESTRUCTION - NORTH ATLANTIC TREATY ORGANIZATION I Distribution and Availability on Back Cover AGARD-CP-480 --I- ADVISORY GROUP FOR AEROSPACE RESEARCH & DEVELOPMENT 7 RUE ANCELLE 92200 NEUILLY SUR SEINE FRANCE AGARD CONFERENCE PROCEEDINGS 480 Low Temperature Environment Operations of Turboengines (Design and User's Problems) Fonctionnement des TurborLacteurs en Environnement Basse Tempkrature (Problkmes PoSes aux Concepteurs et aux Utilisateurs) Papers presented at the Propulsion and Energetics Panel 76th Symposium held in Brussels, Belgium, 8th-12th October 1990. - North Atlantic Treaty Organization --q Organisation du Traite de I'Atlantique Nord I The Mission of AGARD According to its Chartcr, the mission of AGARD is to bring together the leading personalities of the NATO nations in the fields of science and technology relating to aerospace for the following purposes: -Recommending effective ways for the member nations to use their research and development capabilities for the common benefit of the NATO community; - Providing scientific and technical advice and assistance to the Military Committee
    [Show full text]
  • AIRCRAFT SYSTEMS COURSE FILE III B. Tech II Semester
    ERONAUTICAL ENGINEERING MRCET (UGC Autonomous) – – AIRCRAFT SYSTEMS COURSE FILE III B. Tech II Semester (2017-2018) Prepared By Ms. L Sushma, Assoc. Prof Department of Aeronautical Engineering MALLA REDDY COLLEGE OF ENGINEERING & TECHNOLOGY (Autonomous Institution – UGC, Govt. of India) Affiliated to JNTU, Hyderabad, Approved by AICTE - Accredited by NBA & NAAC – A Grade - ISO 9001:2015 Certified) Maisammaguda, Dhulapally (Post Via. Kompally), Secunderabad – 500100, Telangana State, India. III– II B. Tech Aircraft Systems By L SUSHMA I AERONAUTICAL ENGINEERING MRCET (UGC Autonomous) – – MRCET VISION ฀ To become a model institution in the fields of Engineering, Technology and Management. ฀ To have a perfect synchronization of the ideologies of MRCET with challenging demands of International Pioneering Organizations. MRCET MISSION To establish a pedestal for the integral innovation, team spirit, originality and competence in the students, expose them to face the global challenges and become pioneers of Indian vision of modern society. MRCET QUALITY POLICY. ฀ To pursue continual improvement of teaching learning process of Undergraduate and Post Graduate programs in Engineering & Management vigorously. ฀ To provide state of art infrastructure and expertise to impart the quality education. III– II B. Tech Aircraft Systems By L SUSHMA II AERONAUTICAL ENGINEERING MRCET (UGC Autonomous) – – PROGRAM OUTCOMES (PO’s) Engineering Graduates will be able to: 1. Engineering knowledge: Apply the knowledge of mathematics, science, engineering fundamentals,
    [Show full text]
  • Small Gas Turbines Chapter 2 Fuel Systems
    Chapter 2 Fuel Systems A complex part of a typical small gas turbine is the fuel system. Small gas turbines in a similar way to much larger units make high demands on the fuel systems. A typical fuel system is required to start and accelerate the engine, govern or control the engine at one or more running speeds, maintain a given speed under load conditions and in many designs, the engine must be protected against excessive exhaust gas temperatures and compressor surging. All small gas turbines are designed to operate on Jet fuel such as Jet A, Jet A1 and JP4, these fuels are similar to Kerosene. Paraffin is a type of kerosene, as is 28 second heating oil and gas oil. Small engines will run satisfactorily on any of these fuels, tolerance of differing fuels is one of the advantages of the gas turbine engine. As the combustion process is continuous and takes place at constant pressure, there are no problems with detonation or pinking. Detonation or pinking which is associated with piston engines significantly limits their performance. Certain designs of gas turbine intended for specialist stationary applications may be operated on natural gas. Many small engines may be operated on Diesel fuel or Petrol (Gasoline), the basic performance of the engine will be unaffected but prolonged use is not recommended for a number of reasons. Diesel fuel contains sulfur that may deposit itself on components in the fuel system. Certain fuel pump components are often silver-plated which will be damaged by the sulfur content in the fuel.
    [Show full text]
  • Aviation Rulemaking Advisory Committee
    Aviation Rulemaking Advisory Committee Airman Certification System Working Group Interim Recommendation Report August 8, 2018 August 8, 2018 Yvette A. Rose Chair, Aviation Rulemaking Advisory Committee Federal Aviation Administration 800 Independence Avenue, SW Washington, DC 20591 Dear Ms. Rose, On behalf of the Airman Certification System Working Group (ACSWG), we submit the following interim recommendation report to the Aviation Rulemaking Advisory Committee (ARAC) for consideration and implementation. The FAA and the aviation industry have continued its collaborative effort to improve airman training and testing by establishing an integrated, holistic airman certification system that clearly aligns testing with the certification standards, guidance, and reference materials, and maintains that alignment. As part of its ongoing effort, the ACSWG is presenting feedback on draft standards for the Private Pilot Rotorcraft Pilot Helicopter and Instrument Rating – Powered-Lift. Additionally, we have included recommendations on the Aviation Instructor Handbook (FAA-H-8083-9B) and the Helicopter Flying Handbook (FAA-H-8083-21B). Collectively, we recommend and endorse the committee’s transmittal of the working group recommendations to the FAA for further review, incorporation, and execution. We are confident that, by doing so, the safety of aviation will continue to markedly improve. Sincerely, David Oord Susan Parson Eric Crump ARAC Vice-Chair & ACSWG Chair FAA Representative ACSWG Subgroup Lead Senior Director, Regulatory Affairs Flight Standards Service Federal Aerospace Program Director Aircraft Owners and Pilots Association Aviation Administration Polk State College Janeen Kochan, PhD, FRAeS, John “Mac” McWhinney Jackie Spanitz AMT ACS Subgroup Co-chair ACSWG Subgroup Lead ACSWG Subgroup Lead General Human Factors Scientist/Designated Pilot Examiner/ Senior Course Developer Manager Instructor Pilot King Schools, Inc.
    [Show full text]
  • Dept. of Aerospace Engineering
    DEPT. OF AEROSPACE ENGINEERING LIST OF NEW COURSES S.No Code No. Name of the Course L T P Credits Navigation, Guidance and Control of Aerospace 1 18AE2025 3 0 0 3 Vehicles 2 18AE2026 Aircraft Instrumentation & Avionics Laboratory 0 0 3 1.5 3 18AE2027 Heat and Mass Transfer 3 0 0 3 4 18AE2028 Computational Fluid Dynamics 3 0 0 3 5 18AE2029 Computational Fluid Dynamics Laboratory 0 0 2 1 6 18AE2030 Wind tunnel Techniques 3 0 0 3 7 18AE2031 Helicopter Aerodynamics 3 0 0 3 8 18AE2032 Finite Element Analysis 3 0 0 3 9 18AE2033 Finite Element Analysis Laboratory 0 0 2 1 10 18AE2034 Theory of Elasticity 3 0 0 3 11 18AE2035 Design and Analysis of Composite Structures 3 0 0 3 12 18AE2036 Introduction to Non Destructive Testing 3 0 0 3 13 18AE2037 Structural Vibration 3 0 0 3 14 18AE2038 Aeroelasticity 3 0 0 3 15 18AE2039 Cryogenic Propulsion 3 0 0 3 16 18AE2040 Rocket and Missiles 3 0 0 3 17 18AE2041 Advanced Space Dynamics 3 0 0 3 18 18AE2042 Air Traffic Control and Aerodrome Details 3 0 0 3 19 18AE2043 Aircraft Systems 3 0 0 3 20 18AE2044 Basics of Acoustics 3 0 0 3 21 18AE2045 Basics of Aerospace Engineering 3 0 0 3 22 18AE3001 Advanced Aerodynamics 3 0 0 3 23 18AE3002 Advanced Aerodynamics Laboratory 0 0 2 1 24 18AE3003 Aerospace Propulsion 3 0 0 3 25 18AE3004 Aero Propulsion Laboratory 0 0 2 1 26 18AE3005 Orbital Space Dynamics 3 0 0 3 27 18AE3006 Flight Mechanics 3 1 0 4 28 18AE3007 Aerospace Structural Analysis 3 0 0 3 29 18AE3008 Aerospace Structural Analysis Laboratory 0 0 2 1 30 18AE3009 Flight Control Systems 3 0 0 3 31 18AE3010 Flight
    [Show full text]
  • Human Factors Considerations of UAS Procedures and Control Stations: Tasks PC-1 Through PC-3 Pilot and Crew (PC) Subtask
    THIRD PARTY RESEARCH. PENDING FAA REVIEW. DOT/FAA/AR-xx/xx Federal Aviation Administration William J. Hughes Technical Center Aviation Research Division Atlantic City International Airport New Jersey 08405 A10 – Human Factors Considerations of UAS Procedures and Control Stations: Tasks PC-1 through PC-3 Pilot and Crew (PC) subtask Recommended Requirements and Operational Procedures August 30,2017 Final Report This document is available to the U.S. public through the National Technical Information Services (NTIS), Springfield, Virginia 22161. This document is also available from the Federal Aviation Administration William J. Hughes Technical Center at actlibrary.tc.faa.gov. U.S. Department of Transportation Federal Aviation Administration THIRD PARTY RESEARCH. PENDING FAA REVIEW. NOTICE This document is disseminated under the sponsorship of the U.S. Department of Transportation in the interest of information exchange. The U.S. Government assumes no liability for the contents or use thereof. The U.S. Government does not endorse products or manufacturers. Trade or manufacturers’ names appear herein solely because they are considered essential to the objective of this report. The findings and conclusions in this report are those of the author(s) and do not necessarily represent the views of the funding agency. This document does not constitute FAA policy. Consult the FAA sponsoring organization listed on the Technical Documentation page 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). THIRD PARTY RESEARCH. PENDING FAA REVIEW. Legal Disclaimer: The information provided herein may include content supplied by third parties.
    [Show full text]
  • Powerplant Curriculum Practical Project Record
    DEPARTMENT OF EDUCATION PUERTO RICO AVIATION MAINTENANCE INSTITUTE AVIATION MAINTENANCE TECHNICIAN COURSE FAA Approved # DN9T092R POWERPLANT COURSE CURRICULUM VOLUME 4 Revision 1 – June 07, 2019 Exclusive Property Government of Puerto Rico Department of Education Occupational and Technical Education Program DEPARTMENT OF EDUCATION PUERTO RICO AVIATION MAINTENANCE INSTITUTE AVIATION MAINTENANCE TECHNICIAN COURSE FAA Approved # DN9T092R POWERPLANT COURSE CURRICULUM MANUAL RESTRICTED DATA This data, furnished in connection with the request of the Federal Aviation Administration for the operation of Aviation Maintenance Technician Course in Puerto Rico Aviation Maintenance Institute, shall not be disclosed outside the Puerto Rico Department of Education, and shall not be duplicated, used on disclosed in whole or in part for any purpose other than to evaluate the course; provided that if is awarded to this office as result of or in connection with the submission of this data, the Government of Puerto Rico shall have the right to disclose the data the extent provided in contract between both agencies. Exclusive Property Volume : 4 Government of Puerto Rico Page No. : I Department of Education Rev. Num. : 1 Occupational and Technical Education Program Date : June 07, 2019 DEPARTMENT OF EDUCATION PUERTO RICO AVIATION MAINTENANCE INSTITUTE AVIATION MAINTENANCE TECHNICIAN COURSE FAA Approved # DN9T092R POWERPLANT COURSE CURRICULUM MANUAL 1 LIST OF EFFECTIVE PAGES 2 LOG OF REVISION 3 TABLE OF CONTENTS 4 POWERPLANT SCOPE 5 SCHEDULE OF REQUIRED TESTS 6 GLOSSARY OF TERMS AND DEFINITIONS 7 TEXTBOOKS REQUIRED BY THE STUDENTS 8 CURRICULUM REQUIREMENTS 9 POWERPLANT CURRICULUM SUBJECTS Exclusive Property Volume : 4 Government of Puerto Rico Page No. : II Department of Education Rev.
    [Show full text]
  • Ground Handling Accident Involving Cessna 172RG, VH-MKG, Parafield
    InsertGround document handling accident title involving Cessna 172RG, VH-MKG LocationParafield | DateAirport, South Australia | 11 September 2016 ATSB Transport Safety Report Investigation [InsertAviation Mode] Occurrence Occurrence Investigation Investigation XX-YYYY-####AO -2016 -115 Final – 24 February 2017 Cover photo: Richard Woods Released in accordance with section 25 of the Transport Safety Investigation Act 2003 Publishing information Published by: Australian Transport Safety Bureau Postal address: PO Box 967, Civic Square ACT 2608 Office: 62 Northbourne Avenue Canberra, Australian Capital Territory 2601 Telephone: 1800 020 616, from overseas +61 2 6257 4150 (24 hours) Accident and incident notification: 1800 011 034 (24 hours) Facsimile: 02 6247 3117, from overseas +61 2 6247 3117 Email: [email protected] Internet: www.atsb.gov.au © Commonwealth of Australia 2017 Pilotship of intellectual property rights in this publication Unless otherwise noted, copyright (and any other intellectual property rights, if any) in this publication is owned by the Commonwealth of Australia. Creative Commons licence With the exception of the Coat of Arms, ATSB logo, and photos and graphics in which a third party holds copyright, this publication is licensed under a Creative Commons Attribution 3.0 Australia licence. Creative Commons Attribution 3.0 Australia Licence is a standard form license agreement that allows you to copy, distribute, transmit and adapt this publication provided that you attribute the work. The ATSB’s preference is that you attribute this publication (and any material sourced from it) using the following wording: Source: Australian Transport Safety Bureau Copyright in material obtained from other agencies, private individuals or organisations, belongs to those agencies, individuals or organisations.
    [Show full text]
  • Hobart Jetex® 7D Cummins 4BT Diesel (Tier 4I)
    Hobart JetEx® 7D Cummins 4BT Diesel (Tier 4i) EPA TIER 4i / CARB TIER 4i EU STAGE III B Low emissions compliant Performance Features: • Delay stop (for turbo protection) and emergency • Low emission certified engine (Tier 4i) shutdown • Lift-off doors and removable panels provide complete • Reliable, Hobart manufactured AC rectified generator access to engine, generator and control compartments with automatic voltage build-up • Stainless steel fuel tank • Hand activated breaking system • Capable of 12 turboprop aircraft starts on a single gallon • Precise voltage regulation of fuel • Adjustable current limit for safe starting of any DC aircraft • 12 to over 30 hours of operation between refueling • Low noise design (less than 80 dBA) depending on usage • 30 ft. (9 m) DC output cable • Low fuel warning and shutdown HOBART is part of ITW GSE – the world’s leading supplier of Ground Support Equipment It’s all about connections ITW GSE - HOBART 11001 US Highway 41 North Palmetto, FL 34221 U.S.A. Phone (toll free in US): 800-899-1841 Phone (international): +1-941-721-1000 Fax: +1-941-721-1087 Specifications Email: [email protected] Web: www.itwgse.com Hobart JetEx® 7D Engine • Engine start switch • Cummins 4BT 3.3 diesel operating at 1800 RPM (69HP) • Air cleaner restriction indicator 325 August 2014 • 4-stroke, 4 cylinder, diesel turbo-charged engine • Emergency Stop Button • Full application approval by Cummins • Engine idle/run switch • Low oil pressure shutdown, high water temperature shutdown, • Engine “ON” light and high speed limiting
    [Show full text]
  • Aircraft Systems.Pdf
    AERONAUTICAL ENGINEERING MRCET (UGC Autonomous) AIRCRAFT SYSTEMS COURSE FILE IV yr B.Tech I Sem (2019-2020) Prepared By Mr. Sachin Srivastava, Assist. Prof Department of Aeronautical Engineering MALLA REDDY COLLEGE OF ENGINEERING & TECHNOLOGY (Autonomous Institution UGC, Govt. of India) Affiliated to JNTU, Hyderabad, Approved by AICTE Accredited by NBA & NAAC, A Grade – ISO9001:2015Certified) Maisammaguda, Dhulapally (Post Via. Kompally), Secunderabad 500100, Telangana State, India. IV I B. Tech Aircraft Systems by Sachin Srivastava I AERONAUTICAL ENGINEERING MRCET (UGC Autonomous) MRCET VISION To become a model institution in the fields of Engineering, Technology and Management. To have a perfect synchronization of the ideologies of MRCET with challenging demands of International Pioneering Organizations. MRCET MISSION To establish a pedestal for the integral innovation, team spirit, originality and competence in the students, expose them to face the global challenges and become pioneers of Indian vision of modern society. MRCET QUALITY POLICY To pursue continual improvement of teaching learning process of Undergraduate and Post Graduate programs in Engineering & Management vigorously. To provide state of art infrastructure and expertise to impart the quality education. IV I B. Tech Aircraft Systems by Sachin Srivastava II AERONAUTICAL ENGINEERING MRCET (UGC Autonomous) PROGRAM OUTCOMES (PO s) Engineering Graduates will be able to: 1. Engineering knowledge: Apply the knowledge of mathematics, science, engineering fundamentals, and an
    [Show full text]
  • CARTRIDGE STARTERS WORDS: JAMES KIGHTLY ARTWORK: IAN BOTT He Critical Elements for Six Shells Ready to Be Used
    With today’s convenient push-button starters, it is easy to forget that this facility was BRIEFING FILE AEROPLANE JULY 2019 hard-won — previously, many more challenging methods were used to get engines running Under the skin of aviation technology and tactics Starting with a bang The units in more detail Cylinder Barrel assembly Barrels Starter unit Indexing pins Return spring Operating Cam Engine Main spindle spindle gear link Piston Operating 5 Firing 8 Starting dog lever 4 mechanism Combustion Firing pin chamber 1 Helically splined Exhaust shaft 7 3 Cartridge valve Helically splined 9 The Hawker Typhoon’s cartridge sleeve starter is located at the top and Push rod Ensures rear of its Napier Sabre engine FDUWULGJHZRQōWƓUHXQOHVV 2 sealing piston is positioned It consists of two main Linking gear components to crankshaft How it works 11 10 connected by a 1. Pilot pulls a toggle, turning operating spindle 7. Charge pressure pushes the piston… combustion tube: 2. A cam on the spindle pulls sealing piston away from 8. …engaging starter dog with engine gear Five-cartridge barrel breech barrel via levers and… 9. As piston moves, helical splines on shaft and sleeve slide assembly Operated Push pawl 6 3. …the drag pawl rotates the barrel assembly over each other, turning starting dog and engine gear mechanically and Combustion tube Drag pawl electrically by the pilot 4. Pilot releases toggle, lever returns and push pawl 10. At stroke’s end, piston pushes on exhaust valve bolt, completes barrel rotation, aligning fresh cartridge opening the valve Combustion Starter unit Sealing piston levers and repositioning sealing piston 11.
    [Show full text]