AIN 2014 Product Support Survey
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Decision 2005/07/R
DECISION No 2005/07/R OF THE EXECUTIVE DIRECTOR OF THE AGENCY of 19-12-2005 amending Decision No 2003/19/RM of 28 November 2003 on acceptable means of compliance and guidance material to Commission Regulation (EC) No 2042/2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks THE EXECUTIVE DIRECTOR OF THE EUROPEAN AVIATION SAFETY AGENCY, Having regard to Regulation (EC) No 1592/2002 of 15 July 2002 on common rules in the field of civil aviation (hereinafter referred to as the Basic Regulation) and establishing a European Aviation Safety Agency1 (hereinafter referred to as the “Agency”), and in particular Articles 13 and 14 thereof. Having regard to the Commission Regulation (EC) No 2042/2003 of 28 November 2003 on the continuing airworthiness of aircraft and aeronautical products, parts and appliances, and on the approval of organisations and personnel involved in these tasks.2 Whereas: (1) Annex IV Acceptable Means of Compliance to Part- 66 Appendix 1 Aircraft type ratings for Part-66 aircraft maintenance licence (hereinafter referred to as Part-66 AMC Appendix I) is required to be up to date to serve as reference for the national aviation authorities. (2) To achieve this requirement the text of Part-66 AMC Appendix I should be amended regularly to add new aircraft type rating. (3) The regular amendment of Part-66 AMC Appendix I is considered as a permanent rulemaking task for the Agency. This decision represents the first update according to an accelerated procedure accepted by AGNA and SSCC. -
Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory figures As of Sept
Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2014. By Aaron M. U. Church, Associate Editor I 2015 USAF Almanac BOMBER AIRCRAFT flight controls actuate trailing edge surfaces that combine aileron, elevator, and rudder functions. New EHF satcom and high-speed computer upgrade B-1 Lancer recently entered full production. Both are part of the Defensive Management Brief: A long-range bomber capable of penetrating enemy defenses and System-Modernization (DMS-M). Efforts are underway to develop a new VLF delivering the largest weapon load of any aircraft in the inventory. receiver for alternative comms. Weapons integration includes the improved COMMENTARY GBU-57 Massive Ordnance Penetrator and JASSM-ER and future weapons The B-1A was initially proposed as replacement for the B-52, and four pro- such as GBU-53 SDB II, GBU-56 Laser JDAM, JDAM-5000, and LRSO. Flex- totypes were developed and tested in 1970s before program cancellation in ible Strike Package mods will feed GPS data to the weapons bays to allow 1977. The program was revived in 1981 as B-1B. The vastly upgraded aircraft weapons to be guided before release, to thwart jamming. It also will move added 74,000 lb of usable payload, improved radar, and reduced radar cross stores management to a new integrated processor. Phase 2 will allow nuclear section, but cut maximum speed to Mach 1.2. The B-1B first saw combat in and conventional weapons to be carried simultaneously to increase flexibility. Iraq during Desert Fox in December 1998. -
Rolls-Royce / Itp Regulation
EUROPEAN COMMISSION DG Competition Case M.8242 - ROLLS-ROYCE / ITP Only the English text is available and authentic. REGULATION (EC) No 139/2004 MERGER PROCEDURE Article 6(1)(b) in conjunction with Art 6(2) Date: 19/04/2017 In electronic form on the EUR-Lex website under document number 32017M8242 EUROPEAN COMMISSION Brussels, 19.04.2017 C(2017) 2613 final In the published version of this decision, some information has been omitted pursuant to Article PUBLIC VERSION 17(2) of Council Regulation (EC) No 139/2004 concerning non-disclosure of business secrets and other confidential information. The omissions are shown thus […]. Where possible the information omitted has been replaced by ranges of figures or a general description. To the notifying party: Subject: Case M.8242 – Rolls-Royce / ITP Commission decision pursuant to Article 6(1)(b) in conjunction with Article 6(2) of Council Regulation No 139/20041 and Article 57 of the Agreement on the European Economic Area2 Dear Sir or Madam, (1) On 24 February 2017, the European Commission received notification of a proposed concentration pursuant to Article 4 of the Merger Regulation by which the undertaking Rolls-Royce Holdings plc ("Rolls-Royce", United Kingdom) acquires within the meaning of Article 3(1)(b) of the Merger Regulation control of the whole of the undertaking Industria de Turbo Propulsores SA ("ITP", Spain) by way of a purchase of shares (the "Transaction").3 Rolls-Royce is designated hereinafter as the "Notifying Party", and Rolls-Royce and ITP are together referred to as the "Parties". 1 OJ L 24, 29.1.2004, p. -
Design of a Light Business Jet Family David C
Design of a Light Business Jet Family David C. Alman Andrew R. M. Hoeft Terry H. Ma AIAA : 498858 AIAA : 494351 AIAA : 820228 Cameron B. McMillan Jagadeesh Movva Christopher L. Rolince AIAA : 486025 AIAA : 738175 AIAA : 808866 I. Acknowledgements We would like to thank Mr. Carl Johnson, Dr. Neil Weston, and the numerous Georgia Tech faculty and students who have assisted in our personal and aerospace education, and this project specifically. In addition, the authors would like to individually thank the following: David C. Alman: My entire family, but in particular LCDR Allen E. Alman, USNR (BSAE Purdue ’49) and father James D. Alman (BSAE Boston University ’87) for instilling in me a love for aircraft, and Karrin B. Alman for being a wonderful mother and reading to me as a child. I’d also like to thank my friends, including brother Mark T. Alman, who have provided advice, laughs, and made life more fun. Also, I am forever indebted to Roe and Penny Stamps and the Stamps President’s Scholarship Program for allowing me to attend Georgia Tech and to the Georgia Tech Research Institute for providing me with incredible opportunities to learn and grow as an engineer. Lastly, I’d like to thank the countless mentors who have believed in me, helped me learn, and Page i provided the advice that has helped form who I am today. Andrew R. M. Hoeft: As with every undertaking in my life, my involvement on this project would not have been possible without the tireless support of my family and friends. -
Gallery of USAF Weapons Note: Inventory Numbers Are Total Active Inventory Figures As of Sept
Gallery of USAF Weapons Note: Inventory numbers are total active inventory figures as of Sept. 30, 2011. ■ 2012 USAF Almanac Bombers B-1 Lancer Brief: A long-range, air refuelable multirole bomber capable of flying intercontinental missions and penetrating enemy defenses with the largest payload of guided and unguided weapons in the Air Force inventory. Function: Long-range conventional bomber. Operator: ACC, AFMC. First Flight: Dec. 23, 1974 (B-1A); Oct. 18, 1984 (B-1B). Delivered: June 1985-May 1988. IOC: Oct. 1, 1986, Dyess AFB, Tex. (B-1B). Production: 104. Inventory: 66. Aircraft Location: Dyess AFB, Tex.; Edwards AFB, Calif.; Eglin AFB, Fla.; Ellsworth AFB, S.D. Contractor: Boeing, AIL Systems, General Electric. Power Plant: four General Electric F101-GE-102 turbofans, each 30,780 lb thrust. Accommodation: pilot, copilot, and two WSOs (offensive and defensive), on zero/zero ACES II ejection seats. Dimensions: span 137 ft (spread forward) to 79 ft (swept aft), length 146 ft, height 34 ft. B-1B Lancer (SSgt. Brian Ferguson) Weight: max T-O 477,000 lb. Ceiling: more than 30,000 ft. carriage, improved onboard computers, improved B-2 Spirit Performance: speed 900+ mph at S-L, range communications. Sniper targeting pod added in Brief: Stealthy, long-range multirole bomber that intercontinental. mid-2008. Receiving Fully Integrated Data Link can deliver nuclear and conventional munitions Armament: three internal weapons bays capable of (FIDL) upgrade to include Link 16 and Joint Range anywhere on the globe. accommodating a wide range of weapons incl up to Extension data link, enabling permanent LOS and Function: Long-range heavy bomber. -
CAA - Airworthiness Approved Organisations
CAA - Airworthiness Approved Organisations Category BCAR Name British Balloon and Airship Club Limited (DAI/8298/74) (GA) Address Cushy DingleWatery LaneLlanishen Reference Number DAI/8298/74 Category BCAR Chepstow Website www.bbac.org Regional Office NP16 6QT Approval Date 26 FEBRUARY 2001 Organisational Data Exposition AW\Exposition\BCAR A8-15 BBAC-TC-134 ISSUE 02 REVISION 00 02 NOVEMBER 2017 Name Lindstrand Technologies Ltd (AD/1935/05) Address Factory 2Maesbury Road Reference Number AD/1935/05 Category BCAR Oswestry Website Shropshire Regional Office SY10 8GA Approval Date Organisational Data Category BCAR A5-1 Name Deltair Aerospace Limited (TRA) (GA) (A5-1) Address 17 Aston Road, Reference Number Category BCAR A5-1 Waterlooville Website http://www.deltair- aerospace.co.uk/contact Hampshire Regional Office PO7 7XG United Kingdom Approval Date Organisational Data 30 July 2021 Page 1 of 82 Name Acro Aeronautical Services (TRA)(GA) (A5-1) Address Rossmore38 Manor Park Avenue Reference Number Category BCAR A5-1 Princes Risborough Website Buckinghamshire Regional Office HP27 9AS Approval Date Organisational Data Name British Gliding Association (TRA) (GA) (A5-1) Address 8 Merus Court,Meridian Business Reference Number Park Category BCAR A5-1 Leicester Website Leicestershire Regional Office LE19 1RJ Approval Date Organisational Data Name Shipping and Airlines (TRA) (GA) (A5-1) Address Hangar 513,Biggin Hill Airport, Reference Number Category BCAR A5-1 Westerham Website Kent Regional Office TN16 3BN Approval Date Organisational Data Name -
EASA AD No.: 2018-0211
EASA AD No.: 2018-0211 Airworthiness Directive AD No.: 2018-0211 Issued: 28 September 2018 Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EU) 2018/1139 on behalf of the European Union, its Member States and of the European third countries that participate in the activities of EASA under Article 129 of that Regulation. This AD is issued in accordance with Regulation (EU) 748/2012, Part 21.A.3B. In accordance with Regulation (EU) 1321/2014 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Consequently, no person may operate an aircraft to which an AD applies, except in accordance with the requirements of that AD, unless otherwise specified by the Agency [Regulation (EU) 1321/2014 Annex I, Part M.A.303] or agreed with the Authority of the State of Registry [Regulation (EU) 2018/1139, Article 71 exemption]. Design Approval Holder’s Name: Type/Model designation(s): CFM INTERNATIONAL S.A. CFM56-7B engines Effective Date: 05 October 2018 TCDS Number(s): EASA.E.004 Foreign AD: Not applicable Supersedure: This AD supersedes EASA AD 2018-0109 dated 17 May 2018. ATA 72 – Engine – Fan Blades – Inspection Manufacturer(s): SAFRAN Aircraft Engines, formerly SNECMA (France); General Electric Aircraft Engines (United States) Applicability: CFM56-7B20, CFM56-7B22, CFM56-7B22/B1, CFM56-7B24, CFM56-7B24/B1, CFM56-7B26, CFM56-7B26/B1, CFM56-7B26/B2, CFM56-7B27, CFM56-7B27/B1, CFM56-7B27/B3, CFM56-7B20/2, CFM56-7B22/2, CFM56-7B24/2, CFM56-7B26/2, -
Canada Aviation and Space Museum
CANADA AVIATION AND SPACE MUSEUM BOEING MODEL 720B PRATT & WHITNEY CANADA FLYING EXPERIMENTAL TEST BED REGISTRATION C-FETB Introduction The practical era of jet-age passenger transport aircraft officially dawned when the British de Havilland Company D.H.106 Comet made its premiere flight to great acclaim from the Hatfield, Hertfordshire aerodrome in England on 27 July 1949. Catering to British and mid to long-range routes to European, Middle Eastern and overseas destinations, the Comet series of airliners carried their passengers aloft in luxurious opulence for more than twenty years. Military and test derivatives followed suit and these continued flying for many decades, including two Comets for the Royal Canadian Air Force (RCAF). Just 14 days later, across the vast Atlantic Ocean, in the small town of Malton, Ontario, Canada, a new aviation company called Avro Canada successfully accomplished the same task with much less fanfare and accolades. Avro sent its small, medium-range, turbo-jet transport, called the C-102 Jetliner, aloft for its first flight, inaugurating the dreamed potential for such a unique travel experience for the public on the North American continent. United States Air Force personnel found the aircraft favourable when they tried it out on flights at Wright Field, Ohio in March 1951. However, this Canadian dream didn’t last for long. The modestly successful Comet-series didn’t shine as brightly as its popular name when a series of tragic, fatal accidents to production civil aircraft nearly snuffed out its very existence. Following design rectification’s, the Royal Air Force continued to employ Comets in versatile roles, such as modifying the design into the Nimrod. -
ISSEK HSE) Role of Big Data Augmented Horizon Scanning in Strategic and Marketing Analytics
National Research University Higher School of Economics Institute for Statistical Studies and Economics of Knowledge Big Data Augmented Horizon Scanning: Combination of Quantitative and Qualitative Methods for Strategic and Marketing Analytics [email protected] [email protected] XIX April International Academic Conference on Economic and Social Development Moscow, 11 April 2018 Outline - Role of artificial intelligence and big data in modern analytics - System of Intelligent Foresight Analytics iFORA - Combined quantitative and qualitative analysis methodology and software solutions - Use cases - Conclusion and discussion 2 Growing interest in Artificial Intelligence, Big Data and Machine Learning International analytical reports & news feed 12000 10000 8000 Artificial Intelligence 6000 Big Data Machine Learning 4000 2000 0 2000 2001 2002 2003 2004 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016 Russian analytical reports & news feed 800 700 600 500 Artificial Intelligence 400 Big Data 300 Machine Learning 200 100 0 2000 2001 2002 2003 2004 2005 2006 2007 2008 2009 2010 2011 2012 2013 2014 2015 2016 3 Source: System of Intelligent Foresight Analytics iFORA™ (ISSEK HSE) Role of Big Data Augmented Horizon Scanning in Strategic and Marketing Analytics AI-related tasks Tracking latest and challenges trends, technologies, drivers, barriers Market forecasting Trend analysis Understanding S&T modern skills and Instruments for Customers Market Intelligence competences analysis feedback knowledge discovery HR policy Vacancy Feedback mining -
The Aircraft Propulsion the Aircraft Propulsion
THE AIRCRAFT PROPULSION Aircraft propulsion Contact: Ing. Miroslav Šplíchal, Ph.D. [email protected] Office: A1/0427 Aircraft propulsion Organization of the course Topics of the lectures: 1. History of AE, basic of thermodynamic of heat engines, 2-stroke and 4-stroke cycle 2. Basic parameters of piston engines, types of piston engines 3. Design of piston engines, crank mechanism, 4. Design of piston engines - auxiliary systems of piston engines, 5. Performance characteristics increase performance, propeller. 6. Turbine engines, introduction, input system, centrifugal compressor. 7. Turbine engines - axial compressor, combustion chamber. 8. Turbine engines – turbine, nozzles. 9. Turbine engines - increasing performance, construction of gas turbine engines, 10. Turbine engines - auxiliary systems, fuel-control system. 11. Turboprop engines, gearboxes, performance. 12. Maintenance of turbine engines 13. Ramjet engines and Rocket engines Aircraft propulsion Organization of the course Topics of the seminars: 1. Basic parameters of piston engine + presentation (1-7)- 3.10.2017 2. Parameters of centrifugal flow compressor + presentation(8-14) - 17.10.2017 3. Loading of turbine blade + presentation (15-21)- 31.10.2017 4. Jet engine cycle + presentation (22-28) - 14.11.2017 5. Presentation alternative date Seminar work: Aircraft engines presentation A short PowerPoint presentation, aprox. 10 minutes long. Content of presentation: - a brief history of the engine - the main innovation introduced by engine - engine drawing / cross-section - -
Military Vehicle Options Arising from the Barrel Type Piston Engine
Journal of Power Technologies 101 (1) (2021) 22–33 Military vehicle options arising from the barrel type piston engine Pawe l Mazuro1 and Cezary Chmielewski1,B 1Warsaw University of Technology B [email protected] Abstract in terms of efficiency, meaning that piston engines can deliver enhanced range and endurance. This is benefi- The article reviews knowledge about requirements for engines in cial in missions requiring a stopover for refueling and state-of-the-art unmanned aerial vehicles and tanks. Analysis of particularly useful for unmanned supply, observation design and operational parameters was carried out on selected and maritime missions. turboshaft and piston engines generating power in the range of 500 - 1500 kW (0.5 - 1.5 MW). The data was compared In contrast, land combat vehicles have significantly with the performance of innovative, barrel type piston engines, different drive unit requirements. High mobility en- which are likely to become an alternative drive solution in the ables the vehicle to rapidly change location after de- target vehicle groups. tection. To this end, the torque curve as a function of the rotational speed of the shaft is of decisive im- portance. Keywords: military UAV, tanks, turboshaft engines, piston engines, barrel type piston engines The complexity of tank engines adds an additional layer of requirements, impacting the reliability and durability of the power unit, and they come with re- 1 Introduction lated manufacturing and operating costs. In military land vehicles, the engine should be as small This article consolidates knowledge on options and as possible; the space saved can be used for other capabilities arising from use of the barrel type piston purposes. -
ATP® Libraries Catalog
2 ATP® Libraries Catalog Revision Date May 24 2016 ATP 101 South Hill Drive Brisbane, CA 94005 (+1) 415-330-9500 www.atp.com ATP® Policies and Legal www.atp.com/policy © Copyright 2016, ATP. All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted in any form by any means, electronic, mechanical, photocopying, recording or otherwise, without prior written permission of ATP. The information in this catalog is subject to change without notice.ATP, ATP Knowledge, ATP Aviation Hub, HubConnect, NavigatorV, and their respective logos, are among the registered trademarks or trademarks of ATP. All third-party trademarks used herein are the property of their respective owners and ATP asserts no ownership rights to these items. iPad and iPhone are trademarks of Apple Inc., registered in the U.S. and other countries. App Store is a service mark of Apple Inc. All original authorship of ATP is protected under U.S. and foreign copyrights and is subject to written license agreements between ATP and its subscribers. Visit www.atp.com/policy for more information ATP Customer Support Please visit www.atp.com/support for customer support information ATP® Libraries Catalog – Revision Date: May 24 2016 3 CONTENTS CONTENTS ...................................................................................................................................................................... 3 REGULATORY LIBRARIES .............................................................................................................................................