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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. -
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. -
Over Thirty Years After the Wright Brothers
ver thirty years after the Wright Brothers absolutely right in terms of a so-called “pure” helicop- attained powered, heavier-than-air, fixed-wing ter. However, the quest for speed in rotary-wing flight Oflight in the United States, Germany astounded drove designers to consider another option: the com- the world in 1936 with demonstrations of the vertical pound helicopter. flight capabilities of the side-by-side rotor Focke Fw 61, The definition of a “compound helicopter” is open to which eclipsed all previous attempts at controlled verti- debate (see sidebar). Although many contend that aug- cal flight. However, even its overall performance was mented forward propulsion is all that is necessary to modest, particularly with regards to forward speed. Even place a helicopter in the “compound” category, others after Igor Sikorsky perfected the now-classic configura- insist that it need only possess some form of augment- tion of a large single main rotor and a smaller anti- ed lift, or that it must have both. Focusing on what torque tail rotor a few years later, speed was still limited could be called “propulsive compounds,” the following in comparison to that of the helicopter’s fixed-wing pages provide a broad overview of the different helicop- brethren. Although Sikorsky’s basic design withstood ters that have been flown over the years with some sort the test of time and became the dominant helicopter of auxiliary propulsion unit: one or more propellers or configuration worldwide (approximately 95% today), jet engines. This survey also gives a brief look at the all helicopters currently in service suffer from one pri- ways in which different manufacturers have chosen to mary limitation: the inability to achieve forward speeds approach the problem of increased forward speed while much greater than 200 kt (230 mph). -
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 -
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 - -
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 ............................................................................................................................................. -
The Market for Aviation Turbofan Engines
The Market for Aviation Turbofan Engines Product Code #F640 A Special Focused Market Segment Analysis by: Aviation Gas Turbine Forecast Analysis 1 The Market for Aviation Turbofan Engines 2010-2019 Table of Contents Executive Summary .................................................................................................................................................2 Introduction................................................................................................................................................................2 Trends..........................................................................................................................................................................3 Market Focus .............................................................................................................................................................3 Competitive Environment.......................................................................................................................................4 Figure 1 - The Market for Aviation Turbofan Engines Unit Production 2010 - 2019 (Bar Graph) .................................................................................6 Figure 2 - The Market for Aviation Turbofan Engines Value of Production 2010 - 2019 (Bar Graph)...........................................................................6 Manufacturers Review.............................................................................................................................................7 -
Helicopter Noise Reduction Technology, Status Report
Helicopter Noise Reduction Technology Status Report 21 April 2015 Contributors: ICCAIA: Snecma, Airbus Helicopters, Sikorsky Aircraft, Bell Helicopter, AgustaWestland, Turbomeca, Marenco Swisshelicopter Research Centers: NASA, DLR, ONERA, JAXA 1 Contents 1 Introduction .................................................................................................................................................. 3 2 Helicopter noise sources and related noise generation mechanisms ............................................................ 4 2.1 Rotor noise ........................................................................................................................................... 4 2.2 Anti-torque noise .................................................................................................................................. 4 2.3 Engine noise ......................................................................................................................................... 5 2.3.1 Turboshaft Engines.......................................................................................................................... 5 2.3.2 Piston Engines ................................................................................................................................. 5 2.4 Contribution of noise sources depending on flight condition .............................................................. 5 3 State-of-the-Art Helicopters ........................................................................................................................ -
General Electric CF34 Engine
General Electric CF34 Engine 2 STAGE HIGH PRESSURE TURBINE Powerplant FLOW THROUGH ANNULAR FAN VANE COMBUSTION SPINNER 14 STAGE HIGH PRESSURE AXIAL COMPRESSOR 4 STAGE LOW PRESSURE TURBINE SINGLE STAGE FAN BYPASS RATIO 6.2:1 ACCESSORY GEAR BOX FAN BLADE CONTAINMENT CASING Challenger 601 Developed for Training Purposes 4-175 November 1997 CAE SimuFlite 4-176 Developed for Training Purposes Challenger 601 November 1997 Powerplant Engine Oil System B-SUMP SUPPLY OIL VENT AIR REGULATING SCAVENGE OIL VALVE VENT 1 CHIP DETECTOR, INSTALLED ON 1A/3A; OPTIONAL ON 3R A-SUMP B-SUMP C-SUMP 1, 2 & 3 4 & 5 6 & 7 BEARING BEARING BEARING ORIFICE 1 1 HEAT EXCHANGER FUEL SCAVENGE SCREENS (8 PLACES) 1 2 PRESSURE ACCESSORY TRANSMITTER GEARBOX A-SUMP FILTER ELEMENT SCAVENGE 1 PUMP 1 2 3 4 5 6 7 CHECK TANK PRESSURE VALVE RELIEF VALVE 1 1 BYPASS VALVE SCAVENGE PRESSURE ELEMENTS ELEMENT (6) DEAERATOR RELIEF VALVE OIL LEVEL PROBE OIL TANK OIL TEMP PROBE IMPENDING BYPASS 1 LUBE AND SCAVENGE SENSOR ELECTRIC DRAIN PUMP ASSEMBLY MASTER CHIP PORT DETECTOR Challenger 601 Developed for Training Purposes 4-177 November 1997 CAE SimuFlite Engine Fuel System GE CF34-1A/-3A STATOR VANES VG FUEL TEMP TO INLET 14 STAGE 70 70 ECOLOGICAL GUIDE FUEL DRAIN VANES BLEED AIR 60 60 40 40 VG 20 20 0 0 -20 -20 C¡ LR TO ECOLOGICAL SYSTEM FUEL HEATER FEEDBACK N2 SPEED FUEL GOVERNING PLA 4000 3500 FUEL 3000 BYPAS P3 T2C 2000 P 1000 N P 2 800 600 400 200 0 LR BYPASS MAIN FUEL CONTROL FLOW VALVE FUEL PUMP PRIMARY x10 HIGH PRESSURE FUEL FLOW FILTER ELEMENT TORQUE FIREWALL MOTOR SHUTOFF RELIEF -
AIN 2014 Product Support Survey
required tooling and material to to shape connectivity solutions. reliability challenge. Honeywell 2014 Engine rescue an AOG,” the company “When these pilot advisors on has had success in these types Survey Rules told AIN. our Global Customer Committee of location with hydrodynamic Manufacturer Ratings (GCC) told us they needed bet- carbon seal designs and has & Methodology Overall Overall Overall Williams International ter access to Honeywell’s techni- recently introduced them to Average Average Average As with AIN Publications’ previ- “We have been focusing on cal resources, we responded. The the TFE731-20/40/50/60 acces- 2014 2013 2013-2014 ous annual Product Support Surveys, ensuring owners have no worries new Honeywell Pilot Gateway sory gearboxes.” Turbofan the objective this year was to obtain when operating our engines.” To (http://pilots.honeywell.com) Honeywell has drawn on from the users of business jets, accomplish this, Williams intro- is a one-stop shop for our techni- human-factor design principles Rolls-Royce 8.0 7.8 0.2 turboprop airplanes and turbine- duced “significant enhancements cal publications, pilot guides and to reduce the number of tools Williams 8.0 8.1 -0.1 powered helicopters statistically to our Total Assurance Program familiarization videos, all orga- required to perform mainte- Honeywell 7.9 7.8 0.1 valid information about the product (TAP). We created TAP Blue, nized by aircraft make, model nance tasks on the HTF7000. CFE 7.6 7.3 0.3 support provided by engine manu- which provides an unlimited- and system type.” The tool also Historically, more than 30 dif- GE 7.6 7.9 -0.3 facturers over the last year and to duration warranty with coverage allows pilots to provide feed- ferent hand tools were required P&WC 7.6 7.7 -0.1 report this information to our read- beyond that offered anywhere back, report technical problems to perform maintenance tasks Turboprops ers. -
Loss of Control and Collision with Water Involving Eurocopter EC120B, VH
Loss of control and collision with water involving Eurocopter EC120B, VH-WII Hardy Reef, 72 km north-north-east of Hamilton Island Airport, Queensland on 21 March 2018 ATSB Transport Safety Report Aviation Occurrence Investigation (Systemic) AO-2018-026 Final – 16 June 2021 Cover photo: CQ Plane Spotting 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, ACT 2601 Telephone: 1800 020 616, from overseas +61 2 6257 2463 Accident and incident notification: 1800 011 034 (24 hours) Email: [email protected] Website: www.atsb.gov.au © Commonwealth of Australia 2021 Ownership 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 licence 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. Where you want to use their material you will need to contact them directly.