Participation in Programs – Fixed Wing Aircraft
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Hangar 9 Ultimate Manual
TM® WE GET PEOPLE FLYING 46% TOC Ultimate 10-300 ASSEMBLY MANUAL Specifications Wingspan ..........................................................................................100 in (2540 mm) Length ................................................................................................110 in (2794 mm) Wing Area.........................................................................................3310 sq in (213.5 sq dm) Weight ...............................................................................................40–44 lb (18–20 kg) Engine.................................................................................................150–200cc gas engine Radio ..................................................................................................6-channel w/15 servos Introduction Thank you for purchasing the Hangar 9® 46% TOC Ultimate. Because size and weight of this model creates a higher degree for potential danger, an added measure of care and responsibility is needed for both building and flying this or any giant-scale model. It’s important that you carefully follow these instructions, especially those regarding hinging and the section on flying. Like all giant-scale aerobatic aircraft, the Hangar 9® TOC Ultimate requires powerful, heavy-duty servos. Servos greatly affect the flight performance, feel and response of the model. To get the most out of your Ultimate, it’s important to use accurate, powerful servos on all control surfaces. In the prototype models, we used JR 8411 digital servos with excellent -
Aircraft Circular No. 103
NATIONAL ADVISORY COifuciITTEE FOR AERONAUTICS. AIRCRAFT CIRCULAR NO. 103. THE BRISTOL II BULLDOG" (BRITISH)* - A Single-seat All-Steel Fighter. The Bristol "Bulldog" was designed on the Bristol princi ples of metal construction by The Bristol Aeroplane Co., Ltd. The entire structural portion is of high tensile steel (Figs. 1, 2, and 3). The airplane is powered with the IIBristolll Jupiter radial air-cooled engine, either the "Bristolll Jupiter Series VII supercharged engine, when exceptional. speed and performance at high altitudes are espeGially required, or the IIBristol" Jupiter Series VI.A engine when the normal operating area of the airplane is not expected to exceed, say, 15,000 feet. The two types of engine are entirely interchangeable when desired. The speeds maintained at altitudes with the rate of climb. and the ceiling are given in tables at conolusion of this Circular. Fu s e I age The fuselage structure comprises three ·main parts, the front and rear portions and the stern frrune. Of these, the front ~or tion and the stern frame are constructed of high tensile tubes and the rear portion of members built up of high tensile steel str ip in special "Bristolll sections. Front end.- This portion extends from the front bulkhead *From circular issued by The Bristol Aeroplane Co., Ltd., England. N.A.C.A. Aircraft Circular No. 103 2 to the end of the tubular longerons, and acc~mmodates the pilot1s seat, controls lli~d most of the military equipment, etc. No bracing wires are fitted in the side frames and transverse brac ing is fitted only in the foremost panel. -
Aircraft Circulaels National Advisory Committee For
AIRCRAFT CIRCULAELS NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS No 119 THE AVRO TRAINER AIBPLAE (ERI T IS H) A Training Biplane Washington June, 1930 NATIONAL ADVISORY COlvilvITTEE FOR AERONAUTICS. AIRCRAFT CIRCULAR NO. 119. THE "AVRO TRAINER" AIRPLANE (BRITIsH)* A Training Biplane. Although the "Trainer" has scarcely a single dimension in common with the "504," the "family likeness" is quite striking. The two most marked changes are: the different shape of the rudder and the different landing gear. This airplane is primarily intended for training purposes and the requirements of -training have quite obviously been kept prominently in view throughout the design. Large, comfortable cockpits, good view, effective windshields, wide track are some of the features (Figs. 1, 3, 4) of the "Trainer." Constructional Features One of the innovations introduced in the "Avro Trainer" is that it is of all-metal construction (with exception of the fabric covering and the wooden fairings of the fuselage) in order to conform to thb requirements of the Air Ministry. In the tt Trainer" fuselage the modern form of Avro welded tube construction is employed (Figs. 5,6). Uniform stress is not easy of attainment in any aIrcraft structure, and the welded tube fuselage is no exception. In the "Trainer," however, an approach towards it has been made , by *From Flight, My 2, 1930. N.A.C.A. Aircraft Circular No. 119 2 having the longerons of thee different diameters, largest in front, medium from cockpits to about halfway towards the tail, and smallest in the tail end. The smaller tube is inserted a short distance into the larger, and the joint is then welded. -
A Design Study of a Proposed Four-Seat, Amateur-Built Airplane
University of Tennessee, Knoxville TRACE: Tennessee Research and Creative Exchange Masters Theses Graduate School 8-2003 A Design Study of a Proposed Four-Seat, Amateur-Built Airplane D. Andrew Moore University of Tennessee - Knoxville Follow this and additional works at: https://trace.tennessee.edu/utk_gradthes Part of the Mechanical Engineering Commons Recommended Citation Moore, D. Andrew, "A Design Study of a Proposed Four-Seat, Amateur-Built Airplane. " Master's Thesis, University of Tennessee, 2003. https://trace.tennessee.edu/utk_gradthes/2113 This Thesis is brought to you for free and open access by the Graduate School at TRACE: Tennessee Research and Creative Exchange. It has been accepted for inclusion in Masters Theses by an authorized administrator of TRACE: Tennessee Research and Creative Exchange. For more information, please contact [email protected]. To the Graduate Council: I am submitting herewith a thesis written by D. Andrew Moore entitled "A Design Study of a Proposed Four-Seat, Amateur-Built Airplane." I have examined the final electronic copy of this thesis for form and content and recommend that it be accepted in partial fulfillment of the requirements for the degree of Master of Science, with a major in Mechanical Engineering. Dr. Gary Flandro, Major Professor We have read this thesis and recommend its acceptance: Dr. Louis Deken, Dr. Peter Solies Accepted for the Council: Carolyn R. Hodges Vice Provost and Dean of the Graduate School (Original signatures are on file with official studentecor r ds.) To the Graduate Council: I am submitting herewith a thesis written by D. Andrew Moore entitled “A Design Study of a Proposed Four-Seat, Amateur-Built Airplane.” I have examined the final electronic copy of this thesis for form and content and recommend that it be accepted in partial fulfillment of the requirements for the degree of Master of Science, with a major in Mechanical Engineering. -
ATR-42/72 Rev 6
U.S. Department of Transportation Federal Aviation Administration Washington, DC Flight Standardization Board (FSB) Report Revision: 6 Date: 10/14/2016 Manufacturer ATR – GIE Avions de Transport Régional Type Certification Data Sheet (TCDS) A53EU TCDS Identifiers ATR-42 ATR-72 ATR-42-200-300-320-500-600 ATR-72-101-102-201-202-211-212A-212 Pilot Type Rating ATR42 ATR72 Timothy C. Hayward, Chair Flight Standardization Board Federal Aviation Administration Flight Standards Division Seattle Aircraft Evaluation Group 1601 Lind Avenue SW Renton, WA 98057-3356 Telephone: (425) 917-6600 Fax: (425) 917-6638 Revision 6 10/14/2016 ATR-42/ATR-72 FSB Report RECORD OF REVISIONS REVISION SECTION PAGES DATE 1 9.2.4 17–27 01/10/1994 2 ALL ALL 02/01/1996 3 VARIOUS VARIOUS 07/01/1997 4 VARIOUS VARIOUS 7/15/2002 5 ALL ALL 12/05/2014 6 ALL ALL 10/14/2016 HIGHLIGHTS OF CHANGE All Sections All Pages: This revision contains minor editorial changes on every page for clarity, consistency, standardization, updated terminology, acronyms, and United States Workforce Rehabilitation Act Section 508 compliancy. Added Clarity for Training for Seat-Dependent Tasks (6.1.7 and 6.1.7). Added Clarity for Second-in-Command (SIC) Training Tasks (6.1.8). Added Clarity for Unique Training Provisions (6.2.6.1). Page 2 of 26 Revision 6 10/14/2016 ATR-42/ATR-72 FSB Report CONTENTS SECTION PAGE RECORD OF REVISIONS .......................................................................................................2 HIGHLIGHTS OF CHANGE ...................................................................................................2 1. PURPOSE AND APPLICABILITY .........................................................................................4 2. PILOT “TYPE RATING” REQUIREMENTS ..........................................................................7 3. “MASTER COMMON REQUIREMENTS” (MCRs) ..............................................................7 4. -
TAC Register Rev 6 22 Feb 2017
2/22/2017 Aircraft TAC TAC Register Rev 6 22 Feb 2017 THE REPOSITORY (SPREADSHEET): This data presented in this repository is a list of approved SACAA TACs as conferred to current foreign TC holders. Aircraft Type/Model File No. Conditions Category TAC Issue Issue Date Reissue Date Common Name 328 Support Services GmbH Dornier 328-100 & Dornier 328-300 J15/12/529 As per Type Certficate Data Sheet EASA.A.096 Standard Original 11 April 2007 - 328JET (328-300) Agusta S.p.A. (Now Leonardo Helicopter) A109E, A109K2, A109S, AW109SP and A109C J15/12/395 This certificate is issued as per EASA Type Certificate number EASA.R.005 Standard Reissue 15 September 1996 01 August 2013 AB139 J15/12/493 This certificate is issued as per EASA Type Certificate number EASA.R.006 Standard Original 21 April 2006 - AB139, AW139 AW189 J15/12/625 This certificate is issued as per EASA Type Certificate number EASA.R.510 Standard Original 24 November 2016 AW189 Air Tractor Inc. AT-402, AT-402B, AT-502, AT-502A, AT-502B & AT-504, AT-402A J15/12/327 This certificate is issued as per FAA Type Certificate number A17SW Restricted Original 15 October 2013 28 July 2016 AT-602, AT-802 and AT-802A J15/12/380 This certificate is issued as per FAA Type Certificate number A19SW Restricted Original 15 October 2013 - Airbus SAS A300B4-622R J15/12/565 This certificate is issued as per DGAC Type Certificate number 72. Standard Original 23 December 2009 - A320-232, A320-233 J15/12/593 This certificate is issued as per EASA Type Certificate number EASA.A.064 Standard Original 23 December 2011 - A330-301, A330-321, A330-322, A330- 341, A330-342, A330-202, A330-223, A330-243, A330-323, A330-343, A330- 203, A330-201, A330-302, A330-303, A330-223F and A330-243F J15/12/584 This certificate is issued as per EASA Type Certificate number EASA.A.004 Standard Original 08 December 2010 10 November 2016 A340-200, A340-300 and A340-600 series J15/12/382 As per DGAC Type Certficate number 183. -
E N a C / Eetac Atr
E N A C / EETAC ATR FAA regulation analysis for ATR ETOPS validation Jordi CLARAMUNT SEGURA IENAC14 - Erasmus End of studies report / Treball Final de Grau 11/08/2017 FAA regulation analysis for ATR ETOPS validation 2 3 FAA regulation analysis for ATR ETOPS validation Acknowledgements With deepest gratitude and appreciation, I humbly give thanks to the people who helped me in making this end of studies project a possible one. First of all, I would like to offer my special thanks to Souhir Charfeddine, my internship tutor in ATR, for choosing me among the other candidates and giving me the possibility to perform this internship. Thanks for her valuable and constructive help during the planning and development of this internship. I really appreciate all the time she has dedicated to me with all the different meetings we have had inside the company. I have learnt a lot at her side, she has been an amazing tutor. Thank you. I am also grateful to all of those with whom I have had the pleasure to work with during this project. Each of the members I have worked with have provided me extensive and professional guidance and taught me a great deal about certification aspects, as well as other domains. Those include Antonio Paradies, Didier Cailhol, Eric Bédessem, Ciro Manco, Fabien Vançon, Jean-Paul Delpont, Nadège Gualina and Lucille Mitchell. Also, I would like to offer my gratitude to ENAC for first, giving me the possibility to join their Erasmus programme in its great university and then, for allowing me having the chance to do the internship, which has been the best election of my life so far. -
European Aviation Safety Agency
TCDS No.: EASA.A.084 ATR 42 - ATR 72 Page 1 of 35 Issue: 03 Date: 17 October 2012 European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET No. EASA.A.084 for ATR 42 and ATR 72 Type Certificate Holder: ATR-GIE Avions de Transport Régional 1, Allée Pierre Nadot 31712 Blagnac Cedex FRANCE Transport Category: Large Aeroplanes For Models: ATR 42-200, ATR 42-300, ATR 42-320, ATR 42-400, ATR 42-500 ATR 72-101, ATR 72-102, ATR 72-201, ATR 72-202, ATR 72-211, ATR 72-212, ATR 72-212A TCDS No.: EASA.A.084 ATR 42 - ATR 72 Page 2 of 35 Issue: 03 Date: 17 October 2012 Intentionally left blank TCDS No.: EASA.A.084 ATR 42 - ATR 72 Page 3 of 35 Issue: 03 Date: 17 October 2012 TABLE OF CONTENTS SECTION 1: ATR 42 Series ...................................................................................... 4 I. General .......................................................................................................................... 4 II. Certification Basis .......................................................................................................... 5 III. Technical Characteristics and Operational Limitations .................................................11 IV. Operating and Service Instructions ..............................................................................18 SECTION 2: ATR 72 Series .................................................................................... 19 I. General .........................................................................................................................19 II. Certification -
Aircraft Tire Data
Aircraft tire Engineering Data Introduction Michelin manufactures a wide variety of sizes and types of tires to the exacting standards of the aircraft industry. The information included in this Data Book has been put together as an engineering and technical reference to support the users of Michelin tires. The data is, to the best of our knowledge, accurate and complete at the time of publication. To be as useful a reference tool as possible, we have chosen to include data on as many industry tire sizes as possible. Particular sizes may not be currently available from Michelin. It is advised that all critical data be verified with your Michelin representative prior to making final tire selections. The data contained herein should be used in conjunction with the various standards ; T&RA1, ETRTO2, MIL-PRF- 50413, AIR 8505 - A4 or with the airframer specifications or military design drawings. For those instances where a contradiction exists between T&RA and ETRTO, the T&RA standard has been referenced. In some cases, a tire is used for both civil and military applications. In most cases they follow the same standard. Where they do not, data for both tires are listed and identified. The aircraft application information provided in the tables is based on the most current information supplied by airframe manufacturers and/or contained in published documents. It is intended for use as general reference only. Your requirements may vary depending on the actual configuration of your aircraft. Accordingly, inquiries regarding specific models of aircraft should be directed to the applicable airframe manufacturer. -
Explanatory Note to TCDS IM.A.120 – Boeing 737 Issue 11
Explanatory Note to TCDS IM.A.120 – Boeing 737 Issue 11 This annex to the EASA TCDS IM.A.120 was created to publish selected special conditions / deviations / equivalent safety findings that are part of the applicable certification basis: Table of Contents: Certification Review Items: A-10: Additional requirements for import ...........................................................................................3 A. 11-02: Pressurised Cabin Loads ......................................................................................................5 A. 11-04: Emergency Landing Dynamic Loads ...................................................................................6 A. 11-05: Fatigue and Damage Tolerance ............................................................................................7 A. 11-06: Fasteners ...............................................................................................................................9 A. 11-08: Lift and Drag Device Indicator ..........................................................................................10 A. 11-11: Doors ..................................................................................................................................11 A. 11-12: Seat, Berths, Safety Belts and Harness ..............................................................................12 A. 11-13: Direct view and cabin attendant seat ..................................................................................13 A. 11-16: Equipment Systems and Installations ................................................................................14 -
Aviation Transportation Safety Investigation Report A18O0106
Air Transportation Safety Investigation Report A18O0106 IN-FLIGHT SEPARATION OF RIGHT WING Quad City Challenger II (advanced ultralight), C-IGKT North Bay, Ontario, 14.3 nm E 30 July 2018 History of the flight On 29 July 2018, 2 privately operated Quad City Ultralight Aircraft Corporation (Quad City) Challenger II advanced ultralight aircraft equipped with amphibious floats departed Ottawa/Rockcliffe Airport (CYRO), Ontario, for a daytime visual flight rules cross-country flight to North Bay Airport (CYYB), Ontario. While en route, the 2 aircraft encountered strong winds and turbulence, and the pilots decided to land on the Ottawa River, near Mattawa, Ontario. During the landing, the occurrence aircraft (registration C-IGKT, serial number CH2-1199-1919) touched down hard. After a short lunch break, the pilots inspected the 2 aircraft and then flew to CYYB without further incident. On 30 July 2018, the 2 aircraft departed CYYB at 09321 and climbed to between 1800 and 2000 feet above sea level for the return flight to CYRO. At approximately 0950, the occurrence aircraft’s right wing separated from the aircraft when it was over Talon Lake, Ontario, 14.3 nautical miles east of CYYB. The aircraft entered an uncontrolled descent and collided with terrain in a wooded area. A post- impact fire ensued. The pilot was fatally injured. The aircraft was destroyed by impact forces and the post-impact fire. The pilot of the other aircraft overflew the occurrence site and landed on Talon Lake. At 0959, he met a local resident, who called 911 to report the accident. There was no emergency locator transmitter on board, and none was required by regulations. -
NASA Technical Memorandum 0000
NASA/TM–2018-219833 Short-Haul Revitalization Study Final Report Ty V. Marien, Kevin R. Antcliff, Mark D. Guynn, and Douglas P. Wells Langley Research Center, Hampton, Virginia Steven J. Schneider and Michael Tong NASA Glenn Research Center, Cleveland, Ohio Antonio A. Trani and Nicolas K. Hinze Virginia Polytechnic Institute and State University, Blacksburg, Virginia Samuel M. Dollyhigh Analytical Mechanics Associates Inc., Hampton, Virginia May 2018 NASA STI Program . in Profile Since its founding, NASA has been dedicated to the CONFERENCE PUBLICATION. advancement of aeronautics and space science. The Collected papers from scientific and technical NASA scientific and technical information (STI) conferences, symposia, seminars, or other program plays a key part in helping NASA maintain meetings sponsored or this important role. co-sponsored by NASA. The NASA STI program operates under the auspices SPECIAL PUBLICATION. Scientific, of the Agency Chief Information Officer. It collects, technical, or historical information from NASA organizes, provides for archiving, and disseminates programs, projects, and missions, often NASA’s STI. The NASA STI program provides access concerned with subjects having substantial to the NTRS Registered and its public interface, the public interest. NASA Technical Reports Server, thus providing one of the largest collections of aeronautical and space TECHNICAL TRANSLATION. science STI in the world. Results are published in both English-language translations of foreign non-NASA channels and by NASA in the