A Dean Wilson Kit-Built Delight by Budd Davisson by Sparky Barnes Sargent
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Final Report
FINAL REPORT of civil aviation safety investigation CLASSIFICATION Accident Operator Privat Manufacturer TECNAM Aircraft Tecnam P2008-JC Registration country Romania Registration YR-LMP Șirna airfield, Prahova county Location Coordinates: Latitude: 44°47ʹ08ʺN Longitude: 025°59ʹ17ʺE Date and time 31.03.2018 / 18:05 LT (15:05 UTC) No. : A 19 - 12 Date : 13.11.2019 For notifications regarding civil aviation 1-3 Walter Maracineanu Square, 6th floor, accidents and serious incidents: District 1, Bucharest – postal code 010155, Romania Phone: +40 751 192088 (24/7) Phone: +40 21 2220535, Fax: +40 378 107106 E-mail: [email protected] E-mail: [email protected] Website: www.aias.gov.ro Accident –Tecnam P 2008 – YR-LMP – Șirna – Prahova county – 31.03.2018 – SIAA ACKNOWLEDGMENT This REPORT presents data, analysis, conclusions and recommendations of the civil aviation safety investigation commission appointed by the General Director of AIAS. The civil aviation safety investigation has been conducted in accordance with the provisions of the Regulation (EU) no. 996/2010 of the European Parliament and of the Council from 20 October 2010 on the investigation and prevention of accidents and incidents in civil aviation and repealing Directive 94/56/EC, with the provisions of ICAO Annex 13 to the International Civil Aviation Convention signed at Chicago on 7 December 1944, and with the provisions of Government Ordinance no. 26/2009, approved and completed by the Law no. 55/2010, amended and completed by the Government Ordinance no. 17/2018. The objective of the civil aviation safety investigation is to prevent accidents and incidents, by effective determination of facts, causes and circumstances that led to civil aviation occurrences and to issue recommendations for civil aviation safety. -
Certificated Aircraft Engines
CERTIFICATED AIRCRAFT ENGINES SSP1101 DECEMBER 2013 652 Oliver Street Williamsport, PA 17701 U.S.A. Phone: Main OfficeU.S. and Canada Toll Free +1 (800) 2583279 Direct +1 (570) 3236181 Sales Department +1 (570) 3277278 Facsimile +1 (570) 3277101 Visit us on the World Wide Web at: http://www.lycoming.com ©2013 Avco Corporation All Rights Reserved. Lycoming Engines is a division of Avco Corporation. TABLE OF CONTENTS PISTON CERTIFICATED ENGINES – (4) Four Cylinder Series ....................................................................................................................................................... 1 (6) Six Cylinder Series ....................................................................................................................................................... 16 (8) Eight Cylinder Series .................................................................................................................................................... 32 PISTON ENGINE INSTALLATIONS (4) Four Cylinder Installations............................................................................................................................................ 33 (6) Six Cylinder Installations.............................................................................................................................................. 42 TURBOCHARGED .................................................................................................................................................... 46 GEARED................................................................................................................................................................... -
Propulsion Systems for Aircraft. Aerospace Education II
. DOCUMENT RESUME ED 111 621 SE 017 458 AUTHOR Mackin, T. E. TITLE Propulsion Systems for Aircraft. Aerospace Education II. INSTITUTION 'Air Univ., Maxwell AFB, Ala. Junior Reserve Office Training Corps.- PUB.DATE 73 NOTE 136p.; Colored drawings may not reproduce clearly. For the accompanying Instructor Handbook, see SE 017 459. This is a revised text for ED 068 292 EDRS PRICE, -MF-$0.76 HC.I$6.97 Plus' Postage DESCRIPTORS *Aerospace 'Education; *Aerospace Technology;'Aviation technology; Energy; *Engines; *Instructional-. Materials; *Physical. Sciences; Science Education: Secondary Education; Textbooks IDENTIFIERS *Air Force Junior ROTC ABSTRACT This is a revised text used for the Air Force ROTC _:_progralit._The main part of the book centers on the discussion -of the . engines in an airplane. After describing the terms and concepts of power, jets, and4rockets, the author describes reciprocating engines. The description of diesel engines helps to explain why theseare not used in airplanes. The discussion of the carburetor is followed byan explanation of the lubrication system. The chapter on reaction engines describes the operation of,jets, with examples of different types of jet engines.(PS) . 4,,!It********************************************************************* * Documents acquired by, ERIC include many informal unpublished * materials not available from other souxces. ERIC makes every effort * * to obtain the best copravailable. nevertheless, items of marginal * * reproducibility are often encountered and this affects the quality * * of the microfiche and hardcopy reproductions ERIC makes available * * via the ERIC Document" Reproduction Service (EDRS). EDRS is not * responsible for the quality of the original document. Reproductions * * supplied by EDRS are the best that can be made from the original. -
2011 Northeast LSA EXPO
2011 NorthEast LSA EXPO This annual event, organized by EAA Chapter 106 (a 501(c)(3) public charity), showcases Light Sport Aircraft (LSA) and offers 3-4 free & interesting seminars. Rain date: Sun – Sept 12 – check www.EAA106.org ‘News Flash’ for info 3 - 4 F R E E SEMINARS 33 -- 4 F R E E SEMINARS 2011 NorthEast LSA EXPO – 9:30 am ––– Sport Pilot Rules, Light Sport Aircraft & Safety 11:30 am ––– Flight Medical ––– Common medical issues 12:30 pm ––– Terrafugia TransitionTransition® - an LSA --- Update 2:00 pm ––– tbd FAA WINGS CREDIT – Info & Registration: http://www.faasafety.gov/SPANS/event_details.aspx?eid=40036 2011 NorthEast LSA EXPO – EVENT FLYER LINK: http://www.eaa106.org/2011_0917_NorthEast_LSA_EXPO_flyer_7_pgs.pdf 2011 NE LSA EXPO - 11+ LSA AIRCRAFT PLANNING TO DISPLAY: 1 Terrafugia Transition (next generation prototype of their flying car) 2 Evektor Harmony 3 Flight Design CTLS 4 Legend Amphib Cub 2011 5 Remos GX 6 SportCruiser 7 Sting S3 8 Tecnam P2008 9 Van's RV-12 10 So. ME Aviation (school) - their Gobosh G700 11 So. ME Aviation (school) - their Cape Town (Valor on floats) 12 maybe more … (maybe Zenith , Escapade , SportCub , more?) The following may not available for the new date of Sept.17 – TBD: 1 Aerotrek A240 2 Jabiru J230-SP Other LSA and/or aviation exhibitors possible – Check website or contact EAA106. SEE PICTURES & INFO + SEMINARS on the following pages Including “About” EAA106 – and how to JOIN/SUPPORT us ! EAA Chapter 106 is proud to have, as members of our chapter, several of the principals from Terrafugia ! Yes – It is a Flying Car ! Model: ® Terrafugia Transition Info: Street-legal S-LSA. -
Fabrication of Supercharger in Two Wheeler Engine
Vol-2 Issue-2 2016 IJARIIE-ISSN(O)-2395-4396 FABRICATION OF SUPERCHARGER IN TWO WHEELER ENGINE 1 2 3 4 5 T Prakash G Arun Kumar , S Arun Kumar , R Manoj Kumar , M G Midhun 1,2,3,4, MECHANICAL ENGINERRING, VIDYAA VIKAS COLLEGE OF ENGINEERING AND TECHNOLOGY, TIRUCHENGODE, NAMAKKAL (DT) 637214, TAMILNADU, India ABSTRACT A super charger is an air compressor used for forced injection of an internal combustion engine. The purpose of a super charger is to increase the density of air entering the engine to create more power. A supercharger is the compressor is powered by the rotation of chain sprocket in the bike. In addition to the foregoing advantages the supercharger gives greater mechanical efficiency and fuel economy .Moreover, the engine can be made smaller ,the compression can be well below that at which detonation occurs and still afford a surplus of power ,heat losses in the water jacket are reduced because larger chargers of mixture in the cylinders Keyword: - carburetor, chain sprocket etc…. 1. INTRODUCTION A supercharger is an air compressor that increases the pressure or density of air supplied to an internal combustion engine. This gives each intake cycle of the engine more oxygen, letting it burn more fuel and do more work, thus increasing power. Power for the supercharger can be provided mechanically by means of a belt, gear, shaft, or chain connected to the engine’s crankshaft. When power is provided by a turbine powered by exh aust gas, a supercharger is known as a turbo supercharger – typically referred to simply as a turbocharger or just turbo. -
National Advisory Committee for Aeronautics
- I 0 N NATIONAL ADVISORY COMMITTEE 0 FOR AERONAUTICS z U TECHNICAL NOTE No. 1790 INVESTIGATION OF ICING CHARACTERISTICS OF TYPICAL LIGHT-AIRPLANE ENGINE INDUCTION SYSTEMS By Willard D. Coles Lewis Flight Propulsion Laboratory Cleveland, Ohio .AL 'IBR. MANtJACTJ, U, -951 EULVEDA BlVD. LES. 45, LiL w77 Washington February 1949 NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS TECHNICAL NOTE NO. 1790 INVESTIGATION OF ICING CHARACTERISTICS OF TYPICAL LIGHT-AIRPLANE ENGINE INDUCTION SYSTE By Willard D. Coles SUMMARY The icing characteristics of two typical light-airplane engine induction systems were investigated using the carburetors and mani- folds of engines in the horsepower ranges from 65 to 85 and 165 to 185. The smaller system consisted of a float-type carburetor with an unheated manifold and the larger system consisted of a single- barrel pressure-type carburetor with an oil-jacketed manifold. Carburetor-air temperature and humidity limits of visible and serious Icing were determined for various engine power conditions. Several .methods of achieving ice-free induction systems are dis- cussed along with estimates of surface heating requirements of the various induct ion-system components. A study was also made of the icing characteristics of a typical light-airplane air scoop with an exposed filter and a modified system that provided a normal ram inlet with the filter located in a position to Induce inertia separation of the free water from the charge air. The principle of operation of float-type carburetors is proved to make them inherently more susceptible to icing at the throttle plate than pressure-type carburetors.. The results indicated that proper jacketing and heating of all parts exposed to the fuel spray can satisfactorily reduce or eliminate icing in the float-type carburetor and the manifold. -
Contents INTORDUCTION : Mankind‟S Journey Towards Powered Flight
Contents INTORDUCTION : Mankind‟s journey towards powered flight. .......................................................... 4 CHAPTER 1 : Reciprocating engines ................................................................................................... 6 1.1 Inline and V type engines............................................................................................................. 6 1.2 Radial engines ............................................................................................................................... 7 1.3 Carburators .................................................................................................................................... 9 1.4 Fuel injection .............................................................................................................................. 10 1.5The Diesel Aero engine ............................................................................................................... 11 CHAPTER2 : Jet engines ...................................................................................................................... 12 2.1The Turbojet Engine .................................................................................................................... 12 2.1.1 Development of Centrifugal and Axial turbojet engines ..................................................... 13 2.1.2Modern developments ........................................................................................................... 14 2.2Turboprop Engines ...................................................................................................................... -
AFM HBKMI.Pdf
Aircraft Flight Manual Doc. No. 2008/100 Ed. 2 - Rev. 1 2018, March 12th .-····-··-····-······--··\ : l :. ...~ •············~ · / 1 TECNAM P2008 JC MANlJF ACTURER: C. A. TECNAM S.r.l. AIRCRAFTMOD EL: P2008JC EASA T YPE CERTTFICATENR. : A .583 (DATED2013, 27 SEPTEMBER) SERJAL NUMBER: ....J.043 ............. B UILDYEAR: ......~ oJ.5 .......... REGISTRATION MARKINGS: ..qb.-~.~.8 ..1. ... .. This Aircrafl Flight Manual is approved and applies on/y to EASA CS-VLA certifled airplanes. This Manual must be carried in the airplane at all times. This aeroplane has to be operated in compliance with procedures and limitations contained herein. Costruzioni Aeronautiche TECNAM srl Via Maiorise CAPUA (CE) - Italy Tel. +39-0823 997538 WEB: www.tecnam.com SECTION 0 INDEX 1. RECORD OF REVISIONS .......................................................................................... 3 2 . LIST OF EFFECTIVE PAGES .................................................................................... 7 3. FOREWORD .............................................................................................................. 9 4. SECTIONS LIST ...................................................................................................... 10 Ed. 2, Rev. 0 Aircraft Flight Manual INDEX 1. RECORD OF REVISIONS Any revision to the present Manual, except actual weighing data, is recordecl: a Record of Revisions is provided in this Section and the operator is advised to make sure that the record iskepl up-to-date. Thc Manual issue is identificd by Edition and Revision codcs rcported on each page, lower right siele. The revision code is numerical and consists of the number "O"; subsequentrevi sions are identified by the change of the code from "O"to "1" for the firstrevision to the basic publication, "2" for the second one, etc. Should be necessary tocompletely reissue a publication for contents and format changes, the Edition code will change to the next number ("2" for the second edi tion, "3" for the third edition etc). -
Annual Safety Review 2021 Appendix 1
Appendix 1 - List of Fatal Accidents Annual Safety Review 2021 185 occurreNce rePorting rateS Appendix 1 List of fatal accidents Commercial air transport – airlines and air taxi – large aeroplanes Local Date State of Occurrence Location Aeroplane Headline 10/02/2011 Ireland Cork Apt EICK SWEARINGEN - SA227 - BC Impacted runway inverted. 11/11/2012 Italy Roma Fiumicino Airport AIRBUS - A320 Loading crew caught between loader and baggage door. Anti-icing system not activated by flight crew - Pressure sensor 24/07/2014 Mali 80 km south-east of Gossi DOUGLAS - DC9 - 80 - 83 obstructed by ice crystals. Aircraft stalled and crashed. UUWW (VKO): DASSAULT - FALCON 50 - Aircraft collided with a snowplough vehicle during take-off run. Aircraft 20/10/2014 Russian Federation Moskva/Vnukovo EX was destroyed by fire. First officer alone in the cockpit, initiated a rapid descent - Aircraft 24/03/2015 France Prads-Haute-Bléone AIRBUS - A320 - 200 - 211 impacted mountainous terrain. BOMBARDIER - CL600 IRU malfunction - Crew spatial disorientation - Loss of control - Aircraft 08/01/2016 Sweden Oajevágge 2B19 crashed on a mountainous terrain. Non-commercial complex business aeroplanes Local Date State of Occurrence Location Aeroplane Headline 10/12/2012 Cyprus Larnaca CESSNA - 750 - NO SERIES A service vehicle struck the right wingtip, vehicle driver trapped. EXISTS 29/04/2013 Congo, Democratic FZAA (FIH): Kinshasa/N'djili DASSAULT - FALCON 900EX Collision with an individual on ground. Republic of the 12/01/2014 Germany Near Trier-Föhren Airport CESSNA - 501 Aircraft collision against power pole. 03/10/2015 United Kingdom Near Chigwell BEECH - 200 - B200 Aircraft crashed shortly after take-off. -
'·~.; ·Resolution 66-1 Resolution 66-2
'·~.; ·Resolution 66-1 The MVPCB authorizes the Executive Officer to work with the U. S. P. H. Service in relation to survey grant funds for surveillance of 1966 model vehicles vquipped with exhaust controls. Resolution 66-2 The MVPCB u.nder Sec. 24390.(J) of the Health .and Safety Code is given authority to exempt motor vehicles whose emissions are found by appropriate tests to meet State standards without additiona1 equipment. Resolution 66-3 Citroen Cars, Inc. B~verly Hills, filed an application dated.1/6/66 for certification of a crankcase emission control system. · · Resolution 66-4 The Board requests appropriate legislative committees to continue and initiate studies in all areas appropriate to the conservation of the California air resource for consideration by the 1967 Regular . Legislative Session. · Resolution 66..5 .. _Brisko' s Mileage Saver, Inc, filed an application for a certificate · of approval for a crankcase emission control system on Feb. 26, 1966.• Resolution 66-6 Sec. 24386 (5) of the Health and Safety Code provides that the MVPCB · shall exempt classifications of vehicles from the mandatory provisions of the law. Resolution 66-7 Hereules Division of the Hupp Corp. filed an a.pplicat on for a certificate of approva;L for a crankcase emissions control system on Feb. 28, 1966. Resolution 66-8 Rover Motors. Co. Ltd., Solihull, England, filed an application for a certificate of approval for a closed crankcase emission control system. : · Resolution 66-9 · The Standard Screw Co., Cbicagci Division, filed an application for a certificate of approval for a crankcase emission control system. -
Tecnam P2008 Jc
Page 0 - 1 Aircraft Flight Manual Doc. No. 2008/100 Ed.1 – Rev. 0 2013, July 30th TECNAM P2008 JC MANUFACTURER: COSTRUZIONI AERONAUTICHE TECNAM S.r.l. AIRCRAFT MODEL:P2008 JC TH EASA TYPE CERTIFICATE NO: A .583 (DATED 2013, 27 SEPTEMBER) SERIAL NUMBER: ………….............. REGISTRATION MARKINGS: ………….……….. This Aircraft Flight Manual is approved by European Aviation Safety Agency (EASA) and applies only EASA CS-VLA certified airplanes. This Manual must be carried in the airplane at all times. The airplane has to be operated in compliance with procedures and limitations contained herein. Costruzioni Aeronautiche TECNAM srl Via Maiorise CAPUA (CE) – Italy Tel. +39 (0) 823 997538 WEB: www.tecnam.com Page 0 - 2 SECTION 0 INDEX 1. RECORD OF REVISIONS .......................................................................................... 3 2. LIST OF EFFECTIVE PAGES .................................................................................... 8 3. FOREWORD .............................................................................................................11 4. SECTIONS LIST ......................................................................................................12 Ed. 1, Rev. 0 Aircraft Flight Manual INDEX Page 0 - 3 1. RECORD OF REVISIONS Any revision to the present Manual, except actual weighing data, is recorded: a Record of Revisions is provided in this Section and the operator is advised to make sure that the record iskept up-to-date. The Manual issue is identified by Edition and Revision codes reported on each page, lower right side. The revision code is numerical and consists of the number "0"; subsequentrevi- sions are identified by the change of the code from "0" to "1" for the firstrevision to the basic publication, "2" for the second one, etc. Should be necessary tocompletely reissue a publication for contents and format changes, the Edition code will change to the next number (“2” for the second edi- tion, “3” for the third edition etc). -
New Product Announcements AERO 2017
New product announcements AERO 2017 New worldwide Allstar PZL Glider Sp. z o.o. sim+glide: innovative flightsimulator for gliders with 4 Stand: B5-137 axial motions www.szd.com.pl With sim+glide instruction and training of pilots will be in future - independent of weather - possible by day and night - Hedwigstr. 18 more cost efficient - promoting safetyness and rountine - 30159 Hannover enableing programms for specific types of gliders as well as Germany for cross-country and aerobatic flying The mobility with 4 Tel: +49 1704301254 axial motions makes it possible to simulate nearly each flight Fax: +49 511 441732 figure authentically. E-Mail: [email protected] Contact: Bernd Hager Company: Allstar PZL Glider Sp. z o.o. Internet: www.szd.com.pl 2017 1 / 16 Dacher Systems GmbH sky[nav]pro RedLine Box including FLARM for collsion Stand: A6-103 avoidance www.skynavpro.aero After introducing its BlueLine Satellite Box which offers in flight weather and real time tracking and monitoring at AERO Klärwerkstr. 1A 2016 in Friedrichshafen last year, Dacher Systems is now 13597 Berlin launching its RedLine Box, containing hardware to offer Germany collision avoidance with FLARM. Tel: +49 30-398009115 E-Mail: [email protected] Contact: Tiberius Dacher Company: Dacher Systems GmbH Internet: www.dacher-systems.de EWAK GmbH UGM 3644, new type of four-stroke engine Stand: A5 - 301 www.ewak-berlin.com Straße C 15345 Altlandsberg Germany Tel.: +49 176 81297645 E-Mail: [email protected] Contact: Sascha Manthey Company: EWAK GmbH Internet: www.ewak-berlin.com 2017 2 / 16 FernUniversität in Hagen Emergency Landing Assistant (ELA) Stand: FW-BP04 http://www.fernuni-hagen.de/rechnerarchitektur/fas.shtml The Department of Computer Architecture at the FernUniversität in Hagen (Prof.