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Type Certificate Holder Record Teledyne Continental Motors Ownership & Name Change As of April 19, 2011 (Continental Motors, Inc.)
DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION E-233 Revision 18 CONTINENTAL C75-8, -8F, -8FH, -8FHJ, -8FJ, -8J C75-12, -12F, -12FH, -12FHJ, -12FJ, -12J C75-12B, -12BF, -12BFH C75-15, -15F C85-8, -8F, -8FHJ, -8FJ, -8J C85-12, -12F, -12FH, -12FHJ, -12FJ, -12J C85-14F C85-15, -15F November 1, 2011 TYPE CERTIFICATE DATA SHEET NO. E-233 Engines of models described herein conforming with this data sheet (which is part of type certificate No. 233) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Civil Air Regulations provided they are installed, operated and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. Type Certificate Holder Continental Motors Mobile, Alabama 36601 Type Certificate Holder Record Teledyne Continental Motors Ownership & name change as of April 19, 2011 (Continental Motors, Inc.) Model C75-8 C75-12, -15 C85-8 C85-12, -14, -15 Type 4H0A - - - - - - Rating, ICAO or ARDC standard atmosphere Max. continuous hp., r.p.m., full throttle 75-2275 - - 85-2575 - - at sea level pressure altitude Takeoff hp., 5 min., r.p.m. full throttle at 75-2275 - - 85-2575 - - sea level pressure altitude (87-2650 for -J, -FHJ and -FJ models only) Fuel (min. grade aviation gasoline) 73 - - - - - - Lubricating oil, ambient temperature Oil Grade Below 40°F. SAE 20 - - - - - - Above 40°F. SAE 40 - - - - - - Bore and stroke, in. 4.062 x 3.625 - - - - - - Displacement, cu. in. 188 - - - - - - Compression ratio 6.3:1 - - - - - - Weight (dry), lb. -
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................................................................................................................................................................... -
This Photo Shows a 1935 Ford Station Wagon in Brigham City, Utah
www.earlyfordv8victoria.com P.O. Box 53517 Broadmead RPO Victoria, British Columbia V8X 5K2 This photo shows a 1935 Ford Station Wagon in Brigham City, Utah. Actually is the US Mail route Woodie. We think that’s Bruce Somers holding up the door! Page | 1 NOVEMBER 2019 TABLE OF CONTENTS: 1. Club Executive – contact information. 2. 2019 Club agenda & events. 3. Minutes. November 12th, regular club meeting. 4. Club news – updates, breaking news. 5. Tech talk – V8 members input, Q&A. Suggestions News. 6. Photos – Nostalgia EFV8 109, local and worldwide. 7. Buy & sell – parts, restorations, collections. Wanted dead or alive 8. Committees – contacts, functions, updates, help. 9. Fun page – caution, members contributing. 10. Miscellaneous – news and other interests. Contributions always appreciated The next regular club meeting will be held on January 14th , 2020 at Berwick House. 7:30 PM. 4062 Shelbourne St. CU there. Page | 2 NOVEMBER 2019 Early Ford V8 Club R.G. #109 2020 Position Name Telephone Email President Chris Chown 250 595 0312 [email protected] Vice President Mike Mortimer 250 477 0547 [email protected] Treasurer Jim Banks 250 433 4021 [email protected] Secretary Al Wills 250 474 4909 [email protected] Directors Dennis Mounce 250 478 6440 d&[email protected] Lauri Stevens 250 478 7565 [email protected] Chris Chown 250 595 0312 [email protected] Jim Jennings 250 477 5594 [email protected] Bill Pritchard 250 656 7029 [email protected] Don Landels 250 588 1300 [email protected] First Past Bill Pritchard 250 656 7029 [email protected] President Page | 3 NOVEMBER 2019 2019 Club Agenda & Events ACTIVITY AGENDA – January through December JAN 8 REGULAR CLUB MEETING 7:30 AT THE VICTORIAN JAN 19 CHRISTMAS PARTY SHAS Schoolhouse. -
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. -
DA+40+POH.Pdf
AIRPLANE FLIGHT MANUAL DA40 Airworthiness Category : Normal, Utility Requirement : JAR-23 Serial Number :40.698 Registration :N216DG , Doc. No. : 6.01.01-E Date of Issue : 26 June 2000 Signature Authority Stamp A-1 030 Wim, Sclmirchgassc 11 Date of approval 0 9. DEZ . Z.Oa4 This Flight Manuaj has been verified for EASA by the Austrian Civil Aviation Authority J Austro Control (ACG) as Primary Certification Authority (PCA) in accordance with the I valid Certifica1ion Procedures and approved by EASA with approval no ..2.004 :- A~3Zf, f This Flight Manual has been approved by EASA on behalf of CAAC-MD. DIAMOND AIRCRAFT INDUSTRIES GMBH N.A OTTO-STR. 5 A-2700 WIENER NEUSTADT A USTRIA page 0 - 0, R~v. 6 ~V/U~/UO mun U~:~O ~AA OD~ 0~/ ~~!U ~AA LAA~U ANM-lUUL ~3 ~011 AmSafe, Inc. Inflatable Restraints Division 1043 N. 47'" Avenue Phoenix, AZ., 85043 Document No.: E509609 r FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT to PILOT'S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL for Diamond Aircraft Industries, Inc. Model DA40 Aircraft Reg. No. N 2 16 DG Aircraft SIN: 4 0 • 6 9 8 This supplement must be attached to the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual for Diamond Aircraft Model DA 40 when the. Airplane Is modified by the installation of AmSafe Aviation Inflatable Restraint (AAIR,.) System, V23 Version in accordance with STC SA01918LA. The information contained herein supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement, consult c the basic Airplane Flight Manual. -
Air-Cooled Cylinders 1
Air-Cooled Aircraft Engine Cylinders An Evolutionary Odyssey by George Genevro Part 1 - From the Past Should aircraft engines be liquid-cooled or air-cooled? This “difference of opinion” is about a hundred years old and without a doubt the argument will continue as long as piston engines power the airplanes we fly. The manner in which the question is stated is misleading, however, since all waste heat that comes through the structure of an engine is eventually delivered to the air. In “liquid-cooled” engines the coolant can be water, ethylene glycol, a mixture of the two, or one of the many other liquids that have been tried and found wanting. Its primary purpose is to carry heat from the cylinder barrel and head to the radiator through which air, the actual cooling medium, flows. Proponents of liquid-cooling–now as in the past–can point to some benefits and operational advantages such as lessened hazard of shock cooling an engine, being able to direct dedicated coolant flow to critical areas in the cylinder head such as the exhaust valve seat and guide area, flexibility in radiator placement, greater structural rigidity in the engine, and having the option of designing airframes with a relatively small cross-sectional area that could still house a powerful engine. With every advantage, imagined or real, there is almost always a price to pay. Those who opted for liquid-cooled engines had to accept added weight, greater possibility of battle damage in military applications, and greater system complexity as the penalties. Such is life. -
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 - -
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. -
IN the UNITED STATES DISTRICT COURT for the EASTERN DISTRICT of PENNSYLVANIA CHARLES POWERS, on His Own : CIVIL ACTION Behalf An
Case 2:06-cv-02993-TJS Document 152 Filed 02/09/11 Page 1 of 31 IN THE UNITED STATES DISTRICT COURT FOR THE EASTERN DISTRICT OF PENNSYLVANIA CHARLES POWERS, on his own : CIVIL ACTION behalf and on behalf of the : class defined herein : NO. 06-2993 : v. : : LYCOMING ENGINES, a Division of : AVCO CORPORATION; AVCO : CORPORATION; and TEXTRON, INC. : PLANE TIME, LLC, on its own behalf and : CIVIL ACTION on behalf of others similarly situated : : NO. 06-4228 v. : : LYCOMING ENGINES, a Division of : AVCO CORPORATION; AVCO : CORPORATION; and TEXTRON, INC. : MEMORANDUM OPINION Savage, J. February 9, 2011 In these two consolidated putative nationwide class actions, we conduct a choice-of- law analysis and then re-evaluation of whether the plaintiffs have satisfied Rule 23's requirements for class certification. Moving for class certification under Fed. R. Civ. P. 23(b)(3), the plaintiffs seek to represent a class of owners or previous owners of aircraft equipped with engines designed and built by Lycoming Engines.1 They claim that the engines were manufactured with defective crankshafts that can cause a total loss of engine power and in-flight engine 1 The plaintiffs named three defendants, Lycoming Engines, Avco Corporation (“Avco”) and Textron, Inc. Since the motion for certification was filed, Textron has been dismissed. The two remaining defendants are referred to collectively as “Lycoming.” Case 2:06-cv-02993-TJS Document 152 Filed 02/09/11 Page 2 of 31 failures, and that Lycoming knew of and concealed the defect that prevents the crankshafts from functioning as intended. They seek damages for the cost to replace the defective crankshafts, which includes parts, labor, transportation, storage, insurance, the loss of the use of the aircraft while the crankshafts are being replaced and the diminished value of the aircraft. -
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. -
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 ............................................................................................................................................. -
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 ......................................................................................................................