A 120-Hp Turbo Kit for the Rotax 912 Sociation, Inc
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“Bob” Hoover IAC’S 2009 Hall of Fame Inductee
JANUARY 2010 OFFICIALOFFICIAL MAGAZINEMAGAZINE OFOF TTHEHE INTERNATIONALI AEROBATIC CLUB R.A. “Bob” Hoover IAC’s 2009 Hall of Fame Inductee • The IAC turns 40 • The Doug Yost Scholarship PLATINUM SPONSORS Northwest Insurance Group/Berkley Aviation Sherman Chamber of Commerce GOLD SPONSORS Aviat Aircraft Inc. The IAC wishes to thank Denison Chamber of Commerce MT Propeller GmbH the individual and MX Aircraft corporate sponsors Southeast Aero Services/Extra Aircraft of the SILVER SPONSORS David and Martha Martin 2009 National Aerobatic Jim Kimball Enterprises Norm DeWitt Championships. Rhodes Real Estate Vaughn Electric BRONZE SPONSORS ASL Camguard Bill Marcellus Digital Solutions IAC Chapter 3 IAC Chapter 19 IAC Chapter 52 Lake Texoma Jet Center Lee Olmstead Andy Olmstead Joe Rushing Mike Plyler Texoma Living! Magazine Laurie Zaleski JANUARY 2010 • VOLUME 39 • NUMBER 1 • IAC SPORT AEROBATICS CONTENTS FEATURES 6 R.A. “Bob” Hoover IAC’s 2009 Hall of Fame Inductee – Reggie Paulk 14 Training Notes Doug Yost Scholarship – Lise Lemeland 18 40 Years Ago . The IAC comes to life – Phil Norton COLUMNS 6 3 President’s Page – Doug Bartlett 28 Just for Starters – Greg Koontz 32 Safety Corner – Stan Burks DEPARTMENTS 14 2 Letter from the Editor 4 Newsbriefs 30 IAC Merchandise 31 Fly Mart & Classifieds THE COVER IAC Hall of Famer R. A. “Bob” Hoover at the controls of his Shrike Commander. 18 – Photo: EAA Photo Archives LETTER from the EDITOR OFFICIAL MAGAZINE OF THE INTERNATIONAL AEROBATIC CLUB Publisher: Doug Bartlett by Reggie Paulk IAC Manager: Trish Deimer Editor: Reggie Paulk Senior Art Director: Phil Norton Interim Dir. of Publications: Mary Jones Copy Editor: Colleen Walsh Contributing Authors: Doug Bartlett Lise Lemeland Stan Burks Phil Norton Greg Koontz Reggie Paulk IAC Correspondence International Aerobatic Club, P.O. -
Team Oracle 2018 Media Kit
TEAM ORACLE 2018 MEDIA KIT SOARING ON IN THE ORACLE CHALLENGER III For media flights, interviews, photos & video: Suzanne Herrick, Fedoruk & Associates, Inc., 612-247-3079 [email protected] PHOTO BY Mike Killian Follow Sean D. Tucker at: facebook.com/SeanDTucker instagram.com/TeamOracle twitter.com/SeanDTucker & twitter.com/TeamOracle The Team Oracle Airplane Channel on YouTube FASTEN YOUR SEAT BELTS AND HOLD ON TIGHT. IT’S TIME FOR SOME HEART-CHARGING, HIGH-PERFORMANCE POWER AEROBATICS FROM THE LEGEND HIMSELF, MR. SEAN D. TUCKER. THE 2018 TEAM ORACLE AIR SHOW SEASON IS UNDERWAY, FILLED WITH AWE-INSPIRING MOMENTS, THRILLS AND ADRENALINE. This season marks Tucker’s last as a solo performer with exciting plans in store for a performance team. If you haven’t had the opportunity to interview Tucker or better yet, experience flight with Team Oracle, this is the year. Contact Suzanne Herrick at 612-247-3079 or [email protected] for times and options. PHOTO BY Peter Tsai SOARING WITH THE DREAM MACHINE • More than half of Tucker’s power aerobatic maneuvers are unique making Tucker’s performance an unforgettable, awe-inspiring experience. • During the 13-minute Sky Dance performance, Tucker will pull more than nine positive g-forces and more than seven negative g-forces. • The Sky Dance begins with a breathtaking three-quarter loop with eight to 10 snap rolls in which Tucker reaches speeds up to 280 miles per hour at more than 400 degrees per second and six positive g-forces. • Tucker is the world’s only pilot to perform the Triple Ribbon Cut in which he flies just 20 feet above the ground, cutting ribbons on poles placed a mere 750 feet apart. -
FLASHBLACK Instruction Manual
Instruction manual Variable pitch propellers in flight FLASHBLACK FLASHBLACK Tractor Pusher BLACK Tractor Aérodrome de Villefranche Tarare (LFHV) 289 Avenue Odette & Edouard DURAND 69620 FRONTENAS - FRANCE Phone: + 33 (0)4 74 72 12 69 - Fax: +33 (0)4 74 72 10 01 ISO 9001:2015 Certified Company E-mail: [email protected] - www.DUC-helices.com for its Quality System Management DH_FSH-PV_BE_02_F Made in France 04/12/2018 Revision update Date Index Object of modification 23/07/2014 A Creation 20/07/2017 F Add SWIRLBLACK-3 & TBO update 11/12/2017 F Minor correction 10/04/2018 F English language correction 04/12/2018 F Minor change in page 42 This instruction manual is to be maintained throughout the life of the propeller. He may have to evolve. The owner must check with the DUC Hélices Company the latest version being valid applicable to the propeller. Identification Date Delivery note n° Engine/Gearbox Owner ratio Aircraft Pitch range Min: Max: Notes: .............................................................................................................................................................................. .......................................................................................................................................................................................... .......................................................................................................................................................................................... ......................................................................................................................................................................................... -
Looking After Your Rotax 912 Series Engine
LOOKING AFTER YOUR ROTAX 912 SERIES ENGINE Most of the things you wanted to know about servicing a Rotax 912/914 series aircraft engine but were afraid to ask…. By Conrad Beale Copyright ConAir Sports Ltd. All rights reserved. Page 1 of 20 Most of the things you wanted to know about servicing a Rotax 912/914 series aircraft engine but were afraid to ask…. By Conrad Beale This article has been written by Conrad Beale of ConAir Sports Ltd. It is intended to help you look after your 912 series engine. It is in no way endorsed by Rotax. All information contained here in may be subject to change without notice. It does not substitute, override or in any way replace the information given in the Installation / Maintenance or Operators Manuals or any subsequent documentation issued by Rotax. The intention of this article is to assist the many Rotax 4 stroke engine owners, operators and engineers to carry out the work necessary to prolong the life of their Rotax 912/914 series aircraft engines. This article will touch on a number of subjects and will hopefully clear up some of the common questions we get asked. Some areas will be covered in detail, others less so. I hope it covers everything sufficiently. I have been involved with Rotax engines for 25+ years, 18 of which have been working commercially on Rotax aircraft engines. 8 years ago I set up ConAir Sports Ltd with my wife Louise and we are the only UK Skydrive appointed Service Centre for Rotax Aircraft Engines. -
ENGINE TYPE 914 | 115 Hp (UL/F) AIRCRAFT ENGINES
ENGINE TYPE 914 | 115 hp (UL/F) AIRCRAFT ENGINES DESCRIPTION • 4-cylinder • 4-stroke liquid/air-cooled engine with opposed cylinders • with turbo charger • with automatic waste gate control • dry sump forced lubrication with separate oil tank • automatic adjustment by hydraulic valve tappet • 2 carburetors • dual electronic ignition • electric starter • propeller speed reduction unit • engine mount assembly • air intake system • exhaust system FACTS The turbo charged Rotax 914 series offers more performance at high altitudes while keeping weight at a low level. This series offers a time between overhauls of 2.000 hrs and is available as certified (Rotax 914 F) according to FAR 33 and JAR-E and non-certified version (Rotax 914 UL). ENGINE DATA WEIGHT kg lb engine with propeller speed reduction unit i = 2,43 64.0 140.8 exhaust system 4.0 8.8 engine suspension frame 2.0 3.7 overload clutch 1.7 3.7 external alternator 3.0 6.6 air guide hood 0.8 1.8 VERSION PERFORMANCE TORQUE MAX RPM kW ft. lb. 1/min Nm ft. lb. 1/min 1/min 914 UL1)/F2) 84.5 115 5800 144 106 4900 5800 Limited for max. 5 min. BORE STROKE DISPLACEMENT FUEL min. MON 85 RON 95* 79.5 mm 3.13 in 61 mm 2.4 in 1211.2 cm3 73.91 cu. in. min. AKI 91* * leaded or unleaded or AVGAS 100LL 1) UL = non certified 2) F = certified acc. to ARF 33 and JAR-E Picture: 914 UL - DCDI with options WWW.FLYROTAX.COM ® and TM are trademarks of BRP-Rotax GmbH & Co. -
Rotax Service Interval Guide Not New News, but a Very Informative Summary
Rotax Service Interval Guide Not new news, but a very informative summary With growing numbers of 912 & 914 series engines in service these days Rotax have gathered a great deal of field experience and have been continually updating the maintenance procedures. Operators of 912 & 914 series engines can obtain current maintenance manuals free of charge, (yep I did say FREE) from the Rotax aircraft engines web site www.rotax-aircraft-engines.com – just click on the documentation tab & fill in the relevant search boxes to obtain the documents you require. You will find parts lists, line & heavy maintenance manuals, service bulletins, operator’s manuals, installation manuals, and a whole host of information you may not have known about. The system is not perfect, for example parts lists for early engines are not available, but it is pretty good & full of useful documentation. We do find that some Rotax owners find the documentation difficult to interpret and occasionally miss things - agreed it can be difficult to see the wood through the trees, especially after translation. As the maintenance & overhaul information has changed over the last couple of years it’s probably a good time to have a recap on how things are now. So before the flying season gets too busy why not take the opportunity to make sure your engine is ready for the new flying season – I’m assured its going to be a good one this year! Figure 1: Documentation page of the Rotax Aircraft Engines website (www.rotax-aircraft-engines.com) MAINTENANCE SCHEDULES The alterations to the maintenance schedules over the years have mainly been to reduce the work required and the parts replaced, so should you want to save a few pennies in these difficult times you better read on. -
Carburetor Synchronization
Carburetor Synchronization With the proliferation of the Rotax 912 80 hp and the Rotax 912S 100 hp engines, the topic of carburetor synchronization has come to the forefront. Until about the 1980s, the popularity of Continental and Lycoming engines dominated the general aviation market, these engines used a single carburetor providing for a single source of air and fuel to the cylinders. The use of dual carburetors was primarily relegated to the area of the two-stroke ultralight market. And, even with these engines, the process of carburetor synchronization was quite simple and reliable. How- ever, with the popularity of the Rotax 9 series engines, it has become import- ant to under- stand a little bit more about how the induc- tion system works on this amazing little powerhouse. This understand- ing is important not only from a maintenance standpoint, but from a pilot’s per- spective as well. The Rotax 912 is essentially two engines connected to a single crankshaft and gearbox with both Figure: 1 The Rotax 912 is two separate engines connected to a common crankshaft the left and right sides of the engine having their own independent carburetor, ignition, and exhaust sys- tem Figure: 1. As you might well imagine, having two engines trying to run a single propeller requires a bit of choreography between the right and left side of the en- gine in order to make things run smoothly. Most of us, who have spent a consider- able amount of time in the air, can remember a time when one of the cylinders on a four-cylinder engine just quit firing, maybe from fouled spark plugs, or a plugged fuel Figure: 2 Clamping off the crossover (Balance) hose injector. -
The Drive to Outperform
2018 ANNUAL REVIEW FOR THE YEAR ENDED JANUARY 31, 2018 THE DRIVE TO OUTPERFORM FINANCIAL HIGHLIGHTS FISCAL YEAR 2018 REVENUE BASE REVENUE BASE BY CATEGORY BY REGION AT 31/01/18 AT 31/01/18 40.8% 34.8% 15.7% 8.7% 50.5% 32.2% 17.3% YEAR-ROUND SEASONAL PARTS, ACCESSORIES PROPULSION UNITED STATES INTERNATIONAL CANADA PRODUCTS PRODUCTS AND CLOTHING SYSTEMS SHARE PRICE MONTHLY CLOSING PRICE IN CA$ $50.86 JANUARY 2018 $26.03 FEBRUARY 2017 MARCH APRIL MAY JUNE JULY AUGUST SEPTEMBER OCTOBER NOVEMBER DECEMBER TOTAL NORMALIZED NORMALIZED RESEARCH AND REVENUES EBITDA1 EARNINGS PER DEVELOPMENT CA$ MILLIONS, CA$ MILLIONS, SHARE – DILUTED1 SPENDING AT 31/01/18 AT 31/01/18 CA$, AT 31/01/18 IN CA$ MILLIONS + AS A % OF REVENUES CAGR* 9% CAGR* 10% CAGR* 12% 3,194 3,525 3,829 4,172 4,487 380.2 421.3 460.0 502.7 558.6 1.49 1.65 1.71 1.96 2.38 145 + 4% 158 + 4% 164 + 4% 184 + 4% 199 + 4% 14 15 16 17 18 14 15 16 17 18 14 15 16 17 18 14 15 16 17 18 1 See Non-IFRS measures section on p.15. * Compound Annual Growth Rate since 31 January 2014 LETTER TO SHAREHOLDERS FOR FISCAL YEAR 2018 – JOSÉ BOISJOLI THE DRIVE TO OUTPERFORM I am very pleased with the strong financial results we delivered once again, featuring another year of record revenues, continuing our steady positive performance since we became a public company five years ago. We are now three years into our ambitious 2020 plan and remain focused on our strategic priorities of Growth, Agility and Lean enterprise to reach our target: the $6 billion mark and $3.50 diluted earnings per share by fiscal year 2021. -
Diesel, Spark-Ignition, and Turboprop Engines for Long-Duration Unmanned Air Flights
JOURNAL OF PROPULSION AND POWER Diesel, Spark-Ignition, and Turboprop Engines for Long-Duration Unmanned Air Flights Daniele Cirigliano,∗ Aaron M. Frisch,† Feng Liu,‡ and William A. Sirignano‡ University of California, Irvine, California 92697 DOI: 10.2514/1.B36547 Comparisons are made for propulsion systems for unmanned flights with several hundred kilowatts of propulsive power at moderate subsonic speeds up to 50 h in duration. Gas-turbine engines (turbofans and turboprops), two- and four-stroke reciprocating (diesel and spark-ignition) engines, and electric motors (with electric generation by a combustion engine) are analyzed. Thermal analyses of these engines are performed in the power range of interest. Consideration is given to two types of generic missions: 1) a mission dominated by a constant-power requirement, and 2) a mission with intermittent demand for high thrust and/or substantial auxiliary power. The weights of the propulsion system, required fuel, and total aircraft are considered. Nowadays, diesel engines for airplane applications are rarely a choice. However, this technology is shown to bea very serious competitor for long-durationunmanned air vehicle flights. The two strongest competitors are gas-turbine engines and turbocharged four-stroke diesel engines, each type driving propellers. It is shown that hybrid-electric schemes and configurations with several propellers driven by one power source are less efficient. At the 500 KW level, one gas-turbine engine driving a larger propeller is more efficient for durations up to 25 h, whereas several diesel engines driving several propellers become more efficient at longer durations. The decreasing efficiency of the gas-turbine engine with decreasing size and increasing compression ratio is a key factor. -
European Aviation Safety Agency
European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Number : E.121 Issue : 06 Date : 17.06.2014 Type : Rotax 912 series engines Models Rotax 912 A1 Rotax 912 A2 Rotax 912 A3 Rotax 912 A4 Rotax 912 F2 Rotax 912 F3 Rotax 912 F4 Rotax 912 S2 Rotax 912 S3 Rotax 912 S4 Rotax 912 iSc2 Sport Rotax 912 iSc3 Sport List of effective Pages: Page 1 2 3 4 5 6 7 8 9 10 11 12 13 Issue 6 6 6 6 6 6 6 6 6 6 6 6 6 TCDS EASA.E.121 Rotax 912 series engines page 2/13 Issue 06, 17 June 2014, models: 912 A1, A2, A3, A4, F2, F3, F4, S2, S3, S4, iSc2 Sport, iSc3 Sport Intentionally left blank TCDS EASA.E.121 Rotax 912 series engines page 3/13 Issue 06, 17 June 2014, models: 912 A1, A2, A3, A4, F2, F3, F4, S2, S3, S4, iSc2 Sport, iSc3 Sport I - General 1. Type / Models: Rotax 912/ Rotax 912 A1, Rotax 912 A2, Rotax 912 A3, Rotax 912 A4, Rotax 912 F2, Rotax 912 F3, Rotax 912 F4, Rotax 912 S2, Rotax 912 S3, Rotax 912 S4, Rotax 912 iSc2 Sport, Rotax 912 iSc3 Sport 2. Type Certificate Holder: Since March 15, 2014 BRP-Powertrain GmbH & Co KG Rotaxstraße 1 A-4623 Gunskirchen, Austria DOA EASA.21J.048 Before March 15, 2014 BRP-Powertrain GmbH & Co KG Welser Straße 32 A-4623 Gunskirchen, Austria DOA EASA.21J.048 Before February 3, 2009 BRP-Rotax GmbH & Co KG Welser Straße 32 A-4623 Gunskirchen, Austria DOA EASA.21J.048 Before June 16, 2004 Bombardier-Rotax GmbH & Co KG Welser Straße 32 A-4623 Gunskirchen, Austria Before December 29, 2001 Bombardier-Rotax Gesellschaft mbH Welser Straße 32 A-4623 Gunskirchen, Austria 3. -
Carb Ice: the Threat and the Theory
independent SERVICE CENTRE AIRCRAFT ENGINES Part # 44 Carb Ice: The Threat And The Theory 8. Inversion layers may exist whereby icing conditions are more in evidence than lower down, so we can climb by Mike Stratman with plenty of power and suddenly experience icing in an inversion. In the East inversions can be any height in a high pressure system (clear cool day). In a low with Dennis Pagen pressure system inversions don’t usually occur, but plenty of humidity abounds so icing can be a problem. Throttling back from cruise you set up a long glide to In the West, inversions are more likely due to local ef- your home field in the distance. As you descend you can fects and terrain allowing different layers of air to move feel the air change temperature as you pass into a new into an area. Whether or not these inversions present inversion layer. The air is now cool and moist. After several an icing problem depends on where the air mass origi- minutes the engine starts to lose rpm, you increase the nates. The generally drier air in the West reduces the throttle setting without a response. The engine begins to problem greatly. run rough and shake. You work the throttle furiously to no 9. Ice forms for two reasons: drop in temperature due to avail. Despite your best efforts the engine quits. Have you the drop in pressure in the venturi (about a 5 degree just been a victim of Carb Ice? drop in temp) and due to evaporation of gasoline as For years the debate on the facts and fiction surround it mixes with air (this drop can be 60F or more) The Carb Ice in Rotax engines has raged. -
Brp-Powertrain
BRP profile BRP is a world leader in the design, manufacturing, distribution, and marketing of motorized recreational vehicles and powersports engines. BRP sets the pace in the industry with high-performance engines that power the world of motor sports. We refine the optimum every day for more fun and more personal safety. Built on a 70-year tradition of excellence and headquartered in the Canadian town of Valcourt, Québec, BRP operates manufacturing facilities in Canada, the United States, Mexico, Finland and Austria, and has a total workforce of about 7,600 passionate people. BRP products are sold in more than 107 countries around the world. Our internationally recognized product lines include BRP overview • SKI-DOO® and LYNX® (snowmobiles) Name: Bombardier Recreational Products Inc. (BRP) • SEA-DOO® (watercraft) Headquarters: Valcourt, Québec (Canada) • EVINRUDE® (outboard engines) Employees: 7,600 worldwide • CAN-AM® (ATVs, side-by-side vehicles, and Spyder roadsters) Manufacturing Sites: Canada, USA, Mexico, Finland, Austria • ROTAX® (engines, transmissions) Ownership: Shares are traded on the Toronto Stock Exchange under the symbol „DOO“ ROTAX the power to excite Over 90 years in the powertrain industry and going strong, Rotax® engines are the heart and soul of countless products. BRP‘s Austrian facility oversees the worldwide development and production of Rotax engines. In fact, BRP has developed more than 350 engine models for recreational products and produced over 7 million engines. Rotax engines are renowned for their maximum performance, light weight, compactness, fuel efficiency, longevity and reliability. Rotax powertrains with its gearbox and transmission technologies multiply the benefits of the engines by a smart and comfortable transfer of power to the track.