AAIB Bulletin 5/2017
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Alone Across the Atlantic
® 8 - DECEMBER 2013 www.kitplanes.com RV Atlantic Across in an in Swage Fittings Swage Secure? Cables Your Are the Adventure FT A Alone T REVIEW H ’S GUIDE SHOP R E H Easy Fiberglass Prep Aerodynamic Bookworm Tire Changing 101 T Soaring on Homemade Wings 2014 BUYER’S GUIDE2014 ISSUE! N • • • I HP-24 FLIG HP-24 BUYE Over 350 Planes Listed! Planes 350 Over 2014 KIT AIRCR KITPLANES DECEMBER 2013 Kit Buyer’s Guide • Transatlantic RV-8 • HP-24 Sailplane • Design to Fit • Swagelocks • Dawn Patrol • Testing to DO-160 • Home Shop Machines BELVOIR PUBLICATIONS Enjoy the Freedom of Homebuilt Aircraft Weather the Storm with SkyView’s IFR Capabilities Redundant flight instruments that automatically cross-check each other • ADS-B traffic and weather in-flight • SkyView network modules that detect wiring faults without losing capability • Li-Ion backup batteries that keep your SkyView system up when the power goes down • Autopilot with fully coupled ILS and GPS WAAS/LPV approaches. SkyView should already be your IFR platform of choice. But if that’s not enough, SkyView 7.0 introduces geo-referenced instrument approach charts, airport diagrams, and the best mapping software we’ve ever built. Go Fly! www.DynonAvionics.com 425-402-0433 [email protected] Seattle,Washington December 2013 | Volume 30, Number 12 Annual Buyer’s Guide, Part 1 26 2014 KIT AIRCRAFT BUYER’S GUIDE: The state of the kit world is sound. By Paul Dye and Mark Schrimmer. 38 KIT AIRCRAFT QUICK REFERENCE: A brief overview of available kit aircraft for 2014. Compiled by Richard VanderMeulen and Omar Filipovic. -
A Doub Ly International LSA
Canadian-Designed Czech-Built Skylark A doub ly international LSA Story by Dan Johnson, photos by Jim Koepnick portsPlanes.com imports sev- Investigating the Skylark Skylark, but SportsPlanes.com com- eral light-sport aircraft (LSA) My opportunity to fly the Skylark pany pilots Dale Faux and Eric Del- that have found ready buy- came while attending the U.S. Sport lenbach, who is also SportsPlanes. ers. After researching through Aviation Expo in Sebring, Florida, in com’s national sales director, have Sseveral designs, SportsPlanes’ owner January. I flew with Darrell Hamil- wrung the plane out extensively. Josh Foss originally settled on the ton, the SportsPlanes representative Although the Skylark is a Czech- Comco Ikarus C42 and Breezer and for Florida. built LSA, it was designed by David the U.S.-built American Flyer for its Darrell retired from Northwest Marsden, a professor of aeronautical fleet. Most recently, the company Airlines four years ago. He most re- engineering at the University of Al- added the Czech-built Dova Skylark cently crewed the fly-by-wire Airbus berta in Edmonton, Canada. Marsden to its offerings. A320, which needs only small con- was able to use the university’s wind However, the real story of this com- trol movements. But he also piloted tunnel, a capability not available to pany is not Josh Foss’ care in the se- the Boeing 747 and, before that, the many LSA designers. After complet- lection of what airplanes to sell. What McDonnell-Douglas DC-9. The latter, ing the design work, Marsden enlist- may be more important to the mar- he said, took lots of control pressure ed Dova to be the manufacturer. -
POH C42 Series Issue-2 08.07.2013
PILOT OPERATING HANDBOOK for the aircraft IKARUS C 42 Series Modell Nr. C42 / C42B / C42C LTZ-Nr. 61141 / 61141.1 / 61141.5 Type IKARUS C 42 Series Airplane Registration No. __________________________ Airplane Serial-No. __________________________ Reference: POH C42 Series Issue-2 08.07.2013 This handbook is to be kept in the aircraft at all times. The described options of the C42 Series use are certified for Germany and have been tested in Germany. Please note that for using the C42 Series as a towplane for towing gliders, towing aerial signs or decanting sky divers, different regulations may apply in different countries. Please contact your local authorities for further clarification. POH C42 Series Issue-2 08.07.2013 Page 1 of 89 RECORD OF MANUAL REVISIONS No. Issue Description of Changes Date Signature No. 1 1 POH C42 Series 30.08.2012 A.Kurz 2 1 Introduction 06.01.2013 A.Kurz Instructions for the use of the 3 2 24.01.2013 A.Kurz LiFe-Battery Page 55, 63, 71 Note 4 2 08.03.2013 A.Kurz Authorization 5 2 3 Three side view 17.06.2013 A.Kurz Page 50 / 50 Hour Inspection 6 2 08.07.2013 A.Kurz delete POH C42 Series Issue-2 08.07.2013 Page 2 of 89 C42 Series Pilot Operating Handbook Manufacturer Contact Information COMCO IKARUS GmbH Am Flugplatz 11 88367 Hohentengen / Swabia Germany Tel: +49 7572 600 80 Fax: +49 7572 3309 Email: post@comco – ikarus.de Backup Certification Data Contact Information COMCO IKARUS GmbH Am Flugplatz 11 88367 Hohentengen / Swabia Germany Tel: +49 7572 600 80 Fax: +49 7572 3309 Email: post@comco – ikarus.de Owner ______________________________ ______________________________ ______________________________ This Pilot Operating Handbook belongs to the aircraft:_________________ and is to be kept in the aircraft at all times. -
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. -
March - April 2016
publication agreement number 40050880 March - April 2016 Recreational Aircraft Association Canada www.raa.ca The Voice of Canadian Amateur Aircraft Builders $6.95 From The features President’s Desk Glass or Steam: Traditional vs EFIS / JC Audet ..................................................................................................................4 Gary Wolf RAA 7379 Where Is Your Aero Centre? Aero Centre, Weight and Balance, and how it affects flight safety / Frank Gue .........................................8 Vans Rear Wing Spar Bulletin – Do exchange program. Rotax will act as a regional editor to source Man Was Meant To Fly Not ignore supply a kit of parts gratis, and the tech articles and lead stories from by Barry Meek ......................................................................................................................................11 Vans Aircraft has issued a “Before old parts must be returned. Labour the West. Please call the office at Further Flight” Service Bulletin will be reimbursed up to a maximum 800-387-1028 or email to garywolf@ Preciptiation near 0° Celcius 16-03-28 to alert pilots and builders of $550, and must be performed by a rogers.com . Karolina Utko........................................................................................................................................15 of the possibility of rear spar cracks Rotech approved Service Facility or in all models except the RV-12. by a Rotech approved Independent Lawrence Shaw Airspeed vs Angle of Attack The Bulletin describes -
Nigel Charles Looks at the Europa's Dramatically Changed, Graceful Performance with Motor-Glider Wings
FLIGHT TEST Europa XS Motorglider Nigel Charles looks at the Europa’s dramatically changed, graceful performance with motor-glider wings Photos Andrea Featherby Europa XS Motorglider t has been 18 years since I first saw the he recognised that the requirement for long, straightforward design idea for the main wheel, Europa prototype at the PFA Rally at tarmac runways (readily available in the USA) was but his idea to use the flaps to retract the Wroughton. I think I knew almost a handicap in Europe. The UK, for example, has outriggers (like the Harrier jump jet) was a stroke immediately that the Europa was going to be over 500 airfields with runways over 400m but of genius. From this concept the design of the Isomething special. Kit aircraft at that stage were in only about 125 of these offer hard surface monowheel Europa was born. their infancy and we were at a point where runways. He quickly came to the conclusion that The Rotax 912 four-stroke engine had been modern technologies such as composite materials there was demand for an aircraft that could handle available for a while and was proving to be a and lightweight engines were encouraging farm strips and at the same time cruise at a rugged and economical source of power. Ivan innovation. With the help of the LAA (PFA as it reasonable speed while avoiding consuming large based the design around this engine and, despite was known then) a number of kitplane volumes of avgas. attempts by some to use other powerplants, the manufacturers brought their ideas to the The problem was that tyres with a large Rotax stands out as the powerplant of choice marketplace. -
Maintenance Manual Ikarus C42 Series Issue VIII Rev. 1 4.2.1 Periodic Inspections
4.2.1 Periodic inspections Aircraft type: ____________________ Date of inspection: __________________ Call-sign: ____________________ Serial no.: __________________ No. of flight hours ____________________ Inspection Ref. every Signature No. Description every Chapter 50 100 hours hours 1 Clean the aircraft x x 3 Engine cowling Check condition of engine cowling and its attachments; repair 2 x x damage as required Engine 3 Maintenance in accordance with Rotax manual in accordance with Rotax manual Engine compartment Visual inspection of integrity of fire protection mats: 4 - at the fire wall x x - at the push-rods for the nose wheel steering Engine mount Check condition of engine mount, particularly the rivet connections 5 x x and attachment screws; check security of screws Visual inspection of integrity of heat-resistant silicon sealings at the transitions: - engine mount - fuselage tube 6 x x - engine mount - nose wheel spar - nose wheel spar - fuselage tube - fuselage tube - A column Visual inspection of engine damper blocks for porosity, excessive 7 deformation, cracks, etc.; if necessary, replace affected blocks (the x engine must not be removed) Carburettor Visual inspection of carburettors, especially: - air filter connections - fuel line connections 8 x x - equalising line connections - attachment of throttle cables - attachment of choke cables 9 - check carburettor supports for cracks x Check Bowden cables at their exit at the adjustment screws for wear 10 x x 4.3.1.1 and grease them; adjust if necessary (synchronisation) Check condition and attachment of air tubes between carburettor and 11 x x 4.3.1.2 induction system (pressure sensors in the air filters) Maintenance Manual Ikarus C42 Series 57 of 103 Issue VIII Rev. -
Europa Classic Trigear Conversion to an Experimental Amateur Built Light
Europa Classic Trigear Conversion to an Experimental Amateur Built Light Sport Aircraft (EABLSA) by use of Vortex Generators normally used for STOL Modifications Testing Dates 3 January 2010 thru 15 September 2010 Test Aircraft: N12AY Europa Classic Kit Power plant: Rotax 914 Propeller: Warp Drive three blade 64 inch wide chord This test was conducted to determine the feasibility of modifying a Europa Classic or XS kit aircraft to Light Sport Aircraft (LSA) standards. Experience has shown that the Europa kit aircraft is an efficient comfortable cruising aircraft with pleasing lines and superb flight characteristics. Many LSA aircraft are limited in cruise speed, strength, efficiency and comfort, which the Europa is not. The criteria for an aircraft to meet LSA, is in Ref 1 at the end of this document. Aerodynamically, the Europa wing is capable of generating a 1.7 Cl. Simple solution of the lift equation indicates the aircraft should stall at approximately 49 Knots for the XS and 53 for the Classic allowing for the slight differences in wing area. The LSA criteria set for the by the Federal Aviation Authority (FAA) calls for a controllable stall at 45 KIAS. My experience with adding vortex generators (VGs) to the Zenith and Piper Aircraft for STOL operations showed that a full length set of VGs, properly placed can lower the stall speed 5- 8 knots. The application of VGs should bring the stall speed of the Europa down to just meet the criteria listed in Ref 1. Since the maximum continuous power setting of the 914 is 73.5 KW or 95 HP the next problem is achieving a propeller setting that will absorb the power but limit the Europa to 120 Kts IAS cruise at sea level. -
Aircraft Design
Optimal Aircraft Design Aircraft Design D.Breyne Dernière révision 06/11/19 2017 - 2019 Réservé uniquement aux enseignants et élèves de l’Ecole Centrale Paris Reproduction interdite www.oad.aero 1/79 Optimal Aircraft Design Objectives One of the main objectives of this session is to present the design process of an aircraft and more precisely the conceptual design. The other objective is to be aware that is possible to define very quickly the main size of the aircraft only working with order of magnitude. The class will be divided in different groups of three students. Each group will represent the research department of one company. A customer (the teacher) will present to the groups a set of specifications and will ask the groups to fulfil the conceptual design of the corresponding aircraft. The conceptual design will be done using a software (ADS). With this tool, it will be easier to consider the aircraft as a whole and visualize the impact of one technical choice on the whole aircraft: its size, its performance and its cost. At the end of the session, each group will present its work to the customer, in front of the class. www.oad.aero 2/79 Optimal Aircraft Design Table of contents Objectives ............................................................................................................................................... 2 Table of contents .................................................................................................................................... 3 Bloc 1 ...................................................................................................................................................... -
November 2014 23.60
THE MAGAZINE OF THE LIGHT AIRCRAFT ASSOCIATION www.laauk.com NOVEMBER 2014 23.60 • • • • •••• • • •• MA • • •• • • •• " • • • •• • Light Aircraft Association New catalogue now in production - call to reserve your copy today! LA 1::"•411,1 INSTRUMENTS & HARDWARE IOW jk Jaa IS SOS i"U 11FaltM° \Irri "Au iprown CIF c7la 4,fr s'`VALVES SEALANTS & BATTERIES COMPOUNDS *1-3Ea RAW MATERIALS LUBRICANTS PAINTS , DOPES & FABRICS -4i 4`• ' s WINDOWS & TOOLSQ3/41"1"'s411.111411'1, WINDSHIELDS LIGHTS, LAMPS & FILAMENTS INHCF I C pcRRAKFC CONTROL CABLES TYRES ALLtSSLIKIt 41k HOSE & BOOKS .„,--3\ firDUCTING \Pi 414; cel` 117 FILTERS root. a - I a EDITOR'S DESK azahlos Aid Acieg zed ••• •- msYOURASSOCIATION Tell us how you think the AGM should be run — your input really is valued sympathy for those who have forked opt sometimes quite considerable (1 November) and I hope we will have had a reasonable sums ot money fo ensure teat have the right lief/foe. raring or business B attendance.y the time you It read has thisnever we been will have much had of aour 'must AGM do at event Sywell for the arrangement (for schools and instructors/ only to find that the outlay majority of members but it is important because it reiterates that this is wasn't absotutely necessary . an association. our association, and we do have a say in how it is run. Tge feature article this month is Roy Taylor's lovely Bowers Fly Baby. I can say already that there will have been more members' input this an early plans built 'vintage type that unfortunately wasn't popular here year because the response to the drive to get the proxy voting system in the UK but was widely embraced in its native US Roy had previously better understood and used has resulted in around 60 responses as of a built, and still Hes. -
C42 Owner's Manual
C42 Owner’s Manual OHB/C42/001 Issue 16 C42 Owner’s Manual (Microlight) Page 1 C42 Owner’s Manual FLIGHT, OPERATION AND MAINTENANCE MANUAL This Manual belongs to aircraft reg: X-XXXX X_X Type: IKARUS C42 Serial No: xxxx-xxxx Series Build Aircraft Microlight Aircraft Types: IKARUS C42 A & Bravo FB80, C42 FB100 Type Approval Data Sheet (TADS) No. BM 68 Manufacturer: Red Aviation Hangar 6 Wolverhampton Halfpenny Green Airport Bobbington Stourbridge West Midlands DY7 5DY Tel. +44 (0)1384 221600 Email: [email protected] Web: www.red-aviation.com CAA Company Approval No DAI/9953/15 This handbook should be kept with the aircraft. CONTENTS Page CONTENTS ............................................................................................................................................................................... 3 ISSUE AMENDMENTS ............................................................................................................................................................. 4 Preamble ................................................................................................................................................................................ 5 SECTION 1 - AIRFRAME AND ENGINE LIMITATIONS........................................................................................................ 6 SECTION 2 - OPERATIONAL LIMITATIONS ......................................................................................................................... 9 SECTION 3 - OPERATION OF THE POWERPLANT.......................................................................................................... -
Microlight Accident and Incident Summary 0 /201
Microlight Accident and Incident Summary 03/2011 This accident report summary is collated by the BMAA from information gathered. The information sources used are the Air Accident Investigation Branch of the Department for Transport (AAIB), the Civil Aviation Authority Mandatory Occurrence Reports (CAA MOR) and reports made directly to the BMAA by members and operators. The individual reports within the accident summary are taken from the information available to the BMAA and where the BMAA has made comment this is clearly shown. The BMAA does not investigate accidents and incidents, this role being the responsibility of the AAIB and the CAA who have the expertise, experience and funding for investigation. All pilots reading the reports should try to make their own assessment of underlying causes and use the experience of others to enhance their own knowledge to help them become safer pilots. AAIB Bulletin: 1/2011 EW/G2010/09/22 ACCIDENT Aircraft Type and Registration: Ikarus C42 FB80 No & Type of Engines: 1 Rotax 912-UL piston engine Year of Manufacture: 2005 Date & Time (UTC): 21 September 2010 at 1400 hrs Location: Type of Flight: Training Persons on Board: Crew - 1 Passengers - None Injuries: Crew - None Passengers - N/A Nature of Damage: Significant damage to forward fuselage and right wing Commander’s Licence: Student pilot Commander’s Age: 53 years Commander’s Flying Experience: 40 hours (of which 40 were on type) Last 90 days - 6 hours Last 28 days - 6 hours Information Source: Aircraft Accident Report Form submitted by the pilot The student pilot was undertaking a solo flight from edge marker and applied full power.