AAIB Bulletin 3/2015

Total Page:16

File Type:pdf, Size:1020Kb

AAIB Bulletin 3/2015 AAIB Bulletin 3/2015 TO REPORT AN ACCIDENT OR INCIDENT PLEASE CALL OUR 24 HOUR REPORTING LINE 01252 512299 Air Accidents Investigation Branch Farnborough House AAIB Bulletin: 3/2015 Berkshire Copse Road Aldershot GLOSSARY OF ABBREVIATIONS Hants GU11 2HH aal above airfield level lb pound(s) ACAS Airborne Collision Avoidance System LP low pressure Tel: 01252 510300 ACARS Automatic Communications And Reporting System LAA Light Aircraft Association ADF Automatic Direction Finding equipment LDA Landing Distance Available Fax: 01252 376999 AFIS(O) Aerodrome Flight Information Service (Officer) LPC Licence Proficiency Check Press enquiries: 0207 944 3118/4292 agl above ground level m metre(s) http://www.aaib.gov.uk AIC Aeronautical Information Circular mb millibar(s) amsl above mean sea level MDA Minimum Descent Altitude AOM Aerodrome Operating Minima METAR a timed aerodrome meteorological report APU Auxiliary Power Unit min minutes ASI airspeed indicator mm millimetre(s) ATC(C)(O) Air Traffic Control (Centre)( Officer) mph miles per hour ATIS Automatic Terminal Information System MTWA Maximum Total Weight Authorised ATPL Airline Transport Pilot’s Licence N Newtons BMAA British Microlight Aircraft Association N Main rotor rotation speed (rotorcraft) AAIB investigations are conducted in accordance with R BGA British Gliding Association N Gas generator rotation speed (rotorcraft) Annex 13 to the ICAO Convention on International Civil Aviation, g BBAC British Balloon and Airship Club N1 engine fan or LP compressor speed EU Regulation No 996/2010 and The Civil Aviation (Investigation of BHPA British Hang Gliding & Paragliding Association NDB Non-Directional radio Beacon CAA Civil Aviation Authority nm nautical mile(s) Air Accidents and Incidents) Regulations 1996. CAVOK Ceiling And Visibility OK (for VFR flight) NOTAM Notice to Airmen CAS calibrated airspeed OAT Outside Air Temperature cc cubic centimetres OPC Operator Proficiency Check The sole objective of the investigation of an accident or incident under these CG Centre of Gravity PAPI Precision Approach Path Indicator Regulations is the prevention of future accidents and incidents. It is not the cm centimetre(s) PF Pilot Flying CPL Commercial Pilot’s Licence PIC Pilot in Command purpose of such an investigation to apportion blame or liability. °C,F,M,T Celsius, Fahrenheit, magnetic, true PNF Pilot Not Flying CVR Cockpit Voice Recorder POH Pilot’s Operating Handbook DFDR Digital Flight Data Recorder PPL Private Pilot’s Licence Accordingly, it is inappropriate that AAIB reports should be used to assign fault DME Distance Measuring Equipment psi pounds per square inch or blame or determine liability, since neither the investigation nor the reporting EAS equivalent airspeed QFE altimeter pressure setting to indicate height EASA European Aviation Safety Agency above aerodrome process has been undertaken for that purpose. ECAM Electronic Centralised Aircraft Monitoring QNH altimeter pressure setting to indicate EGPWS Enhanced GPWS elevation amsl EGT Exhaust Gas Temperature RA Resolution Advisory EICAS Engine Indication and Crew Alerting System RFFS Rescue and Fire Fighting Service EPR Engine Pressure Ratio rpm revolutions per minute ETA Estimated Time of Arrival RTF radiotelephony ETD Estimated Time of Departure RVR Runway Visual Range FAA Federal Aviation Administration (USA) SAR Search and Rescue FIR Flight Information Region SB Service Bulletin FL Flight Level SSR Secondary Surveillance Radar ft feet TA Traffic Advisory AAIB Bulletins and Reports are available on the Internet ft/min feet per minute TAF Terminal Aerodrome Forecast http://www.aaib.gov.uk g acceleration due to Earth’s gravity TAS true airspeed GPS Global Positioning System TAWS Terrain Awareness and Warning System GPWS Ground Proximity Warning System TCAS Traffic Collision Avoidance System hrs hours (clock time as in 1200 hrs) TGT Turbine Gas Temperature HP high pressure TODA Takeoff Distance Available hPa hectopascal (equivalent unit to mb) UHF Ultra High Frequency IAS indicated airspeed USG US gallons IFR Instrument Flight Rules UTC Co-ordinated Universal Time (GMT) This bulletin contains facts which have been determined up to the time of compilation. ILS Instrument Landing System V Volt(s) IMC Instrument Meteorological Conditions V Takeoff decision speed Extracts may be published without specific permission providing that the source is duly acknowledged, the material is 1 IP Intermediate Pressure V Takeoff safety speed reproduced accurately and it is not used in a derogatory manner or in a misleading context. 2 IR Instrument Rating VR Rotation speed ISA International Standard Atmosphere V Reference airspeed (approach) Published 12 March 2015 Cover picture courtesy of Richard Ross REF kg kilogram(s) VNE Never Exceed airspeed © Crown copyright 2015 ISSN 0309-4278 KCAS knots calibrated airspeed VASI Visual Approach Slope Indicator KIAS knots indicated airspeed VFR Visual Flight Rules Published by the Air Accidents Investigation Branch, Department for Transport KTAS knots true airspeed VHF Very High Frequency Printed in the UK on paper containing at least 75% recycled fibre km kilometre(s) VMC Visual Meteorological Conditions kt knot(s) VOR VHF Omnidirectional radio Range AAIB Bulletin: 3/2015 CONTENTS SPECIAL BULLETINS / INTERIM REPORTS None SUMMARIES OF AIRCRAFT ACCIDENT (‘FORMAL’) REPORTS None AAIB FIELD INVESTIGATIONS COMMERCIAL AIR TRANSPORT FIXED WING None ROTORCRAFT None GENERAL AVIATION FIXED WING Yak-52 G-YAKR 29-Mar-14 3 ROTORCRAFT None SPORT AVIATION / BALLOONS None AAIB CORRESPONDENCE INVESTIGATIONS COMMERCIAL AIR TRANSPORT Airbus A320-232 G-TTOB 18-Dec-14 15 Boeing 737-8JP(WL) LN-DYS 23-Dec-14 17 GENERAL AVIATION DA 42 Twin Star G-CTCF 02-Dec14 19 Denney Kitfox Mk 2 G-KITY 19-Nov-14 21 Pietenpol Air Camper G-ECVB 23-Jul-14 23 Piper PA-28-161 Cherokee Warrior II G-BFYM 30-Dec-14 25 Piper PA-28-181 Cherokee Archer II G-TALE 01-Nov-14 26 SPORT AVIATION / BALLOONS Ikarus C42 FB100 G-FLYC 02-Jan-15 28 Pegasus Quik G-CBVN 30-Nov-14 30 Pegasus XL-Q G-MWOY ∫ ∫ 19-Nov14 31 P&M Aviation QUIK GT450 G-CEGJ Team Minimax G-MYRG 06-Dec-14 33 © Crown copyright 2015 i AAIB Bulletin: 3/2015 CONTENTS Cont MISCELLANEOUS ADDENDA and CORRECTIONS Reims Cessna F172P Skyhawk G-BITM 27-Sep-14 37 Sikorsky S-76C G-WIWI 03-May-12 38 List of recent aircraft accident reports issued by the AAIB 39 (ALL TIMES IN THIS BULLETIN ARE UTC) © Crown copyright 2015 ii AAIB Bulletin: 3/2015 AAIB Field Investigation reports A field investigation is an independent investigation in which AAIB investigators collect, record and analyse evidence. The process may include, attending the scene of the accident or serious incident; interviewing witnesses; reviewing documents, procedures and practices; examining aircraft wreckage or components; and analysing recorded data. The investigation, which can take a number of months to complete, will conclude with a published report. © Crown copyright 2015 1 AAIB Bulletin: 3/2015 G-YAKR EW/C2014/03/04 ACCIDENT Aircraft Type and Registration: Yak-52, G-YAKR No & Type of Engines: 1 Ivchenko Vedeneyev M-14P piston engine Year of Manufacture: 1989 (Serial no: 899803) Date & Time (UTC): 29 March 2014 at 1453 hrs Location: Near Highwood, Chelmsford, Essex Type of Flight: Private Persons on Board: Crew - 1 Passengers - 1 Injuries: Crew - 1 (Fatal) Passengers - 1 (Fatal) Nature of Damage: Aircraft destroyed Commander’s Licence: Airline Transport Pilot’s Licence Commander’s Age: 50 Commander’s Flying Experience: in excess of 15,000 hours1 (of which approximately 40 hours2 were on type) Last 90 days - 1 hour Last 28 days - 1 hour Information Source: AAIB Field Investigation Synopsis The aircraft was carrying out a local flight when, five minutes into the flight, it was observed flying at low level. Having carried out a level turn, the aircraft climbed sharply and entered a stall or spin, from which it did not recover before striking the ground. Both occupants received fatal injuries and there was a fire. The reason the aircraft was flying at low level and the cause of the final manoeuvre could not be determined. History of the flight The pilot, who was one of three co-owners of the aircraft, arrived at North Weald mid-morning and prepared for a short local flight. He had not made an arrangement to take anyone with him, until he met someone at the airfield and offered him the opportunity to fly as a passenger. Following pre-flight preparations, some of which were witnessed by onlookers at the flying club, the aircraft’s engine was started and at 1439 hrs the pilot booked out by radio for a “TWENTY MINUTE LOCAL FLIGHT”. The aircraft taxied for departure from Runway 02 and took off Footnote 1 No up-to-date log books were available; the total hours stated is taken from the pilot’s medical declaration in October 2013. 2 Flight records for G-YAKR were audited but did not match records kept of movements at North Weald; time on type is derived from information on an insurance application in March 2013 adjusted to reflect some recent flying. © Crown copyright 2015 3 AAIB Bulletin: 3/2015 G-YAKR EW/C2014/03/04 at 1447 hrs. Following an apparently normal takeoff run, the aircraft lifted off and climbed before turning on course towards the east. The AFISO last saw the aircraft climbing away from the airfield, above 1,000 ft aal. In the pilot’s final communication to the AFISO, at 1448 hrs, he reported that he was “VACATING TO THE EAST”. No further transmissions from the pilot were heard. Primary radar returns show that the aircraft then flew a predominantly easterly track. Although the aircraft was fitted with a transponder which, according to the other co-owners, was serviceable, no secondary radar responses from the aircraft were recorded. Therefore, there was no height information. The aircraft’s track included a left and then right turn, which were co-incident with the position of a small airfield.
Recommended publications
  • Zulassungen Aktuell
    Eidgenössisches Departement für Umwelt, Verkehr, Energie und Kommunikation UVEK Bundesamt für Zivilluftfahrt Luftfahrtentwicklung Annex II Propellerflugzeuge, Motorsegler und Tragschrauber bis 8'618kg MTOM Mühlestrasse 2, 3096 Bern (Schweiz) Telefon +41 31 325 8039/40 Fax +41 31 325 9212 FOCA Noise Annex II/ 17.03.2020 Seite 1 von 35 Flugzeughersteller Motor Propellerhersteller Start- / Dauer- MTOM [kg] Pegel Grenzwert Geb.- Muster Schalldämpfer Muster Leistung [kW] Prop.- Kap.6 / Kap. 10 Kap.6 / Kap. 10 klasse [dB(A)] [dB(A)] Start- / Dauer- durchm. [m] Drehz. [1/min] Aeronca Aircraft Corporation Continental A-65-8 Sensenich / 567 /D63.8 / 76.0 11AC Univair J-3 Exhaust System 74CK-0-74 2300 / 2300 1.88 Alisport Srl. Alisport Srl. A302efi Alisport Srl. / 300 /D59.9 / 65.0 Silent II Original Monoplana 2045 / 2045 1.41 Alisport Srl. LZ Design D.O.O. EFI LZ Design D.O.O. 22.0 / 22.0 313.5 /D65.0 / 65.0 Silent II electro EFI-SIL-P15-100 4500 / 4500 1 noise level set to limit American Champion Aircraft Corp Continental C-90-8F Sensenich / 66.8 554 61.9 /68.0 / 76.0 D 7AC M76AK-2-46 / 2475 1.88 American Champion Aircraft Corp Continental O-200-A McCauley / 74.9 748 66.0 /70.0 / 79.1 C 7ECA Andere 1A100/ACM6948 / 2650 1.75 American Champion Aircraft Corp Lycoming O-320-A2B McCauley / 111.4 750 68.0 /70.0 / 79.1 C 7GCB Frankfurter 1A170/7448 / 2700 1.88 American Champion Aircraft Corp Rolls-Royce O-200-A MT-Propeller / 612 66.5 /68.2 / 76.3 B 7AC CONV MT 178R 110-2C / 2490 1.78 Auster Lycoming O-290-D2 McCauley / 100.3 840 71.6 /71.2 / 80.8 A
    [Show full text]
  • BRP the Company Overview at BRP, We Believe That Passion and Innovation Moves the Powersports World
    AIRCRAFT ENGINES POWERFUL LIGHT EFFICIENT www.flyrotax.com BRP THE COMPANY OVERVIEW At BRP, we believe that passion and innovation moves the powersports world. We are a world leader in the design, manufacturing, distribution and marketing of NAME motorized recreational vehicles and power sports engines. Bombardier Recreational Products Inc. (BRP) Built on a 70-year tradition of excellence and head- HEADQUATERS quartered in the Canadian town of Valcourt, Québec, Valcourt, Québec (Canada) BRP owns manufacturing facilities in Canada, the United States, Mexico, Finland and Austria and has a total EMPLOYEES workforce of about 6.000 passionate people. 6.000 worldwide BRP products are distributed in more than 100 countries MANUFACTURING SITES by over 5.000 dealers and distributors. Austria, Canada, USA, Mexico, Finland Our internationally recognized product lines include: OWNERSHIP - Ski-Doo and Lynx (snowmobiles) 50 % Bain Capital, 35 % Bombardier Family, - Sea-Doo (watercraft boats) 15 % Caisse de dépôt et placement du Québec - Evinrude and Johnson (outboard engines) - Can-Am (ATVs/quads, Side-by-side vehicles and roadsters) - Rotax (engines) BRP-POWERTRAIN THE DIVISION Decades of experience, a top workforce and leading research: engines manufactured by BRP-Powertrain are the driving force – within the corporate group and for Austria as a business location. BRP-Powertrain sets the pace in its industry. High-performance engines power the world of motor sports. Refining the optimum every day for more fun and fewer emissions. Engines produced by BRP-Powertrain set global benchmarks in the industry: maximum performance with a light weight and high fuel efficiencies, low noise and reduced emissions, longevity and reliability are what characterize the engines.
    [Show full text]
  • Bmaa Technical Information Leaflet (Til) Til 069 Issue 2
    BMAA TECHNICAL INFORMATION LEAFLET (TIL) TIL 069 ISSUE 2 SERIES MAJOR MODIFCATIONS 1. Introduction BMAA major modifications that have been both well defined by the original applicant and for which quality control procedures have been put in place are defined as ‘series’ modifications. Subsequent applicants apply for these in the same way as for ‘one-off’ BMAA modifications (using form BMAA/AW/002a), but do not need to provide a technical justification. Notes: o Series modifications must be identical to the first approval; if there is any change or non-compliance with respect to the original MAAN then a new approval is required. o Note that BMAA ‘series’ major modifications may not be applied for with a Permit revalidation application. This is because a Flight Release Certificate has to be issued and then signed by a BMAA Inspector. o BMAA 'series' major modifications are now charged at a reduced rate (compared to ‘one-off’ modifications). A list of existing BMAA 'series' modifications can be found below. 2. Existing BMAA Series Major Modifications The table below contains a list of issued BMAA ‘Series’ Major Modifications (up to January 2021 / MAAN 2864). The ‘Type(s)’ and ‘Brief description’ are indicative only; the BMAA Technical Office should be consulted prior to applying for the modification to confirm the details of the modification. MAAN Issue Type(s) Brief description 1001 1 Pathfinder Intro of 2.3:1 and 2.86:1 reduction drive ratios 1002 2 130SX/Halfpint E Rotax 337 and Newton 2-blade, 54" x 42.5" prop 1061 2 Hornet Duel Trainer Raven 45 litre plastic fuel tank 1066 1 Goldwing Intro Nicklow 2.86:1 reduction and Romain 2-blade 58" x 34" prop 1069 2 Goldwing Installation of Konig SC430 radial engine with Catto 56"X 28" prop 1076 1 Raven-X 3-blade Ivoprop, 62"x 9deg to Rotax 447.
    [Show full text]
  • Österreichische Gesellschaft Für Zivilluftfahrt Mbh the Austrian Civil Aviation Administration
    Österreichische Gesellschaft für Zivilluftfahrt mbH The Austrian Civil Aviation Administration T I T E L B L A T T Muster-Kennblatt Nr.: UA 003/89 Ausgabe Datum Nr. Grundmuster: Ikarus C 22 5 23.11.1995 Baureihe: Ikarus C 22B 5 23.11.1995 Ikarus C 22C 1 30.07.2001 Dokumentennummer: TD AOT ACE 003 v5.0 (Musterkennblatt UA 003/89) Österreichische Gesellschaft für Zivilluftfahrt mbH The Austrian Civil Aviation Administration Allgemeines Ultraleicht-Musterkennblatt Nr.: UA 003/89 Ausgabe Nr.: 5 Datum: 23.11.1995 Musterbezeichnung: Ikarus C 22 Daten des Grundmusters UL-Baumuster: Ikarus C 22 Hersteller: COMCO GesmbH. Tannenweg 20 Aidlingen / Deutschland Bauvorschriften: Betriebstüchtigkeitsforderungen für Ultraleicht- Flugzeuge des DaeC und des DULV vom Oktober 1984 Antragsteller auf Musterprüfung: COMCO GesmbH. Tannenweg 20 Aidlingen / Deutschland Technische Merkmale und Betriebsgrenzen Baumerkmale: Einmotoriger, zweisitziger dreiachsgesteuerter abgestrebter Hochdecker mit tragender Struktur aus AL-Rohren und Profilbildung der Tragflächen und Leitwerke aus Kunststoffgeweben, Dreibein- Bugfahrwerk, Motor vorne an Rumpfröhre montiert; Kreuzleitwerk. Abmessungen: Flügelspannweite 10,46 m Flügelfläche 15,70 m² Länge 5,60 m Triebwerk: 1. 2 Zylinder, 2-Takt Drehschieber-Reihenmotor, flüssigkeitsgehkühlt, stehend montiert mit Untersetzungsgetriebe 3 : 1 Hersteller: Rotax Type: 462 UL Start- und Dauerleistung: 38 kW (52 PS) bei 6500 1/min Höchstzulässige Drehzahl: 6800 1/min 2. Ausführung mit Doppelzündung und 2 Vergasern; 40 kW; Untersetzungsgetriebe 3,5 : 1 Type: 582 UL Start- und Dauerleistung: 40 kW (53,6 PS) bei 60001/min Dokumentennummer: TD AOT ACE 003 v5.0 (Musterkennblatt UA 003/89) Höchstzulässige Drehzahl: 64001/min Muster: Ikarus C 22 Kennblatt-Nr.: UA 003/89 Ausgabe-Nr.: 5 - 2 - Luftschraube: zu Rotax 462 UL: 1.
    [Show full text]
  • 912 ULS/S | 100 Hp Engine Facts
    AIRCRAFT ENGINES POWERFUL LIGHT EFFICIENT www.flyrotax.com BRP THE COMPANY OVERVIEW At BRP, we believe that passion and innovation moves the powersports world. We are a world leader in the design, manufacturing, distribution and marketing of NAME motorized recreational vehicles and power sports engines. Bombardier Recreational Products Inc. (BRP) Built on a 70-year tradition of excellence and head- HEADQUATERS quartered in the Canadian town of Valcourt, Québec, Valcourt, Québec (Canada) BRP owns manufacturing facilities in Canada, the United States, Mexico, Finland and Austria and has a total EMPLOYEES workforce of about 6.000 passionate people. 6.000 worldwide BRP products are distributed in more than 100 countries MANUFACTURING SITES by over 5.000 dealers and distributors. Austria, Canada, USA, Mexico, Finland Our internationally recognized product lines include: OWNERSHIP - Ski-Doo and Lynx (snowmobiles) 50 % Bain Capital, 35 % Bombardier Family, - Sea-Doo (watercraft boats) 15 % Caisse de dépôt et placement du Québec - Evinrude and Johnson (outboard engines) - Can-Am (ATVs/quads, Side-by-side vehicles and roadsters) - Rotax (engines) BRP-POWERTRAIN THE DIVISION Decades of experience, a top workforce and leading research: engines manufactured by BRP-Powertrain are the driving force – within the corporate group and for Austria as a business location. BRP-Powertrain sets the pace in its industry. High-performance engines power the world of motor sports. Refining the optimum every day for more fun and fewer emissions. Engines produced by BRP-Powertrain set global benchmarks in the industry: maximum performance with a light weight and high fuel efficiencies, low noise and reduced emissions, longevity and reliability are what characterize the engines.
    [Show full text]
  • 066-070 LAA Sept08 26/08/2008 3:08 Pm Page 67
    066-070_LAA_Sept08 26/08/2008 3:07 pm Page 66 Classifieds For all display or commercial advertising AIRCRAFT FOR SALE enquiries please call our Advertising Manager Victoria Griffiths on +44 (0) 1223 497068 or email [email protected] You can email your classified DYN-AERO MCR01 CLUB. Excellent advertisement direct to the LAA condition, completed 2005, permit to at the following address: TWO SEAT VERSION OF CURRIE July 2009. 110hrs TTE/AF. Rotax 912S [email protected] WOT. Fantastic open cockpit fun with with PV50 CS prop. Comprehensive Next issue: August 2008 new aerobatic LAA permit. Zero timed panel inc. Txpdr (C), horizon, EIS, fuel Deadline for booking and copy: 14th July 2008 Lycoming O-320 (150 HP) engine and computer. Always hangared. Great per- formance, handling and economy £52k. Classified advertising rates full recent aircraft overhaul Only two owners from new. Selling after 10 year View at Branscombe E Devon. £15 per single column cm (one-off) affair due to limited time! A fraction of tel: 01404 871599 £13 per single column cm (Series of six) £10 per single column cm (Series of 12) the price of a Pitts or Skybolt at £16,950 e-mail [email protected] or without engine for £9,950 Contact Display advertising rates Ian Hannah on 0773 960 0421 or Full page cover position £1500 [email protected] EMERAUDE CP301A Continental C90 14F. Full page £1100 TTAF and engine 1400hrs. Permit until April Half page £600 Quarter page £350 ARV SUPER 2. As new. 10 hours airframe, 0 09.
    [Show full text]
  • Civil Aviation Authority – Safety Regulation Group Microlight Type Approval Data Sheet (Tads) No: Bm43 Issue: 10 Tads Bm43 I
    CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM43 ISSUE: 10 TYPE: Mainair Mercury (1) MANUFACTURER: Mainair Sports Ltd now supported by P & M Aviation Ltd, Unit B, Crawford Street Rochdale, Lancashire, OL16 5NU. (2) UK IMPORTER: N/A (3) CERTIFICATION: BCAR Section S, Advance Issue March 1983 BCAR Section S, Paper, 11 October 1988 (4) DEFINITION OF 440 Dual Master List of Drawings, Issue 7 BASIC STANDARD: Flash Wing Master Drawing List, Issue 6 (5) COMPLIANCE WITH THE MICROLIGHT DEFINITION (a) MTOW 370 kg (b) No. Seats 2 (c) Maximum Wing Loading 23.78 kg/m² (d) Vso 24 kts (25 mph) (e) Permitted range of pilot weights 55 – 90 kg per seat. (f) Typical Empty Weight (ZFW) (Mercury 503) 146kg (Mercury 462) 150kg (Mercury 582) 153kg (g) ZFW + 172 kg crew + 1 hr fuel (503) 333kg (litres / kg) (426) 341 kg (582) 343 kg (h) ZFW + 86 kg pilot + full fuel (503) 264 Kg [279 kg ( litres / kg) with mod 99] (462) 268kg [283 kg with mod 99] (582) 271 kg [286 kg with mod 99] (i) Max ZFW at initial permit issue (503) 183 Kg (462) 179 kg (582) 180 kg TADS BM43 Issue 10 Page 1 of 13 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM43 ISSUE: 10 (6) POWER PLANTS Mercury 503 Mercury 503 Mercury 503 Mercury 462 Mercury 462 Mercury 462 Designation Engine Type Rotax 503 Rotax 503 Rotax 503 Rotax 462 Upright Rotax 462 Upright Rotax 462 Upright Upright Upright Upright Single Points Ign Single Points Ign Single Points Ign or Twin Electronic or Twin Electronic or Twin Electronic Ign.
    [Show full text]
  • Repair Manual 462-532-582 Rev.0 10/1994
    Repair Manual for engine type 462 - 532 - 582 UL Edition: 10 1994 Bombardier-Rotax GmbH 4623 GUNSKIRCHEN Telefon: (0)7246/271-0* Welser Strasse 32 Telefax: (0)7246/370 recommended ATS 900,-- FOR INFORMATION ONLY. price: WITHOUT COMMITMENT TO ADVISE MODIFICATIONS. Part no: 899 081 Table of contents 1) Introduction:.................................................................................................................. 6 1.1) Engine number: ............................................................................................................................. 6 1.2) General notes: ............................................................................................................................... 7 2) Technical data: ............................................................................................................. 8 2.1) Technical data ROTAX engine type 462 UL: .............................................................................. 8 2.2) Technical data ROTAX engine type 532 UL: ............................................................................ 10 2.3) Technical data ROTAX engine type 582 UL: ............................................................................ 12 3) Tools and supplementary means: ........................................................................... 15 3.1) Standard tools: ............................................................................................................................15 3.2) Special service tools for the engine: .......................................................................................
    [Show full text]
  • Rotax Hovercraft Et Aircraft Engin Es
    TABLE DES MATIERES 1 AVANT PROPOS ....................................................................................................................... 1 1.1 NUMEROTAT ION DES MOTEURS ...................................................................... 2 1.2 NOTES GENERALES ...................................................................................... 2 2 CARACTERJSRQUES TECHNIQUES ..................................................................................... 3 2.1 MOTEURS TYPE 462 UL ............................................................................................ 3 2.2 MOTEURS TYPE 532 UL ..................................................................................... 5 2.3 MOTEURS TYPE 582 UL ............................................................... .. .................... 7 3 OUTILLAGES ET INGREDIENTS ...........................................................................................11 3.1 OUTILLAGE STANDARD .................................................................................. 11 3.2 OUTILLAGES SPECIAUX .................................................................................12 3.3 OUTILLAGES SPECIAUX POUR REDUCTEURS "A" et "B" .................................15 3.4 OUTILLAGES SPECIAUX POUR REDUCTEUR "Cu .......................................... 16 3.5 INGREDIENTS ET PRODUITS DIVERS ............................................................... 17 4 INSTALLATION DU MOTEUR ...............................................................................................
    [Show full text]
  • 7 TADS BM4 Issu
    CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM4 ISSUE: 7 TYPE: Gemini Flash (1) MANUFACTURER: Mainair Sports Ltd now supported by P & M Aviation Ltd. Unit B, Crawford Street, Rochdale, Lancashire, OL16 5NU. (2) UK IMPORTER: N/A (3) CERTIFICATION: BCAR Section S, Advance Issue March 1983 BCAR Section S, Paper, 11 October 1988 (4) DEFINITION OF 440 Dual Master List of Drawings, Issue 7 BASIC STANDARD: Flash Wing Master Drawing List, Issue 5 (5) COMPLIANCE WITH THE MICROLIGHT DEFINITION (a) MTOW 344 kg (pre Mod 21A) 370 kg (post Mod 21A) (b) No. Seats 2 (c) Maximum Wing Loading 23.92 kg/m² (d) Vso 24 kts (25 mph) (e) Permitted range of pilot weights 55 – 90 kg per seat. (f) Typical Empty Weight (ZFW) (Flash 440) 145kg (Flash 447) 145kg (Flash 503) 145kg (Flash 462) 145kg (g) ZFW + 172 kg crew + 1 hr fuel (440) 337kg (litres / kg) (447) 328 kg (503) 332 kg (462) 336 kg (h) ZFW + 86 kg pilot + full fuel (440) 263 Kg ( litres / kg) (447) 263 kg (503) 263 kg [278 kg with mod 99] (462) 263 kg [278 kg with mod 99] (i) Max ZFW at initial permit issue 178 Kg TADS BM4 Issue 7 Page 1 of 13 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM4 ISSUE: 7 (6) POWER PLANTS Gemini Flash 440 Gemini Flash 440 Gemini Flash 447 Gemini Flash 447 Gemini Flash 447 Gemini Flash 447 Designation Engine Type Fuji Robin Fuji Robin Rotax 447 Inverted Rotax 447 Inverted Rotax 447 Upright Rotax 447 Upright EC44PN EC44PN Upright Inverted Reduction Gear 2.67:1 2.67:1 2.58:1 2.58:1 2.58:1 2.58:1 Exhaust System Rota Flow Rota Flow Rotax 2 x 90 Rotax 2 x 90 Rotax Side Rotax Side Underslung Underslung Underslung Underslung Mounted Mounted Intake System Unique Foam Unique Foam Rotax Intake Rotax Intake Rotax Intake Rotax Intake Muffler Muffler Muffler Muffler Muffler Muffler Propeller Type Mainair Sports Mainair Sports Newton Mainair Sports Mainair Sports Mainair Sports Round Tip Round Tip Propeller Dia x Pitch 62” x 30” 62” x 30” 62” x 38” 62” x 37” 62” x 35” 62” x 40” Noise Type Cert No.
    [Show full text]
  • Microlight Type Approval Data Sheet BM 23 Issue 14
    CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM23 ISSUE: 14 TYPE: Gemini Flash 2 Alpha (1) MANUFACTURER: Mainair Sports Ltd now supported by P & M Aviation Ltd., Unit B, Crawford Street Rochdale, Lancashire, OL16 5NU. (2) UK IMPORTER: N/A (3) CERTIFICATION: BCAR Section S, Advance Issue March 1983 BCAR Section S, Paper, 11 October 1988 (4) DEFINITION OF 440 Dual Master List of Drawings, Issue 7 BASIC STANDARD: Flash Wing Master Drawing List, Issue 5 (5) COMPLIANCE WITH THE MICROLIGHT DEFINITION (a) MTOW 370 kg (b) No. Seats 2 (c) Maximum Wing Loading 23.78 kg/m² (d) Vso 24 kts (25 mph) (e) Permitted range of pilot weights 55 – 90 kg per seat. (f) Typical Empty Weight (ZFW) (Alpha 503) 149kg (Alpha 462) 149kg (Alpha 503-2V) 151kg (Alpha 582) 157kg (g) ZFW + 172 kg crew + 1 hr fuel (503) 336kg (litres / kg) (426) 340 kg (503-2V) 338 kg (582) 347 kg TADS BM23 Issue 14 Page 1 of 15 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM23 ISSUE: 14 (h) ZFW + 86 kg pilot + full fuel (503) 267 Kg [290 kg ( litres / kg) with mod99] (462) 267 kg [292 kg with mod99] (503-2V) 269 kg [292 kg with mod99] (582) 275 kg [298 kg with mod99] (i) Max ZFW at initial permit issue (503) 183 kg (462) 179 kg (503-2V) 183 kg (582) 180 Kg TADS BM23 Issue 14 Page 2 of 15 CIVIL AVIATION AUTHORITY – SAFETY REGULATION GROUP MICROLIGHT TYPE APPROVAL DATA SHEET (TADS) NO: BM23 ISSUE: 14 (6) POWER PLANTS Gemini Flash 2 Gemini Flash 2 Gemini Flash 2 Gemini Flash 2 Gemini Flash 2 Gemini Flash 2 Gemini Flash 2 Designation Alpha 503 Alpha 503 Alpha 503 Alpha 462 Alpha 462 Alpha 462 Alpha 462 Engine Type Rotax 503 Rotax 503 Rotax 503 Rotax 462 Upright Rotax 462 Upright Rotax 462 Upright Rotax 462 Upright Upright Upright Upright Single Points Ign Single Points Ign Single Points Ign or Twin Electronic or Twin Electronic or Twin Electronic Ign.
    [Show full text]
  • Contents Contents
    AAIB Bulletin: 11/2013 CONTENTS SPECIAL BULLETINS / INTERIM REPORTS None AAIB FIELD INVESTIGATIONS COMMERCIAL AIR TRANSPORT FIXED WING None ROTORCRAFT None GENERAL AVIATION FIXED WING Grob G115E Tutor G-BYUB 23-Aug-12 ∫ ∫ 3 Grob G115E Tutor G-CGKC 09-Jan-13 ROTORCRAFT None SPORT AVIATION / BALLOONS None AAIB CORRESPONDENCE INVESTIGATIONS COMMERCIAL AIR TRANSPORT DHC-8-402 Dash 8 G-FLBD 01-Jun-13 11 Short SC7 Skyvan 3 G-BEOL 03-May-13 13 GENERAL AVIATION Cirrus SR22 N450CD 05-Apr-13 15 Gulfstream AA-5B Tiger G-BJAJ 02-Jun-13 17 Jodel D117A G-BEDD 10-Jul-13 18 Jodel D120A Paris-Nice G-BICR 29-Aug-13 20 Lancair 320 G-FOPP 16-May-13 21 Minicab (JB01 Standard) G-AWEP 06-Jul-13 22 Pietenpol Air Camper G-DAYZ 12-Jul-13 25 Pioneer 300 Hawk G-OHJE 06-Jul-13 26 Piper J3C-65 Cub G-BTET 31-Aug-13 28 Piper PA-28R-180 Cherokee Arrow G-OKAG 29-Jul-13 29 Piper PA-28-161 Cherokee Warrior II G-BOHA 17-Jul-13 31 © Crown copyright 2013 i AAIB Bulletin: 11/2013 AAIB CORRESPONDENCE INVESTIGATIONS Cont GENERAL AVIATION Cont Pitts S-1S G-EEPJ 10-Aug-13 33 Pitts S-1T Special G-WILD 31-Mar-13 35 Tecnam P2002-JF Sierra G-UFCM 25-Jul-13 38 Valentin Taifun 17E D-KFIH 11-Aug-13 40 W.A.R. FW190 (replica) G-SYFW 19-Jul-13 42 Yak-52 G-STNR 23-Aug-13 44 SPORT AVIATION / BALLOONS Cosmik Aviation EV-97 Eurostar G-CEHL 09-Aug-13 45 EV-97 Eurostar G-CDNI 03-May-13 47 EV-97 TeamEurostar UK G-CFNW 14-Aug-13 48 Gemini Flash IIA G-MVXB 13-Jul-13 49 Kolb Twinstar Mk III (Modified) Twinstar G-MYXS 27-Jul-13 50 Pegasus Quantum 15-912 G-EEKS 29-Jun-13 51 Pegasus Quik G-CDSA 06-Jul-13
    [Show full text]