DOCSLIB.ORG

[email protected] C/ Fruela, 6 Fax: +34 91 463 55 35 28011 Madrid (España) Foreword

Total Page：16

File Type：pdf, Size：1020Kb

Download full-text PDF Read full-text
Ciaiac@Fomento.Es C/ Fruela, 6 Fax: +34 91 463 55 35 28011 Madrid (España) Foreword CICIAIAIACAC COMISIÓN DE INVESTIGACIÓN DE ACCIDENTES E INCIDENTES DE AVIACIÓN CIVIL Report ULM A-006/2017 Accident involving a Tecnam P96 G 100 aircraft, registration EC-ZGK, in the vicinity of the Loring airfield (El Molar, Madrid, Spain) on 31 March 2017 Informe técnico ULM A-006/2017 Accident involving a Tecnam P96 G 100 aircraft, regis- tration EC-ZGK, in the vicinity of the Loring airfield (El Molar, Madrid, Spain) on 31 March 2017 SUBSECRETARÍA GOBIERNO MINISTERIO DE ESPAÑA DE FOMENTO COMISIÓN DE INVESTIGACIÓN DE ACCIDENTES E INCIDENTES DE AVIACIÓN CIVIL © Ministerio de Fomento Secretaría General Técnica Centro de Publicaciones NIPO Línea: 161-18-117-5 NIPO Papel: 161-18-116-X Deposito Legal: M-14040-2018 Maquetación: David García Arcos Impresión: Centro de Publicaciones COMISIÓN DE INVESTIGACIÓN DE ACCIDENTES E INCIDENTES DE AVIACIÓN CIVIL Tel.: +34 91 597 89 63 E-mail: [email protected] C/ Fruela, 6 Fax: +34 91 463 55 35 http://www.ciaiac.es 28011 Madrid (España) Foreword This report is a technical document that reflects the point of view of the Civil Aviation Accident and Incident Investigation Commission (CIAIAC) regarding the circumstances of the accident object of the investigation, and its probable causes and consequences. In accordance with the provisions in Article 5.4.1 of Annex 13 of the International Civil Aviation Convention; and with articles 5.5 of Regulation (UE) nº 996/2010, of the European Parliament and the Council, of 20 October 2010; Article 15 of Law 21/2003 on Air Safety and articles 1., 4. and 21.2 of Regulation 389/1998, this investigation is exclusively of a technical nature, and its objective is the prevention of future civil aviation accidents and incidents by issuing, if necessary, safety recommendations to prevent from their reoccurrence. The investigation is not pointed to establish blame or liability whatsoever, and it’s not prejudging the possible decision taken by the judicial authorities. Therefore, and according to above norms and regulations, the investigation was carried out using procedures not necessarily subject to the guarantees and rights usually used for the evidences in a judicial process. Consequently, any use of this report for purposes other than that of preventing future accidents may lead to erroneous conclusions or interpretations. This report was originally issued in Spanish. This English translation is provided for information purposes only. Report ULM A-006/2017 Index ABBREVIATIONS ............................................................................................................................ v Synopsis ......................................................................................................................................... vi 1. FACTUAL INFORMATION ....................................................................................................... 1 1.1 History of the flight ........................................................................................................ 1 1.2 Injuries to persons .......................................................................................................... 3 1.3 Damage to aircraft ......................................................................................................... 3 1.4 Other damage................................................................................................................ 3 1.5 Personnel information .................................................................................................... 3 1.5.1 Information on the aircraft’s pilot .......................................................................... 3 1.6 Aircraft information ....................................................................................................... 4 1.6.1 System for opening and closing the engine cover .................................................. 4 1.7. Meteorological information ............................................................................................ 5 1.8 Aids to navigation .......................................................................................................... 5 1.9 Communications ............................................................................................................ 6 1.10 Aerodrome information ................................................................................................. 6 1.11 Flight recorders .............................................................................................................. 6 1.12 Wreckage and impact information ................................................................................. 6 1.13 Medical and pathological information ............................................................................ 9 1.14 Fire ................................................................................................................................ 9 1.15 Survival aspects .............................................................................................................. 9 1.16 Tests and research .......................................................................................................... 9 1.16.1. Eyewitness statements ...................................................................................... 9 1.17 Organizational and management information ................................................................ 11 1.18 Additional information ................................................................................................... 11 1.18.1. Flight Manual .................................................................................................... 11 1.19 Useful or effective investigation techniques .................................................................... 11 2. ANALYSIS ............................................................................................................................... 12 2.1 General aspects.............................................................................................................. 12 2.2 Of the wreckage ............................................................................................................ 12 2.3 Of the operation ............................................................................................................ 13 3. CONCLUSIONS ....................................................................................................................... 14 3.1 Findings ......................................................................................................................... 14 3.2 Causes/Contributing factors ........................................................................................... 14 iv Report ULM A-006/2017 Abbreviations ° ‘ “ Sexagesimal degrees, minutes and seconds °C Degrees centigrade AESA National Aviation Safety Agency GPS Global Positioning System h Hours hp Horsepower Km/h Kilometers per hour LT Local time m Meters N North UTC Coordinated Universal Time W West v Report ULM A-006/2017 Synopsis Operator: Private Aircraft: Tecnam P96 G 100, registration EC-ZGK Date and time of accident: 31 March 2017 at approx. 20:30 LT2 Site of accident: Vicinity of the Loring airfield in El Molar (Madrid, Spain). Persons onboard: 2 occupants, 1 pilot & 1 passenger. Both seriously injured. Type of flight: General Aviation-Private Phase of flight: Takeoff-Initial climb Date of approval: 20 December 2017 Summary of accident: On Friday 31 March 2017, a Tecnam P96 Golf 100 aircraft, registration EC-ZGK, suffered an accident while on a local flight in the vicinity of the Loring airfield in the town of El Molar. There were two persons onboard. After takeoff, as the aircraft was on the initial climb, the engine cover accidentally opened and the pilot decided to return to the airfield. Upon realizing he would not reach the field, he performed an emergency landing in a crop field. During the landing run, the aircraft impacted a stone wall, which caused it to flip over. The occupants were seriously injured and the aircraft sustained heavy damage. 2 All times in this report are local unless otherwise specified. On the date of the accident, local time was equivalent to UTC+2. vi Report ULM A-006/2017 1. FACTUAL INFORMATION 1.1 History of the flight On Friday 31 March 2017, a Tecnam P96 Golf 100 aircraft, registration EC-ZGK, took off from runway 24 at the Loring airfield with the intention of making a local flight with a planned duration of fewer than 15 minutes, departing from and landing at the same field. There were two occupants onboard. The pilot stated that they had delayed the departure to wait for the wind conditions to improve, as there had been strong winds all day. While they waited, the pilot and the passenger, who is also a pilot, checked the condition of the aircraft and the pilot conducted the pre-flight check. After taking off, and while turning left for the crosswind leg, at an altitude that the pilot estimated to be higher than 100 m, the engine cover began to open on the left side in the direction of motion, resulting in a constant and uncontrolled banging as the cover was bent from the front to the back. The pilot assessed the situation and fearing that the cover could strike the propeller, or that it might detach and impact the cockpit and the occupants, or the tail assembly, whose cloth elevator could easily have been damaged, he decided to cut the engine to reduce the cover’s motion and return to the runway without flaps. After completing the turn, he realized that
Load more

Recommended publications
  • Tecnam P2008-JC, G-HRLE No & Type of Engines
    AAIB Bulletin: 7/2018 G-HRLE EW/G2018/04/16 ACCIDENT Aircraft Type and Registration: Tecnam P2008-JC, G-HRLE No & Type of Engines: 1 Rotax 912-S2 piston engine Year of Manufacture: 2015 (Serial no: 1052) Date & Time (UTC): 19 April 2018 at 1010 hrs Location: Fishburn Airfield, Durham Type of Flight: Private Persons on Board: Crew - 1 Passengers - None Injuries: Crew - None Passengers - N/A Nature of Damage: Damaged beyond economic repair Commander’s Licence: Light Aircraft Pilot’s Licence Commander’s Age: 63 years Commander’s Flying Experience: 196 hours (of which 41 were on type) Last 90 days - 6 hours Last 28 days - 2 hours Information Source: Aircraft Accident Report Form submitted by the pilot Synopsis Immediately after takeoff, the aircraft suffered a loss of power and landed heavily in a field of rapeseed, adjacent to the airfield. History of the flight In good weather conditions, the pilot taxied the aircraft, which had not been flown for three weeks, to the refuelling facility at Fishburn Airfield. After adding fuel, to an indicated level of approximately 50% in the left tank and 75% in the right, the pilot re-started the engine and completed the pre-takeoff checks, without encountering any difficulty. The grass Runway 08 was used for takeoff and all was normal until approximately 150 ft agl, when the engine “spluttered” and lost power, forcing the pilot to land ahead in an adjacent field of rapeseed. The aircraft touched down heavily, causing the landing gear to collapse and damaging the wings, but it came to rest upright and the pilot was able to turn off the electrics and vacate out his door.
    [Show full text]
  • Aerodynamic Analysis and Design of a Twin Engine Commuter Aircraft
    28TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES AERODYNAMIC ANALYSIS AND DESIGN OF A TWIN ENGINE COMMUTER AIRCRAFT Fabrizio Nicolosi*, Pierluigi Della Vecchia*, Salvatore Corcione* *Department of Aerospace Engineering - University of Naples Federico II [email protected]; [email protected], [email protected] Keywords: Aircraft Design, Commuter Aircraft, Aerodynamic Analysis Abstract 1. Introduction The present paper deals with the preliminary design of a general aviation Commuter 11 seat Many in the industry had anticipated 2011 to be aircraft. The Commuter aircraft market is today the year when the General Aviation characterized by very few new models and the manufacturing industry would begin to recover. majority of aircraft in operation belonging to However, the demand for business airplanes and this category are older than 35 years. Tecnam services, especially in the established markets of Aircraft Industries and the Department of Europe and North America, remained soft and Aerospace Engineering (DIAS) of the University customer confidence in making purchase of Naples "Federico II" are deeply involved in decision in these regions remained weak. This the design of a new commuter aircraft that inactivity, nonetheless, was offset in part by should be introduced in this market with very demand from the emerging markets of China good opportunities of success. This paper aims and Russia. While a full resurgence did not take to provide some guidelines on the conception of place in 2011, the year finished with signs of a new twin-engine commuter aircraft with recovery and reason of optimism. GAMA eleven passengers. Aircraft configuration and (General Aviation Manufacturer Association) cabin layouts choices are shown, also compared 2011 Statistical Databook & Industry Outlook to the main competitors.
    [Show full text]
  • European Aviation Safety Agency
    TCDS No.EASA.A.576 P2010 Page 1 of 17 Issue 10, 08 October 2020 EASA TYPE-CERTIFICATE DATA SHEET EASA.A.576 P2010 Costruzioni Aeronautiche TECNAM S.P.A. Via S. D'acquisto, 62 80042 Boscotrecase, Napoli ITALIA Issue 01: 26 Sept 2014 Issue 02: 05 May 2015 Issue 03: 16 Dec 2015 Issue 04: 22 Dec 2016 Issue 05: 29 March 2018 Issue 06: 25 March 2019 Issue 07: 23 May 2019 Issue 08: 20 Dec 2019 Issue 09: 07 Aug 2020 Issue 10: 08 Oct 2020 EASA Form NR 90 CS-23 Issue 01 TCDS No.EASA.A.576 P2010 Page 2 of 17 Issue 10, 08 October 2020 CONTENT SECTION A: P2010 A.I. General A.II. Certification Basis A.III. Technical Characteristics and Operational Limitations A.IV. Operating and Service Instructions A.V. Operational Suitability Data (OSD) A.VI. Notes SECTION B: P2010 TDI B.I. General B.II. Certification Basis B.III. Technical Characteristics and Operational Limitations B.IV. Operating and Service Instructions B.V. Operational Suitability Data (OSD) B.VI. Notes ADMINISTRATIVE SECTION I. Acronyms II. Type Certificate Holder Record III. Change Record TCDS No.EASA.A.576 P2010 Page 3 of 17 Issue 10, 08 October 2020 SECTION A: P2010 A.I. General 1. Data Sheet No.: EASA.A.576 2. a) Type: P2010 b) Model: P2010 c) Variant: --_ 3. Airworthiness Category: CS-23 Normal category 4. Type Certificate Holder: Costruzioni Aeronautiche Tecnam S.p.A. Via Salvo D’acquisto 62 80042 Boscotrecase, Napoli ITALIA 5. Manufacturer: see Note 5 6.
    [Show full text]
  • With the Tecnam Traveller Going
    The official magazine of the Aircraft Owner and Pilots Association www.aopa.co.uk 789NM IN A STEARMAN CIRCUIT TRAINING TRIG'S LATEST Sue Girdler takes the classic Adam Winter offers advice on We look at the newest radios on aircraft from Kent to Prestwick how to correctly join a circuit offer from the UK's Trig Avionics Going Famed for its single-engine aircraft, Tecnam has switched gears with its 11-seat mini airliner. We get the inside with the track on the P2012 Tecnam Traveller MAGAZINE 02.2018 FREE TO MEMBERS WWW.AOPA.CO.UK 03 CHAIRMAN'S MESSAGE GA IS THE GLUE EDITOR David Rawlings THAT BINDS [email protected] ART EDITOR AVIATION Dan Payne [email protected] efore Christmas, together with about 80 guests from the General Aviation community and Members of the Houses of Parliament and SUB EDITOR Lords, I attended a reception held by the All-Party Parliamentary Group Lucy Debenham B (APPG) on General Aviation. The Group’s Chairman, the Rt Hon Grant Shapps, used the occasion to announce the establishment of the Government’s CONTRIBUTORS first ever General Aviation Champion, Mr Byron Davies, who will advise and inform Adam Winter, Nick Wilcock, the Secretary of State for Transport, the Rt Hon Chris Grayling MP. It had been Pauline Vahey, Sue Girdler, recognised that GA was “…the glue that binds the entire aviation sector together…”. John Walker, John Pett Byron had been the first Chair of the APPG until he lost his seat in the June 2017 General Election. Both Byron and Grant are pilots/owners and long-standing PUBLISHED BY members of AOPA.
    [Show full text]
  • Easa Type-Certificate Data Sheet Easa.A.576 P2010
    TCDS No.EASA.A.576 P2010 Page 1 of 17 Issue 11, 31 May 2021 EASA TYPE-CERTIFICATE DATA SHEET EASA.A.576 P2010 Costruzioni Aeronautiche TECNAM S.P.A. Via S. D'acquisto, 62 80042 Boscotrecase, Napoli ITALIA Issue 01: 26 Sept 2014 Issue 02: 05 May 2015 Issue 03: 16 Dec 2015 Issue 04: 22 Dec 2016 Issue 05: 29 March 2018 Issue 06: 25 March 2019 Issue 07: 23 May 2019 Issue 08: 20 Dec 2019 Issue 09: 07 Aug 2020 Issue 10: 08 Oct 2020 Issue 11: 31 May 2021 EASA Form NR 90 CS-23 Issue 01 TCDS No.EASA.A.576 P2010 Page 2 of 17 Issue 11, 31 May 2021 CONTENT SECTION A: P2010 A.I. General A.II. Certification Basis A.III. Technical Characteristics and Operational Limitations A.IV. Operating and Service Instructions A.V. Operational Suitability Data (OSD) A.VI. Notes SECTION B: P2010 TDI B.I. General B.II. Certification Basis B.III. Technical Characteristics and Operational Limitations B.IV. Operating and Service Instructions B.V. Operational Suitability Data (OSD) B.VI. Notes ADMINISTRATIVE SECTION I. Acronyms II. Type Certificate Holder Record III. Change Record TCDS No.EASA.A.576 P2010 Page 3 of 17 Issue 11, 31 May 2021 SECTION A: P2010 A.I. General 1. Data Sheet No.: EASA.A.576 2. a) Type: P2010 b) Model: P2010 c) Variant: --_ 3. Airworthiness Category: CS-23 Normal category 4. Type Certificate Holder: Costruzioni Aeronautiche Tecnam S.p.A. Via Salvo D’acquisto 62 80042 Boscotrecase, Napoli ITALIA 5.
    [Show full text]
  • Flight Manual Us-Lsa P2008
    P2008 Flight Manual FLIGHT MANUAL US-LSA P2008 Manufacturer COSTRUZIONI AERONAUTICHE TECNAM S.r.l. Serial number: ________________ Build year: ___________________ Registration: __________________ Introduction This manual contains information to be furnished to the pilot as required by the FAA in addition to further information supplied by the manufacturer. This manual must always be present on board the aircraft. The aircraft is to be operated in compliance with information and limitations contained herein. All sections follow the ASTM guidelines as finalized 14December 2007. Ed2 rev0- 18/03/2013 1 P2008 Flight Manual Record of Revisions Any revisions to the present Manual, except actual weighing data, must be recorded in the following table. New or amended text in the revised pages will be indicated by a black vertical line in the left-hand margin; Log of Revisions Revision No. Date released Chapters Approved By 2 P2008 Flight Manual List of Effective Pages Page Date Page Date Page Date 1 18-03-2013 36 “ 2 “ 37 “ 3 “ 38 “ 4 “ 39 “ 5 “ 40 “ 6 “ 41 “ 7 “ 42 “ 8 “ 43 “ 9 “ 44 “ 10 “ 45 “ 11 “ 46 “ 12 “ 47 “ 13 “ 48 “ 14 “ 49 “ 15 “ 50 “ 16 “ 51 “ 17 “ 52 “ 18 “ 53 “ 19 “ 54 “ 20 “ 55 “ 21 “ 56 “ 22 “ 57 “ 23 “ 58 “ 24 “ 59 “ 25 “ 60 “ 26 “ 61 “ 27 “ 62 “ 28 “ 63 “ 29 “ 64 “ 30 “ 65 “ 31 “ 66 “ 32 “ 67 “ 33 “ 68 “ 34 “ 35 “ 3 P2008 Flight Manual Table of Contents FLIGHT MANUAL .............................................................................................................................................................. 1 US-LSA
    [Show full text]
  • Tecnam P2008 Jc
    Page 0 - 1 Aircraft Flight Manual Doc. No. 2008/100 Ed.1 – Rev. 0 2013, July 30th TECNAM P2008 JC MANUFACTURER: COSTRUZIONI AERONAUTICHE TECNAM S.r.l. AIRCRAFT MODEL:P2008 JC TH EASA TYPE CERTIFICATE NO: A .583 (DATED 2013, 27 SEPTEMBER) SERIAL NUMBER: ………….............. REGISTRATION MARKINGS: ………….……….. This Aircraft Flight Manual is approved by European Aviation Safety Agency (EASA) and applies only EASA CS-VLA certified airplanes. This Manual must be carried in the airplane at all times. The airplane has to be operated in compliance with procedures and limitations contained herein. Costruzioni Aeronautiche TECNAM srl Via Maiorise CAPUA (CE) – Italy Tel. +39 (0) 823 997538 WEB: www.tecnam.com Page 0 - 2 SECTION 0 INDEX 1. RECORD OF REVISIONS .......................................................................................... 3 2. LIST OF EFFECTIVE PAGES .................................................................................... 8 3. FOREWORD .............................................................................................................11 4. SECTIONS LIST ......................................................................................................12 Ed. 1, Rev. 0 Aircraft Flight Manual INDEX Page 0 - 3 1. RECORD OF REVISIONS Any revision to the present Manual, except actual weighing data, is recorded: a Record of Revisions is provided in this Section and the operator is advised to make sure that the record iskept up-to-date. The Manual issue is identified by Edition and Revision codes reported on each page, lower right side. The revision code is numerical and consists of the number "0"; subsequentrevi- sions are identified by the change of the code from "0" to "1" for the firstrevision to the basic publication, "2" for the second one, etc. Should be necessary tocompletely reissue a publication for contents and format changes, the Edition code will change to the next number (“2” for the second edi- tion, “3” for the third edition etc).
    [Show full text]
  • Twin Safety On
    tecnam p2006t rr:GA 19/3/11 17:08 Page 30 TwinTwinFlight test: Tecnam P2006T safety safety on on Geoffrey Boot renews his MEP and IR in this stylish Tecnam twin and finds it very much to his liking. Photos: Flyer magazine ollowers of my flying exploits may My colleague Andy Cragg, with whom I UK and Ireland. After some frustrating recall an appetite for two engine have owned aeroplanes for many a year, delays over the winter with the snow and Fflying. Of late, however, even our has been suggesting we cast our eyes cold weather conspiring against us we venerable Twin Comanche, which has over the miniature version of the finally got together in January on a sadly been grounded for some months, Partenavia, the new Tecnam P2006T, for sunny, but later very wet and overcast has come under suspicion for being fuel some time. To be honest, in my ignorance day, providing an opportunity for me to hungry (now more per litre than cheap I had dismissed it simply because it test the aeroplane and for Tim to test me. wine!) so much so that we have been featured Rotax engines. My early Let me set the scene. Tim arrives, we using our SF260 for hops across the Irish encounters with the two stroke versions have a cup of tea; Andy arrives, we Sea from the Isle of Man. However, one had not been that happy. walk round the aeroplane, Andy takes engine with the 60-plus miles of rough However, the requirement for an IR off for a few circuits; Tim returns and in Irish Sea below, particularly in winter, and MEP renewal prompted me to phone the meantime I’ve planned the IR test; requires faith and courage.
    [Show full text]
  • TECNAM ASTORE Specification & Description
    SPECIFICATION & DESCRIPTION Pag. | 1 TECNAM ASTORE Specification & Description INTRODUCTION INDROD UCTION This document is published for the purpose of providing general information for the evaluation of design, performance and equipment of the Tecnam model Astore. Should more information be required, please contact: This document describes only the Tecnam model Astore, its powerplant and equipment. www.tecnam.com Pag. | 2 SPECIFICATION & DESCRIPTION Table of Contents General description .......................................................................................................................................... 3 Construction ...................................................................................................................................................... 3 Landing Gear ................................................................................................................................................... 3 Powerplant and propeller ............................................................................................................................. 3 Cabin .................................................................................................................................................................. 3 Three views ........................................................................................................................................................ 6 Astore Standard equipment list .......................................................................................................................
    [Show full text]
  • Tecnam P2010
    Aircraft Flight Manual Doc. No. 20101100 Ed.2 Rev.12 2019, October 21 TECNAM P2010 MANUFACTURER: rn\17lln KJNI AHWNA1f11CllH TECNAM .\ r I. AIRCRAFT MODEL: P10/0 111 EASA TYPE C ERTIFICATE No: EASA.A.576 (DATED 2014, SEPTEMBER 26 ) SERIAL NUMBER: ................... ?.?.~ ..... ......... 2015 BUILD YEAR: . .. .... .. HB-KMT REGISTRATION MARKINGS:.. ........ This manual 1s approved m accordance with 14 CFR 21 29 for US registered air­ craft, and is approved by the Federal Aviation Adn11mstrat1on. This Manual must be earned m the airplane at all limes. The a1rplane has lo be operated m compliance with procedures and lim1/alions contained herein. Costruzioni Aeronautiche TECNAM srl Via Maiorisc CAPUA (CE) - Ital y Tel. +39 0823 99.75 .38 WEB: www.tecnam.com INDEX 1. RECORD OF REVISIONS ............................................................... 3 2. LIST OF EFFECTIVE PAGES.......................................................... 7 3. FOREWORD ................................................................................... 8 4. SECTIONS LIST ............................................................................ 9 2"J Ed1t1on - Rev. 0 Aircraft Flight Manual INDEX 1. RECORD OF REVISIONS Any revision to the present Manual, except actual weighing data, is recorded: a Record of Revisions is provided at the front of this manual and the operator is ad­ vised to make sure that the record is kept up-to-date. The Manual issue is identified by Edition and Revision codes reported on each page, lower right side. The revision code is numerical and consists of the number "O"; subsequent revi­ sions are identified by the change of the code from "O" to "I" for the first revision to the basic publication, "2" for the second one, etc. Should be necessary to completely reissue a publication for contents and format changes, the Edition code will change to the next number ("2" for the second edi­ tion.
    [Show full text]
  • P Twentyten Mkii TDI
    P TwentyTen MkII TDI Specification and Description P2010 SPECIFICATION AND DESCRIPTION Introduction P TwentyTenTDI P2010 P TwentyTen TDI This document applies only to the Tecnam P2010 TwentyTen TDI and is published for the purpose of providing general information for the evaluation of design, powerplant, performance and equipment. Should more information be required, please contact: Costruzioni Aeronautiche Tecnam SpA Via Maiorise 81043 Capua CE - Italy Tel. +39 0823 622297 Fax. +39 0823 622899 www.tecnam.com [email protected] http://www.tecnam.com/aircraft/p2010TDI/ All information here applies to the Tecnam model P2010 P TwentyTen TDI equipped with the Continental CD170 engine. 2 P2010 GENERAL DESCRIPTION Introduction P TwentyTenTDI The P2010TDI is where performance and comfort meet in one sexy IFR package. 4 seats. 3 passenger doors. 1 baggage door. Continental CD-170. Metal wings, landing gear and stabilator. Carbon fibre fuselage. Balanced controls. Unsurpassed stability. The state-of-the-art Tecnam P TwentyTen is the most advanced high-wing for an elegance and styling you would expect from Tecnam’s Italian design modern single-engine aircraft in the marketplace, today with Continental CD-170 team. Metal is used for the wing and stabilator to provide further strength and Diesel engine. This four-seater aeroplane brings together an advanced stability. The wing is based on the well-proven NACA63A aerofoil. Through technology all carbon fibre fuselage with a metal wing and stabilator, an partial tapering, the design brings it close to the optimal lift distribution (elliptical). expansive cabin featuring ergonomic front and rear seats with exceptional The all movable type (stabilator) horizontal tail, a trade mark of all Tecnam legroom and a separate third entry door.
    [Show full text]
  • P92 Eaglet LSA Maintenance Manual
    P92 Eaglet Line Maintenance Manual LINE MAINTENANCE MANUAL US-LSA P92 Eaglet Manufacturer COSTRUZIONI AERONAUTICHE TECNAM S.r.l. Type Certificate: ASTM SLSA Serial number: ________ Build year: ___________ Registration: __________ This manual contains information to be furnished to the pilot as required by the FAA in addition to further information supplied by the manufacturer. The aircraft is to be operated and maintained in compliance with information and limitations contained herein. All sections follow the ASTM guidelines as finalized 14 December 2007. 1 Revision Date: 12-14-2007 Revision Number: 1.01 Doc. N° 27-13-200-00 P92 Eaglet Line Maintenance Manual Record of Revisions Any revisions to the present Manual, except actual weighing data, must be recorded in the following table. New or amended text in the revised pages will be indicated by a black vertical line in the left-hand margin; Revision No. and date will be shown on the left-hand side of the amended page. Log of Revisions Revision No. Date released Chapters Approved By 1.00 12-14-2007 All Tecnam 1.01 02-02-2009 2, 3, 5, 27 Tecnam Revision n°1, 2nd February 2009 2 Revision Date: 12-14-2007 Revision Number: 1.01 Doc. N° 27-13-200-00 P92 Eaglet Line Maintenance Manual List of Valid Pages Page Date Page Date 1 12-14-2007 36 12-14-2007 2 02-02-2009 37 12-14-2007 3 02-02-2009 38 12-14-2007 4 12-14-2007 39 12-14-2007 5 02-02-2009 40 12-14-2007 6 12-14-2007 41 12-14-2007 7 12-14-2007 42 12-14-2007 8 12-14-2007 43 12-14-2007 9 12-14-2007 44 12-14-2007 10 12-14-2007 45 12-14-2007 11
    [Show full text]