Tecnam P2012 Traveller
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Commuter Aircraft Scenario
CEAS –TCAD 2014 4th Symposium of Collaborative Aircraft Design Reference Aircraft General Aviation Aircraft Design Fabrizio NICOLOSI University of Naples «Federico II» Dept of Industrial Eng. –Aerospace Division [email protected] CEAS –TCAD 2014 , 4th Symposium of Collaborative Aircraft Design GA and Commuter Aircraft Scenario GAMA – General Aviation Manufacturers Association Each Year Databook on General Aviation (Statistics & Industry Outlook) CEAS –TCAD 2014 , 4th Symposium of Collaborative Aircraft Design Possible future Scenario SAT – Small Air Transport Roadmap (EC Research fin. Project) Preliminary demand forecast by Europe for 2030 317,000 flight/year 720 Aicrafts (600 piston engine prop) CEAS –TCAD 2014 , 4th Symposium of Collaborative Aircraft Design Commuter Aircraft Scenario GAMA Data-book is an impressive source of data and statistics for those interested in GA, and it is mainly related to US. Average Age of Registered General Aviation Fleet 4 CEAS –TCAD 2014 , 4th Symposium of Collaborative Aircraft Design Small Aircraft Operation Small Aircraft Transport will serve: - The need for low-intensity intercity routes - Regions with less developed infrastructures - The needs of European business travel Main Costraints: General Aviation (GA) refers to all flights other - REGULATORY than military and scheduled airline and regular - OPERATIONAL cargo flights, both private and commercial. - FINANCIAL In USA the Regulatory framework is significantly different from the European one OPERATIONAL CONSTRAINTS • All weather operations -
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. -
Warbirds Over Wanaka the Pearse Project Cirrus Adventure: the Long Way to Brisbane
KiwiFlyer TM Magazine of the New Zealand Aviation Community Issue 45 2016 #2 $ 6.90 inc GST ISSN 1170-8018 Warbirds Over Wanaka The Pearse Project Cirrus Adventure: The long way to Brisbane Products, Services, News, Events, Warbirds, Recreation, Training and more. KiwiFlyer Issue 45 2016 #2 From the Editor In this issue Welcome to KiwiFlyer #45. We hope you’ll find 7. The Pearse Project plenty of good reading within. Ivan Mudrovich has spent more than a decade creating a faithful interpretation of Richard There’s more than a few owners of GA and Pearse’s 1903 aircraft. Chris Gee attended the recreational aircraft who will have thought at some attempts to get it airborne. time “I could fly to Australia”. And then added “if I wanted to” and then left it at that. Satisfying 10. Cirrus Adventure: The long way to Brisbane to think that you could, but in reality all a bit too Lance Weller wanted to relocate his Cirrus from risky and difficult, and for that matter, hardly cost NZ to Brisbane and chose a route through efficient. Albeit that Lance Weller had the additional Noumea and PNG. He tells the adventure here. motive of relocating his Cirrus to Brisbane, Lance is indeed someone who headed off on an international 16. EAA AirVenture Oshkosh with Gaye Pardy flight(s) ‘because he could’. Far from taking the This years Gaye Pardy Travel tour to Oshkosh traditional route via Norfolk and Lord Howe Islands, will be their 30th. All aviation enthusiasts should Lance and co-pilot Garth Jensen made the journey go at least once. -
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. -
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. -
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. -
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. -
[email protected] 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. -
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 -
Paper Title (Use Style: Paper Title)
Numerical Aerodynamic Analysis of a New Twin Engine Commuter Aircraft Longitudinal and Lateral-Directional Derivatives [Nicolosi Fabrizio, Corcione Salvatore, Della Vecchia Pierluigi, Agostino De Marco] Abstract — This paper deals with numerical investigation preliminary design phase and aerodynamic analysis have been about both longitudinal and lateral-directional static shown by authors in previous scientific articles [1-3]. Fig. 1 aerodynamic characteristics of a new twin-engine commuter shows the aircraft three views. P2012 has a straight tapered aircraft with eleven seats, Tecnam P2012. Numerical analyses wing with surface of about 25 square meters and a wing span have been performed on complete and many partial aircraft of about 14 meters. Two quasi symmetrical nacelles are configurations in order to evaluate the contribution of each installed on wing and two winglets are mounted at wing tip. aircraft component and to estimate their mutual interferences. Slender fuselage geometry of about 12 meters can The analyses have been conducted at wind tunnel Reynolds accommodate up to 11 occupants (2 pilots plus 9 passengers) number in order to provide a validation of the numerical with an higher fineness ratio for the aircraft category equal to investigation. Finally numerical analyses have been also l /d = 7.24. P2012 main geometrical dimensions are performed at free flight conditions, in order to have an estimation F F of the Reynolds number effect in especially on the aircraft base summarized in Table I. Conventional horizontal body mounted drag coefficient and on the wing span loads in both flap up and tail plane has been adopted with a horn balanced elevator flap down conditions. -
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). -
New Product Announcements AERO 2017
New product announcements AERO 2017 New worldwide Allstar PZL Glider Sp. z o.o. sim+glide: innovative flightsimulator for gliders with 4 Stand: B5-137 axial motions www.szd.com.pl With sim+glide instruction and training of pilots will be in future - independent of weather - possible by day and night - Hedwigstr. 18 more cost efficient - promoting safetyness and rountine - 30159 Hannover enableing programms for specific types of gliders as well as Germany for cross-country and aerobatic flying The mobility with 4 Tel: +49 1704301254 axial motions makes it possible to simulate nearly each flight Fax: +49 511 441732 figure authentically. E-Mail: [email protected] Contact: Bernd Hager Company: Allstar PZL Glider Sp. z o.o. Internet: www.szd.com.pl 2017 1 / 16 Dacher Systems GmbH sky[nav]pro RedLine Box including FLARM for collsion Stand: A6-103 avoidance www.skynavpro.aero After introducing its BlueLine Satellite Box which offers in flight weather and real time tracking and monitoring at AERO Klärwerkstr. 1A 2016 in Friedrichshafen last year, Dacher Systems is now 13597 Berlin launching its RedLine Box, containing hardware to offer Germany collision avoidance with FLARM. Tel: +49 30-398009115 E-Mail: [email protected] Contact: Tiberius Dacher Company: Dacher Systems GmbH Internet: www.dacher-systems.de EWAK GmbH UGM 3644, new type of four-stroke engine Stand: A5 - 301 www.ewak-berlin.com Straße C 15345 Altlandsberg Germany Tel.: +49 176 81297645 E-Mail: [email protected] Contact: Sascha Manthey Company: EWAK GmbH Internet: www.ewak-berlin.com 2017 2 / 16 FernUniversität in Hagen Emergency Landing Assistant (ELA) Stand: FW-BP04 http://www.fernuni-hagen.de/rechnerarchitektur/fas.shtml The Department of Computer Architecture at the FernUniversität in Hagen (Prof.