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Efter detta datum då EASA bildades skall samtliga luftfartyg som har ett svenskt FABRIKAT Aero Commander (Se Rockwell) Aeronca MODELL LFV Nr TCDS

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TYPE-CERTIFICATE DATA SHEET - EASA. Just sharing my See the TCDS for details of the manuals for all other engine variants. 3. The TCDS includes some 

Page 5. TCDS No.EASA.A.576. P2010. Page 4 of 10.

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Description: The EV-97 VLA is a two-seater, all metal, cantilever low-wing monoplane with two side-by-side seats, fixed tricycle landing gear, TCDS No.: EASA.A. 064 AIRBUS A318, A319, A320, A321 Issue: 27 Date: 6 March 2017 2) TSL7009, v 0 3.00, 2020-11-09 Ansökningsblankett för miljö och luftvärdighetshandlingar för EASA luftfartyg (Del-M och Del-ML) 1 (Observera att den här ansökningsblanketten inte ska användas vid ansökan som gäller s.k. Bilaga I luftfartyg EASA.SAS.A.041 Segelflugzeugbau A. Neukom Page 1 of 2 Issue 01, 27/03/2007 Elfe European Aviation Safety Agency . EASA .

av M Ahmad · 2012 — PAM följer idag EASA Part-145 och har som mål att bli en verksamhet som är godkänd TCDS. Type Certificate Data Sheet. TCH. Type Certificate Holder 

2. Reference Date for determining the applicable airworthiness requirements 25 May 1990 (JAA Validation Reference Date). 3. EASA Certification Basis 3.1.

Aug 7, 2006 TYPE CERTIFICATE DATA SHEET NO. 2A13. This data sheet, which is a part of Type Certificate 2A13, prescribes conditions and limitations 

Copies are not controlled.

EASA AD 2021-0026 affects the same airworthiness limitations (task and life limits) as those in EASA AD 2020-0211, the airworthiness limitations in the service information referenced in EASA AD 2021-0026 prevail.
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European Aviation Safety Agency. EO STC. Supplementary Type Certificate.

Type Certificate Data Sheet  av M Ahmad · 2012 — PAM följer idag EASA Part-145 och har som mål att bli en verksamhet som är godkänd TCDS.
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5. State of Design Authority EASA (pre EASA: DGAC, France) 6. Type Certificate Date by DGAC FR 27 October 1977 7. Type Certificate n° EASA.R.008 (former DGAC FR: 157) 8. Type Certificate Data Sheet n° EASA.R.008 (former by DGAC FR: 157) 9. EASA Type Certification Date 28 September 2003, in accordance with CR (EU) 1702/2003, Article 2, 3., (a),

Tecnam P2002. Page 4 of 12.


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TCDS Number: EASA.A.059 Foreign AD: Not applicable Revision: This AD revises EASA AD 2013-0242 dated 02 October 2013, which superseded EASA AD 2009-0129 dated 19 June 2009. ATA 32 Landing Gears – Steering / Steering Manifold – Func tional Check / Modification Manufacturer(s): Piaggio Aero Industries S.p.A. (PAI)

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Notes: 1) When MOD 2010/002 (EASA approval 10052750) is installed 2) When MOD 2010/032 (EASA approval 10055692) is installed 3) When MOD 2010/078 (EASA approval 10065113) is installed 4) When MOD 2010/133 (EASA approval 10069356) is installed See FAA TCDS E41NE. 2. Reference Date for determining the applicable airworthiness requirements 25 May 1990 (JAA Validation Reference Date). 3.