04/01/2013 Page 1/462 - EASA

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EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10017117 AEROSPACE DESIGN FACILITIES Ltd. EASA.R.S.01099 EUROCOPTER FRANCE AS 355 Installation of Wescam nose mount This STC is approved only for the product 18.08.2005 SERIE configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 10017147 AEROSPACE DESIGN FACILITIES Ltd. EASA.R.S.01250 EUROCOPTER FRANCE AS 350 |nstallation of Wescam combined nose and Approval limited to nose mount only 01.03.2006 SERIE side mount 10017276 AEROSPACE DESIGN FACILITIES Ltd. EASA.R.S.01512 EUROCOPTER FRANCE AS ADF2003-001 Utility Pole Mount.This STC None. 21.08.2008 355F supersedes EASA approval 2004-1997, dated EUROCOPTER FRANCE AS 355F1 EUROCOPTER FRANCE AS 355F2 EUROCOPTER FRANCE AS 355N 5 March 2004. 10028585 AEROSPACE DESIGN FACILITIES Ltd. P-EASA.R.S.01444 REV. 2 1. AS350 B, B1, B2, BA, BB, B3 Cowling - Secondary Latching None Prior to installation of this modification it 14.09.2010 1. AS350 D, EC130B4 must be determined thatthe 2. AS355E, interrelationship between this modification 2. AS355F, AS355F1, AS355F2, and any other previouslyinstalled 2. AS355N, AS355NP modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10013963 AEROSPACE ENGINEERING SOLUTIONS 10014122 AEROSPACE ENGINEERING SOLUTIONS 10014123 AEROSPACE ENGINEERING SOLUTIONS 10014557 AEROSPACE ENGINEERING SOLUTIONS 10014854 AEROSPACE ENGINEERING SOLUTIONS 10014949 AEROSPACE ENGINEERING SOLUTIONS 10015236 AEROSPACE ENGINEERING SOLUTIONS 10034052 AEROSPACE ENGINEERING SOLUTIONS 10037704 AEROSPACE ENGINEERING SOLUTIONS 10040625 AEROSPACE ENGINEERING SOLUTIONS EASA.A.S.00652 REV 2 BOEING 767-300 Introduction of Matsushita In-Flight Entertainment System This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. EASA.A.S.01232 BOEING 767-300 Introduction of 258 Passenger Configuration & Associated Cabin Changes EASA.A.S.01233 BOEING 767-300 Introduction of Matsushita in-Flight Entertainment System EASA.A.S.02655 BOEING 767-300 Introduction of Main/APU Battery Paralleling for Restricted to Aircraft G-DBLA ASN 26063 & G- Extended Standby Power Time Capability. PJLO ASN 26064. EASA.A.S.03078 B767 Introduction of 290 Pac Place Interior Configuration S/N 23765 ONLY. 31.05.2007 EASA.A.S.03212 BOEING 757-200 Introduction of alternative EGPWS Mode 6 FAA STC ST00381SE must be installed prior 21.08.2007 Callout Menu. to the installation of this STC EASA.A.S.03662 BOEING 757-200 Introduction of Flight Control Computer (FCC) • Prior to installation of this modification the 13.08.2008 Interlock2. installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.• Th P-EASA.A.S.03621 REV. 1 B757-200 Introduction of IFE System Circuit Breaker, None The embodiment of this STC also 02.03.2011 Relays and Wiring. constitutes an Alternative Means ofCompliance (AMOC) to the requirements of FAA AD 2007-16-12, which hasbeen adopted by EASA. This AMOC is issued in respect of the installationof this STC in lieu of the mandated Boeing SB 75 A319-132 Introduction of Panasonic dMPES In Flight None Prior to installation of this modification it 16.12.2011 Entertainment - IFE System must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product 321-231 Introduction of Panasonic MPES IFE system The approval is limited to MSN 2730 and MSN 2793 02.11.2005 30.05.2005 30.05.2005 10.10.2006 Prior to installation of this modification it 16.07.2012 must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 04/01/2013 Page 38/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10027883 AEROSPACE ENGINEERING REV. 1 A320-214 Introduction of Rockwell Collins dPAVES IFE Not applicable Prior to installation of this modification it 22.03.2011 SOLUTIONS LIM SystemRevision of the EASA STC 10027883 must be determined thatthe to remove EWIS limitation interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10031517 AEROSPACE ENGINEERING SOLUTIONS LIM 10036814 AEROSPACE ENGINEERING SOLUTIONS LIM 10040704 AEROSPACE ENGINEERING SOLUTIONS LIM 10014059 AEROSPACE ENGINEERING SOLUTIONS Ltd 10014208 AEROSPACE ENGINEERING SOLUTIONS Ltd 10014495 AEROSPACE ENGINEERING SOLUTIONS Ltd 10016714 AEROSPACE FILTRATION SYSTEMS, Inc. 10016715 AEROSPACE FILTRATION SYSTEMS, Inc. 10016741 AEROSPACE FILTRATION SYSTEMS, Inc. 10016929 AEROSPACE FILTRATION SYSTEMS, Inc. CAA UK CAA.21NE2.00057 B757-220, MSN 27973 Introduction of Driessen G1A and G4B Galleys Restricted to ASN 27973 Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 20.08.2010 REV. 3 CAA UK CAA.21NE2.00057 REV. 2 B757-204/-236 FAR Part 26 Validation for EASA STC CAA.21NE2.00057 A321 Introduction of Twin Class Cabin Interior Configuration. EASA.A.S.01143 B757-200 Introduction of Pegasus Flight Management Computers & Multi Mode Receivers (MMRs) None Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 07.10.2011 The EASA STC 10038683 is a prerequisite for the installation of thisSTC. The approval holder shall fulfill the 20.07.2012 obligations of Part 21, Paragraph21A.109.Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repai EASA.A.S.01360 B767-300 Introduction of 279 passenger configuration 01.07.2005 EASA.A.S.02557 B767-300 Introduction of 290 passenger place interior configuration EASA.IM.R.S.01008 REV. 1 FAA STC SR09421RC BELL 206L-3 Installation of Aerospace Filtration System This STC is approved only for the product BELL 206L-4 (AFS) Engine Inlet Barrier Filter (IBF) system in configuration as defined in the approved design accordance with the FAA STC SR09421 RC. data referred to in the paragraph "Description". AFS Drawing Number 10600, Revision B dated Compatibility with other aircraft/engine 17/6/2004FAA STC SR09421RC dated configurations shall be determined by the 25/08/2004 (Rotorcraft Certification Offiice S installer. EASA.IM.R.S.01009 FAA STC SR09368RC BELL 407 Installation of Aerospace Filtration System EASA.IM.R.S.01067 FAA STC SR01394LA MD HELICOPTERS 369D MD HELICOPTERS 369E MD HELICOPTERS 369F MD HELICOPTERS 369FF MD HELICOPTERS 369H MD HELICOPTERS 369HE MD HELICOPTERS 369HM MD HELICOPTERS 369HS EASA.IM.R.S.01315 FAA STC SR09451RC BELL 206B Installation of Aerospace Filtration Systems (AFS) Engine Inlet Barrier Filter (IBF) on Bell 206B helicopters.Validation of FAA STC SR09451RC dated December 14, 2005. This STC is classified as ‘BASIC’ by the FAA and is approved under the post type Validati 1. Rotorcraft Flight Manual Supplement dated (AFS) Engine Inlet Barrier Filter (IBF) system in 10/12/2003 is a required part of this STC2. accordance with the FAA STC "Instructions for continued airworthiness" AFS- SR09368RC.AFS Drawing Number 10600, BH407-IBF-KIT-ICA is also required part of this Revision A dated 8/4/2003 FAA STC STC.3. This STC is approved only for the SR09421RC dated 25/08/2004 (Rotorcraft Certification Office So product configuration as define Installation of Aerospace Filtration Systems This STC is approved only for the product Inlet Barrier Filter System instead of Engine Air configuration as defined in the approved design Separator (with or without Mist Eliminator) or data referred to in the paragraph "Description". FOD Screen. According to FAA STC Compatibility with other aircraft/engine SR01394LA. Master Data List: MD500-IBF-KIT- configurations shall be determined by the MDL, Rev. D, dated 30.09.2004 or later installer. 04/01/2013 Page 39/462 23.03.2005 22.05.2006 27.01.2005 27.01.2005 16.08.2005 05.12.2007
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04/01/2013 Page 1/462 - EASA

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