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 10017003 GENEVA AVIATION, INC. EASA.IM.R.S.01414 FAA STC SH4785NM EUROCOPTER FRANCE AS 350 Installation of Dome Light / Air Vent 27.02.2008 B AssemblyThis STC is the validation of FAA EUROCOPTER FRANCE AS 350 STC SH4785NM issued on 06 November, B1 EUROCOPTER FRANCE AS 350 B2 EUROCOPTER FRANCE AS 350 B3 EUROCOPTER FRANCE AS 350 BA EUROCOPTER FRANCE AS 350 C EUROCOPTER FRANCE AS 350 D EUROCOPTER FRANCE AS 350 D1 1989 10017004 GENEVA AVIATION, INC. EASA.IM.R.S.01415 FAA STC SH5120NM EUROCOPTER FRANCE AS 350 Installation of a two place front seat. Copilot dual controls may not be installed with 20.03.2008 B this STC;Number of occupants increased to 7 EUROCOPTER FRANCE AS 350 (1 pilot and 6 passengers) with this STC B1 installed.The following placard to be installed EUROCOPTER FRANCE AS 350 on the instrument panel in front of the B2 EUROCOPTER FRANCE AS 350 B3 EUROCOPTER FRANCE AS 350 BA EUROCOPTER FRANCE AS 350 C EUROCOPTER FRANCE AS 350 D EUROCOPTER FRANCE AS 350 D1 EUROCOPTER FRANCE AS 355E EUROCOPTER FRANCE AS 355F EUROCOPTER FRANCE AS 355F1 EUROCOPTER FRANCE AS 355F2 EUROCOPTER FRANCE AS 355N pilot:AIRCRAFT IS BALLASTED TO ALLO 10017054 GENEVA AVIATION, INC. EASA.IM.R.S.01483 FAA STC SR00191SE EUROCOPTER FRANCE AS 350 Installation of a single place pilot/copilot seat in Prior to installation of this modification the 27.08.2008 B accordance with MDL GA156 installer must determine that the EUROCOPTER FRANCE AS 350 interrelationship between this modification and B1 any other previously installed modification EUROCOPTER FRANCE AS 350 will introduce no adverse effect upon the B2 EUROCOPTER FRANCE AS 350 B3 EUROCOPTER FRANCE AS 350 BA EUROCOPTER FRANCE AS 350 C EUROCOPTER FRANCE AS 350 D EUROCOPTER FRANCE AS 355E EUROCOPTER FRANCE AS 355F EUROCOPTER FRANCE AS 355F1 EUROCOPTER FRANCE AS 355F2 EUROCOPTER FRANCE AS 355N airworthiness of the product. 10030234 GENEVA AVIATION, INC. P- FAA STC SH4776NM AS 350 B, AS 350 B1, AS 350 B2 Installation of replacement transmission None 1.,,Prior to installation of this modification 17.02.2009 EASA.IM.R.S.01482 AS 350 B3, AS 350 BA, AS 350 D cowling panels i.a.w. MasterDrawing List the installer mustdetermine that the GA119.This STC is the validation of FAA STC interrelationship between this modification SH4776NM (issued on October 06,1989). and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product.2.,,The ins 04/01/2013 Page 234/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10030479 GENEVA AVIATION, INC. P- FAA STC SR00219SE 1. AS350B, AS350B1, AS350B2 Horizontal Stabilizer Color Camera MountThis None Prior to installation of this modification it 17.06.2010 EASA.IM.R.S.01510 1. AS350BA, AS350D STC is the validation of FAA STC SR00219SE must be determined thatthe 2. AS355E, AS355F, AS355F1, (last amended August 11,1995) interrelationship between this modification 2. AS355F2, AS355N and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10036806 GENEVA AVIATION, INC. P- EASA.IM.R.S.01362 10036868 GENEVA AVIATION, INC. P- EASA.IM.R.S.01400 FAA STC SR00521SE 1. AS350B, AS350BA, AS350B1 1. AS350B2, AS350B3, AS350D 2. AS355E, AS355F, AS355F1 2. AS355F2 3. BELL 407 FAA STC SR00643SE 1. AS350 D/-B/-B1/-B2/-BA 2. AS355 E/-F/-F1/-F2 3. BO-105 A/-C/-S/-LS A-1 3. BO-105 LS A-3 4. BELL 206 L-3/-L-4 4. BELL 206A/-A-1/-B/-L/-L-1 4. BELL 407 10015647 GKN AEROSPACE CHEM-TRONICS Inc. EASA.IM.A.S.01620 - AIRBUS A318 AIRBUS A319 AIRBUS A320 AIRBUS A321 10016008 GKN AEROSPACE CHEM-TRONICS Inc. EASA.IM.A.S.02173 FAA STC ST01189LA BOEING DC-9-81/82 BOEING DC-9-83 (MD-83) BOEING DC-9-87 (MD-87) BOEING MD-88 Installation of Geneva Aviation Audio System per Geneva Aviation MasterDrawing List GA182This STC is the validation of FAA STC SR00521SE (last amended April 09,2009) Installation of Geneva Aviation Video System per Geneva Aviation MasterDrawing List GA183This STC is the validation of FAA STC SR00643SE (last amended April 17,2009) Replacement CFM56-5B Inlet Barrel Lower Panel Assembly (Part Number 030-13001- 1)Replacement CFM56-5B Inlet Barrel Lower Panel Assembly (Part Number 030-13001-1) Installation of ASTECH Manufacturing, Inc. inlet assembly 10016312 GKN AEROSPACE CHEM-TRONICS Inc. EASA.IM.A.S.02616 FAA STC SA5818NM MD-88 FAA STC SA5818NM “Installation of Astech/MCI tailpipe assembly. 10016441 GKN AEROSPACE CHEM-TRONICS Inc. EASA.IM.A.S.02786 FAA STC ST01898LA; WILLIAM BON AIRBUS A319 AIRBUS A320 AIRBUS A321 10016571 GKN AEROSPACE CHEM-TRONICS Inc. EASA.IM.A.S.02969 FAA STC ST01578LA;BOND TEL.011 AIRBUS A319-113 AIRBUS A319-114 AIRBUS A320-111 AIRBUS A320-211 AIRBUS A320-212 Installation of ASTECH Engineered Products fan cowl door in accordance with ASTECH’s Master Drawing List V2500 Cowl Door Assembly No. MDL030-16103, Revision “A”. Installation of ASTECH Engineered Products, Inc. Inlet Inner BarrelAssembly in accordance with Master Drawing List, A320/CFM56- 5ASeries Engine Inlet, Drawing List Number MDL030-11030 Revision C. Any optional Geneva Aviation modifications listed in InstallationInstructions, to be installed in conjunction with this STC, shall beEASA approved. The STC applicability does not cover the model AS350B3 incorporatingmodification OP-4305 (Arriel2D engine in Any optional Geneva Aviation modifications listed in InstallationInstructions, to be installed in conjunction with this STC, shallbe EASA approved.This STC covers installation of the complete set of equipment as definedby this STC or a subset of thos This approval should not be extended to other specified airplanes of this model series on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any those other previously Prior to installation of this modification the 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.1 The ins Prior to installation of this modification the 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. 10014305 GKN AEROSPACE SERVICES LIMITED EASA.A.S.01549 REV. 1 BOEING 737 Number 1 Cockpit Windshields. Addition of This approval provides for the installation of the layers of polyurethane interlayer to the existing referenced windows individually or in any qualified designs to improve in-servicereliability combination. 10014677 GKN AEROSPACE SERVICES LIMITED EASA.A.S.02838 BOEING 747 Introduction of cockpit windows with improved design for Boeing 747 series aircraft. GKN p/n 06314 and 06315 as replacement for Boeing p/n 65B27042 and 65B27046 and GKN p/n 06316 and 06317 as replacement for Boeing p/n 065B27043 and 65B27047. This approval provides for the installation of the referenced windows indivdually or in any combination. Prior to installation of this modification it 07.10.2011 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. 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. 04/01/2013 Page 235/462 13.10.2011 30.01.2006 31.10.2006 19.03.2008 10.10.2008 12.12.2008 12.01.2007 10.04.2007
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04/01/2013 Page 1/462 - EASA

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