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 10015986 O&N AIRCRAFT MODIFICATIONS, INC. EASA.IM.A.S.02139 FAA STC SA1035NE CESSNA 150F Installation of a 14.6 gallon aft fuselage tank in 1. FAA Approved Supplement to Pilot’s 13.10.2006 CESSNA 150G baggage compartment. Operating Handbook and / or FAA Approved CESSNA 150H Airplane Flight Manual, Nr. 19, 20 and 21, CESSNA 150J dated Jan. 13-93, or later approved revision, is CESSNA 150K required Cessna 150F, G, H, J, K ,L & M and CESSNA 150L CESSNA 150M CESSNA 152 152.2. This installation is not eligible 10015797 OFEK HOLDING CORPORATION EASA.IM.A.S.01858 FAA STC SA01415CH PIPER PA-31T Installation of camera provisions in fuselage This STC is approved only for the product 30.01.2006 floor cut-out 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. 10015798 OFEK HOLDING CORPORATION EASA.IM.A.S.01859 FAA STC SA01961CH PIPER PA-31T Installation OFEK Holding Company camera provisions installed pursuant to STC SA01962CH 30.01.2006 10034682 OGMA, INDUSTRIA AERONAUTICA DE EMB-135BJ Change Number 1086.07 - "Installation of none Prior to installation of this modification it 19.04.2011 coffee maker & associated watertank" 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. 10037579 OGMA, INDUSTRIA AERONAUTICA DE EMB-145EP, EMB-145LR EMB-145LU 10039843 OGMA, INDUSTRIA AERONAUTICA DE EMB-145EP EMB-145EU EMB-145LR EMB-145LU 10042497 OGMA, INDUSTRIA AERONAUTICA DE EMB-145EP,EMB-145LR,EMB- 145LU Installation of a VIP meeting room on EMB-145 Aircraft S/N 145076, 145084, 145129, 145135, Prior to installation of this modification it 08.12.2011 and 145147. 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 Nespresso Coffe Maker InstallationDescription as per Change Dossier, ref. 11P05CD00001 initial issue, dated 23th May 2012. VIP room extension and Iridium Satphone system installation on EMB-145 10031182 OHS AVIATION SERVICES GmbH EASA.A.S.03940 328-100, 328-300 Change seat cushions bottom and backrest, JB6series and AMP 1300 series for DO 328- 100 and -300 10015480 ONBOARD SYSTEMS INTERNATIONAL EASA.IM.A.S.01238 FAA STC ST10395SC MD-11 EASA Validation of FAA STC ST10395SC on “Installation of two non-taxi, take-off and landing (TT7L) courier seats" and associated Airplane Flight Manual Supplement 10016706 ONBOARD SYSTEMS INTERNATIONAL EASA.IM.R.S.00457 REV. 1 FAA STC NO SR01424SE AS355 E, AS355 F, AS355 F1, AS355 F2, AS355 N, AS355 NP Applicability for the following S/N: 145076, 145084, 145129, 145135,145147, 145242, 145258. The change is applicable to the following aircraft having OGMA STC10037579 incorporated, and that do not have flux valve sensors: A/C SN145076, 145084, 145129, 145135, and 145147 Prior to installation of this modification it 29.05.2012 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. Prior to installation of this modification it 05.12.2012 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. 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 30.07.2010 1. 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. 31.05.2005 Cargo Hook Kit model 200-292-01 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. 21.07.2010 04/01/2013 Page 348/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016709 ONBOARD SYSTEMS INTERNATIONAL EASA.IM.R.S.00553 REV. 1 FAA STC SR00699SE BELL 204B To amemd EASA STC EASA.IM.R.S.00553 to Approval of this change in type design applies 19.10.2005 BELL 205A list the correct document number for the only to Bell 204B, 205A, 205A-1, 212, 412 and BELL 205A-1 Rotorcraft Flight Manual Supplement 412EP rotorcraft which where prevsiously BELL 212 (RFMS)Ass.:Section 4 of Onboard Systems equipped with an approved installation of the BELL 412 Service Manual No. 122-004-00.Rotorcraft following cargo hook: Bell P/N 204-072-924-1 BELL 412 EP Flight Manual Supplement No. 121-020-00 dated 24 September or Breeze Eastern P/n SP7109-1, 10016711 ONBOARD SYSTEMS INTERNATIONAL EASA.IM.R.S.00623 FAA STC SR01166SE EUROCOPTER FRANCE AS 350 Cargo Hook Kit installation, in accordance with 1. This STC is approved only for the product 15.03.2005 B3 FAA STC No. SR1166SE issued January 22, configuration as defined in the approved design 2003. data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 10016726 ONBOARD SYSTEMS INTERNATIONAL EASA.IM.R.S.01027 REV. 2 FAA STC SR00886SE AS350B, AS350BA, AS350B1 Installation of Cargo Hook Kit Model 200-261- The cargo hook kits approved under this STC Prior to installation of this modification it 13.01.2010 AS350B2, AS350B3, AS350D 00, 200-261-01, and200-353-00This STC is a can be installed on AS 350B, BA, B1, B2, and must be determined thatthe EC130B4 revision to EASA STC EASA.IM.R.S.01027 D helicopters equipped with Eurocopter swing interrelationship between this modification Revision 1 throughthe validation of amendment or slingtype systems, or on AS350B3 equipped and any other previouslyinstalled dated 11 August, 2009 to FAA STC with Eurocopter sling type systemonly, or on modification and/ or repair will introduce SR00886SE. EC 130B4 equipped with Eurocopte no adverse effectupon the airworthiness of the product. 10016781 ONBOARD SYSTEMS INTERNATIONAL EASA.IM.R.S.01122 FAA STC SH1262NW EUROCOPTER FRANCE AS 350 B EUROCOPTER FRANCE AS 350 B1 EUROCOPTER FRANCE AS 350 B2 EUROCOPTER FRANCE AS 350 BA EUROCOPTER FRANCE AS 350 D EUROCOPTER FRANCE AS 350 10016789 ONBOARD SYSTEMS INTERNATIONAL EASA.IM.R.S.01136 FAA STC SH4908NM D1 MD HELICOPTERS 369D MD HELICOPTERS 369E 10016804 ONBOARD SYSTEMS INTERNATIONAL EASA.IM.R.S.01164 FAA STC SR01588SE EUROCOPTER FRANCE AS 350 B EUROCOPTER FRANCE AS 350 B1 EUROCOPTER FRANCE AS 350 B2 EUROCOPTER FRANCE AS 350 B3 EUROCOPTER FRANCE AS 350 BA EUROCOPTER FRANCE AS 350 10016806 ONBOARD SYSTEMS INTERNATIONAL EASA.IM.R.S.01166 FAA STC SR00369SE D BELL 206L BELL 206L-1 BELL 206L-3 BELL 206L-4 BELL 407 10016807 ONBOARD SYSTEMS INTERNATIONAL EASA.IM.R.S.01167 FAA STC SR00892SE MD HELICOPTERS 369D MD HELICOPTERS 369E MD HELICOPTERS 369F MD HELICOPTERS 369FF MD HELICOPTERS 369HE MD HELICOPTERS 369HM MD HELICOPTERS 369HS MD HELICOPTERS 500N 10016809 ONBOARD SYSTEMS INTERNATIONAL EASA.IM.R.S.01169 FAA STC SR00557SE ROBINSON R22 ROBINSON R22 ALPHA ROBINSON R22 BETA ROBINSON R22 MARINER Electronic Model E-69 Cargo Hook Load Cell System p/n 200-295-00, in accordance with Onboard Systems Master Drawing List n° 155- 010-00, revision 10 dated 15/06/04 approved by FAA, or later FAA approved revision. Installation of Model E-51 Cargo Hook Load Cell System PN 200-034-00. This STC is the validation of the FAA STC SH4908NM amended on05/11/1990 and limited to MDHI 369 D and E models 1 - The present STC is the validation of the FAA STC SH1262NW last amended on 15/03/05, limited to Eurocopter AS 350 B, BA, B1, B2,and D models.2 – The system covered by this STC can be installed on AS 350 helicopters equipped with Eurocopter sling systems 1. This STC is to be installed on aircraft models specified in "applicability" section above, equipped with MDHI Cargo Hook Kit No.369H90072, using MDHI cargo hook manual release PN 14323-2 only.2. Installation, Inspection and Operation must be done in acc ONBOARD SYSTEMS fuel drain guard kit for Refer to FAA STC SR01588SE reissued Eurocopter AS 350 series helicopter.Validation September 29, 2005 of FAA STC SR01588SE Cargo hook installation n. 200-215-00 Approval of this change in type design applies to only those Bell model rotorcraft listed above, which were previously equipped with an FAA approved installation of Bell cargo hook suspension systems 206-706-341-5, 206-706- 341-101; 206-706-341-109 and eith Installation of Onboard Systems Model 200- This cargo hook is not approved for human 264-00 Cargo Hook kit.EASA validation of FAA external load.Approval of this installation STC n0 SR00892SE, amended January 13th, applies to the above listed model rotorcraft 2003, or later approved revision.This STC is only, which were previously equipped with an classified 'Basic' by the FAA and is approved approved installation of McDonnell Douglas under the post type Validation Princip cargo hook suspension systems and car 10.01.2007 12.10.2005 06.03.2006 27.09.2006 08.07.2008 Cargo Hook Suspension System 02.01.2006 04/01/2013 Page 349/462
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04/01/2013 Page 1/462 - EASA

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