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 10014296 AIR CARAIBES INDUSTRIES EASA.A.S.01540 DORNIER DO 228-202K Flight Data Recorder installation. Installation of 1. This STC is limited to MSN 8139, F-OGOL SSFDR type flight data recorder following OPS 1.725 implementation. 12.09.2005 10016784 AIR COMM CORPORATION EASA.IM.R.S.01125 SR00491DE EUROCOPTER FRANCE EC 120 B Installation of Cabin Air Conditioning system.The present STC is the validation of the 10016787 AIR COMM CORPORATION EASA.IM.R.S.01132 SR00463DE AGUSTA A-119 FAA STC n°SR00491DE. Air Conditioning System for Agusta A 119FAA This approval should not be extended to STC SR00463DE issued on 11th January 2002 rotorcraft of this model on which other and amended on 24th January 2006 previously approved modifications are incorporated unless it is determinded that the interrelationship between this change and any of those other previously approved modificati 10016812 AIR COMM CORPORATION EASA.IM.R.S.01173 FAA STC SR00222DE BELL 407 Installation of a vapour cycle air conditioning system None 30.06.2006 10016939 AIR COMM CORPORATION EASA.IM.R.S.01327 FAA STC SH4057NM SIKORSKY S-76A Installation of bleed air cabin heater and This STC is approved only for the product 08.05.2007 SIKORSKY S-76B windshield defrost system.Note: STC configuration as defined in the approved design SIKORSKY S-76C SH4057NM was originally approved by the UK data referred to in the paragraphs "Description" CAA under Airworthiness Approval note NO. and “Associated Technical Documentation”. 25242. This approval adds models S76A and Compatibility with other aircraft/engine S76B to the approval. This STC supersedes UK CAA A configurations shall be determined 10016959 AIR COMM CORPORATION EASA.IM.R.S.01356 FAA STC SR00601DE EUROCOPTER EC 135 Installation of Cabin Air Conditioning System i.a.w. FAA STC SR00565DE, dated 22/06/2005. 09.10.2007 10017044 AIR COMM CORPORATION EASA.IM.R.S.01468 FAA STC SH5226NM BELL 230 Installation of a bleed air cabin heating system. 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. 02.09.2008 10026907 AIR COMM CORPORATION P- FAA STC SR00230DE BELL 407 Bell Helicopter Model 407 Cabin Ventilation None 1) Prior to installation of this modification 21.08.2009 EASA.IM.R.S.01559 System. the installer mustdetermine that the interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product. 2) The inst 10028717 AIR COMM CORPORATION FAA STC SR00693DE BELL HELICOPTER 429 Installation of Cabin Air Conditioning System Provisions 24.01.2006 02.03.2006 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. 04.02.2010 10029555 AIR COMM CORPORATION FAA STC SR00543DE EC 130 B4 Installation of Cabin Air Conditioning System 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. 12.04.2010 10030166 AIR COMM CORPORATION FAA STC SR00463DE A119, AW119 MKII FAA STC No. SR00463DE Installation of Air Conditioning System 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. 31.05.2010 10038232 AIR COMM CORPORATION FAA STC SR00692DE 429 Installation of Bleed Air Heater 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 30.01.2012 04/01/2013 Page 50/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10029849 AIR CRUISERS COMPANY FAA STC SR02538NY BELL 407 Bell 407 Emergency Float Kit P/N 67432- For installation only on Bell 407 models Prior to installation of this modification it 26.04.2010 101Note: This STC is for the installation of the previously equipped with theBell Emergency must be determined thatthe Pneumatic ActivationSystem only. Float Gear Skid tubes BHT P/N 206-053-184- interrelationship between this modification 121 and206-053-184-122 or approved and any other previouslyinstalled equivalents. The ACC Bell 407 Emergency modification and/ or repair will introduce Float Installation Kit is used in conjunctionwith no adverse effectupon the airworthiness the f of the product. 10029956 AIR CRUISERS COMPANY FAA STC SR02633NY BELL 206 L-4 Bell 206L-4 Emergency Float Kit P/N 67585- 101 10013926 AIR FRANCE EASA.A.S.00198 REV. 1 BOEING 747-400 Air France B747-400 "ULYSSE" cabin 1.The approval of this modification is limited to reconfiguration. This is a revision to STC Ref the Boeing B747-400 MAS 24969, 24990, EASA.A.S.00198, to extend the applicability to 25344, 25600, 25601, 25602, 32868, 32869, the aircraft B747-400 F-GITH MSN 32868, F- 32871, 25238, 25302, 25559, 25628, 25630, GITI MSN 32869 and F-GEXA MSN 24154. 24154, 24155. The limitations and conditions The general description is included in the Air F defined in the EASA Datasheet are appli 10013927 AIR FRANCE EASA.A.S.00225 REV. 2 BOEING 747-400 ISPSS Installation on B747-400 in accordance with MA.PM 263/03 rev 5 dated 22/09/2005 The ACC Bell 206L-4 Emergency Float Prior to installation of this modification it 06.05.2010 Installation Kit is for theinstallation of the must be determined thatthe Pneumatic Activation System only, and is used interrelationship between this modification inconjunction with the float bags Type Certified and any other previouslyinstalled per TCCA TC H-92 (BellP/Ns 206-706-210- modification and/ or repair will introduce 113). no adverse effectupon the airworthiness of the product. 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 installer. 10013939 AIR FRANCE EASA.A.S.00375 REV. 1 AIRBUS A319-115 A319 CJ CASTA II Cabin Reconfiguration 1. This STC is limited to the A319-115 CJ MSN's 1485 and 15562. 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 config 10013947 AIR FRANCE EASA.A.S.00405 REV 1 BOEING 777-200-228-300 RAAS (Runway Awareness and Advisory 1. See AFM limitations for options to be 13.07.2006 System) activation. Air France AEO 77-34- used.2. Applicable to a/c serial numbers 0051 rev. 2 dated November 24, 2004CAS- listed in Air France CAS-B777-05-0192. This B777-05-19 rev 0 dated 29 June 2006 (or later STC is approved only for the product approved issue)RAAS Activation on B777-200/- configuration as defined in the approved design 300 Air France aircraftNote: This modification ext data referred to in the paragraph "D 10013996 AIR FRANCE EASA.A.S.01030 REV 1 AIRBUS A321-211 Cabin reconfigurationChange Approval Sheet ref. CAS-A320-04-015 revision 2, dated October 21, 2005 This STC is limited to the A321 MSN 1017 08.09.2006 10014054 AIR FRANCE EASA.A.S.01137 BOEING 767-200-300 Installation of Elementary Surveillance Dual ATC Mode S on B767-300The ATC Mode S computers TPR 720 are replaced by a TPR 901 which is compliant with ATC Mode S Elementary surveillance requirements.ATC Mode S Elementary surveillance implementation is descr 22.08.2005 10014055 AIR FRANCE EASA.A.S.01138 BOEING 767-200-300 Installation of Elementary Surveillance Dual ATC Mode S on B767-300The ATC Mode S computers TPR 720 are replaced by a TPR 901 which is compliant with ATC Mode S Elementary surveillance requirements.ATC Mode S Elementary surveillance implementation is descr 07.04.2005 10014056 AIR FRANCE EASA.A.S.01139 BOEING 747-200-300 Installation of EGPWS.This STC supersedes and cancels DGAC STC IM29-SF-0282. 18.05.2005 10014057 AIR FRANCE EASA.A.S.01140 BOEING 747-300 Elementary surveillance dual ATC Mode S installation. This STC is limited to the B747 MSN 24106. 15.03.2007 10014065 AIR FRANCE EASA.A.S.01151 AIRBUS A320 Cabin passenger seats relocation and floor proximity emergency escape path marking change 07.04.2005 10014264 AIR FRANCE EASA.A.S.01494 B767 Rockwell Collins Aero I SATCOM installation 19.12.2005 04/01/2013 Page 51/462 19.10.2005 20.02.2006 18.10.2005
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