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 10035437 AMAC AEROSPACE SWITZERLAND AG A319-133 Satcom and LAN / WLAN System Installation Not Applicable 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 22.06.2011 10036061 AMAC AEROSPACE SWITZERLAND AG B737-700IGW VIP seat change / Replacement of single seat by one with massagefeature. 10037123 AMAC AEROSPACE SWITZERLAND AG A319-133 Monitor Replacement / Exchange of Plasma- TV with LCD-TV screens in VIPcabin. 10039943 AMAC AEROSPACE SWITZERLAND AG A319-133 Interior RefurbishmentBy: - Carpet and Curtain replacement- Seat re-upholstery- Replacement of 4 double seats by 2 L-Shape Divans- VCC (IFE) Cabinet relocation- IFE upgrade- Additional Power Outlets installation- Emergency Equipment replacement 10041797 AMAC AEROSPACE SWITZERLAND AG B777-200LR Interior Outfitting project BA01-2500 (S/N 40753) The change consists in a complete cabin interior outfitting of B777-200LR S/N 40753 aircraft with a 125 passengers, plus 16 crew seatingarrangement in a new "VVIP" Cabin Interior suitable for"Private/Smokin 10016760 AMERICAN EUROCOPTER CORPORATION 10016761 AMERICAN EUROCOPTER CORPORATION 10016769 AMERICAN EUROCOPTER CORPORATION 10016778 AMERICAN EUROCOPTER CORPORATION 10016779 AMERICAN EUROCOPTER CORPORATION 10016834 AMERICAN EUROCOPTER CORPORATION EASA.IM.R.S.01089 FAA STC SR09281RC-D EUROCOPTER FRANCE EC 155 B1 American Eurocopter LLC Modification FAA STC SR09281RC-D.Installation of a Garmin Global Positioning System (GPS) - GPS 500. This approval is limited to Aircraft B737- 700IGW, Serial Number 36027. Prior to installation of this modification it 09.08.2011 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. S/N: 2421 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. 04.11.2011 S/N: 1335 ,,A7-HHJ Approval valid only for MSN 1335. The aircraft is certified for private use only. It is prohibited tooperate the aircraft for hire or offered for common carriage. The aircraft is a "No Smoking" aircraft. A Minimum of 1 Cabin Crew is required. 04.06.2012 S/N 40753 For other Lim 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. 16.10.2012 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 EASA.IM.R.S.01090 FAA STC SR09290RC-D EUROCOPTER FRANCE EC 155 Installation of horizontal tip position/anti- installer. This STC is approved only for the product B1 collision strobe lights 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.IM.R.S.01100 FAA STC SR09282RC-D EUROCOPTER FRANCE EC 155 American Eurocopter LLC Modification FAA This STC is approved only for the product B1 STC SR09282RC-D. Installation of a configuration as defined in the approved design Honeywell Enhanced Ground Proximity data referred to in the paragraph "Description". Warning System. Compatibility with other aircraft/engine configurations shall be determined by the installer. EASA.IM.R.S.01117 FAA STC SH8804SW-D EUROCOPTER FRANCE EC 155 Installation of a Universal Navigation UNS- 1F B1 Flight Management System for IFR enroute & non-precision approaches. EASA.IM.R.S.01118 FAA STC SR09295RC-D EUROCOPTER FRANCE EC 155 Installation of navigation, communications & This STC is approved only for the product B1 various electrical equipment 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.IM.R.S.01205 FAA STC SH7339SW-D EUROCOPTER FRANCE AS Installation of an extended radome and FLIR 365N2 2000 infrared imaging system, in accordance EUROCOPTER FRANCE AS with AEC Drawing List n° 365A73-9037, 365N3 revision H dated 09 October 2000, or later FAA EUROCOPTER FRANCE SA 365N EUROCOPTER FRANCE SA 365N1 approved revision. 04/01/2013 Page 72/462 15.08.2005 20.07.2005 11.08.2005 10.10.2005 10.10.2005 28.08.2006
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016835 AMERICAN EUROCOPTER EASA.IM.R.S.01206 FAA STC SH7338SW-D EUROCOPTER FRANCE AS Installation of an AFT mounted retractable 28.08.2006 CORPORATION 365N2 Nightsun Searchlight System, in accordance EUROCOPTER FRANCE AS with AEC Drawing List n° 365A73-9036, 365N3 revision F dated 19 March 1999, or later FAA EUROCOPTER FRANCE SA 365N1 approved revision. 10016836 AMERICAN EUROCOPTER EASA.IM.R.S.01207 FAA STC SH7022SW-D EUROCOPTER FRANCE AS Installation of Radio Master switch, in Compatibility of this modification with 20.07.2006 CORPORATION 365N2 accordance with AEC Drawing List No. previously approved modifications must be EUROCOPTER FRANCE AS 365A73-9034, revision B dated 25 April 2002, determined by the installer. 365N3 EUROCOPTER FRANCE SA 365N1 or later EASA approved revision 10016837 AMERICAN EUROCOPTER EASA.IM.R.S.01208 SH7014SW-D EUROCOPTER FRANCE AS Installation ofvertical fin anti-collision light, in Compatibility of this modification with 20.07.2006 CORPORATION 365N2 accordance with AEC Drawing List No. previously approved modifications must be EUROCOPTER FRANCE AS 365A73-9027, revision E dated 09 June 2003, determined by the installer. 365N3 EUROCOPTER FRANCE SA 365N1 or later EASA approved revision 10016838 AMERICAN EUROCOPTER EASA.IM.R.S.01209 SH5499SW-D EUROCOPTER FRANCE AS Installation of supplement strobe light, in Compatibility of this modification with 20.07.2006 CORPORATION 365N2 accordance with AEC Drawing List No. H365- previously approved modifications must be EUROCOPTER FRANCE AS 64-2D-101, revision L dated 06 June 2003, or determined by the installer. 365N3 EUROCOPTER FRANCE SA 365N1 later EASA approved revision 10016839 AMERICAN EUROCOPTER EASA.IM.R.S.01210 SH8790SW-D EUROCOPTER FRANCE AS Installatino of a Bendix/King GPS KLN 90B or 07.12.2006 CORPORATION 365N2 KLN 900 for IFR en route operations in EUROCOPTER FRANCE SA accordance with AEC Drawing List 365A73- 365N1 9060, revision C, dated 02/03/2005, or later EASA approved revision. 10016943 AMERICAN EUROCOPTER EASA.IM.R.S.01337 FAA STC SH8803SW-D EUROCOPTER FRANCE AS Installation of combination position lights and Compatibility of this modification with 13.06.2007 CORPORATION 365N2 strobe lights with supplemental anti-collision previously approved modifications must be EUROCOPTER FRANCE SA lights replacing the red, green and white determined by the installer. 365N1 position lights.. 10016944 AMERICAN EUROCOPTER EASA.IM.R.S.01338 FAA STC SH7018SW-D EUROCOPTER FRANCE AS Installation of 4.0 inch Footwell in the Compatibility of this modification with 13.06.2007 CORPORATION 365N2 passenger cabin of the Model SA365A73- previously approved modifications must be EUROCOPTER FRANCE SA 365N1 9022. determined by the installer. 10033895 AMERICAN EUROCOPTER FAA STC SR09094RC-D EC 135 P1 (CDS) Installation of a collective activated tenth None. Prior to installation of this modification it 17.02.2011 CORPORATION EC 135 P1 (CPDS) hourmeter in accordancewith AEC Drawing List must be determined thatthe EC 135 P2 (CPDS) 135A82-8006.This EASA STC is based on interrelationship between this modification EC 135 P2+ FAA STC SR9094RC-D. and any other previouslyinstalled EC 135 T1 (CDS) modification and/ or repair will introduce EC 135 T1 (CPDS) no adverse effectupon the airworthiness EC 135 T2 (CPDS) EC 135 T2+ of the product. 10035015 AMERICAN EUROCOPTER REV. 1 FAA STC NO. SR09262RC-D EC135 P1(CDS), EC135 Installation of a Belly and Fin Strobe lights in None. Prior to installation of this modification it 23.05.2011 CORPORATION P1(CPDS), accordance with AECDrawing List 135A82- must be determined thatthe EC135 P2(CPDS), EC135 P2+, 8018. interrelationship between this modification EC135 T1(CDS), EC135 and any other previouslyinstalled T1(CPDS), modification and/ or repair will introduce EC135 T2(CPDS), EC135 T2+ no adverse effectupon the airworthiness of the product. 10035617 AMERICAN EUROCOPTER CORPORATION 10035996 AMERICAN EUROCOPTER CORPORATION FAA STC SH8171SW-D SA 365 N1,AS 365 N2 Installation of Bendix /King EFIS 40 Electronic none If the holder agrees to permit another Flight InstrumentationSystem in accordance person to use this certificate toalter the with AEC Drawing List 365A73-9051Revision B product, the holder shall give the other dated10/1/93 or Bendix /King EFIS 50 person writtenevidence of that Electronic Flight InstrumentationSystem in permission.Prior to installation of this accordance with AEC Drawing List 365A73- modification it must be determined thatthe interrelationship FAA STC SR09306RC-D MBB-BK 117-C2 Installation of tailboom mounted aft ballast in accordance with AmericanEurocopter Drawing List 145A82-8006. None Compatibility of this modification when more than 4.5 kg of additionalequipment is installed on the tailboom has to be determined prior toinstallation.Prior to installation of this modification it must be determined thatthe interrelationship between this m 04/01/2013 Page 73/462 05.07.2011 03.08.2011
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04/01/2013 Page 1/462 - EASA

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