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 10039720 SNAKY CREEK ENTERPRISES, LLC FAA STC SR02977CH AW109SP EASA Validation of FAA STC SR02977CH None Prior to installation of this modification it 04.06.2012 "Installation of a medical floorliner in must be determined thatthe accordance with RSG AeroDesign Master interrelationship between this modification Document List00A02160003, No Revision, and any other previouslyinstalled dated February 23, 2011, or later FAA modification and/ or repair will introduce approvedrevisions" no adverse effectupon the airworthiness of the product. 10039721 SNAKY CREEK ENTERPRISES, LLC FAA STC SR02980CH AW109SP EASA Validation of FAA STC SR02980CH "Installation of an interior panelsystem in accordance with RSG AeroDesign Master Document List00A02160001, No Revision, dated February 23, 2011, or later FAA approvedrevisions" 10041098 SNAKY CREEK ENTERPRISES, LLC FAA STC SA02488CH PC-12 PC-12/45 PC-12/47 Air Ambulance Conversion Install air ambulance conversion in accordance with Spectrum AeromedInc. Master Drawing List 6045DL, dated July 23, 2007 or later FAAapproved revisions. 10014506 SOCATA EASA.A.S.02576 TBM 700 STC 34.001.06/Gamin GNS530 TAWS. TBM 700 equipped Garmin GNS 530 only s/n to 433 excepted 269. 10014524 SOCATA EASA.A.S.02607 TB 200 Validation of definition specificities of TB200 STC 53.001.06 applicable to TB200 s/n 1633 S/N 1633 aircraft, compared to TB200 GT certified aircraft definition only 10015065 SOCATA EASA.A.S.03391 SOCATA TBM 700 Installation of a multi-functions display Garmin This revision can be installed on TBM 700 s/n GMX 200 connected to already installed to 433 when equipped with EADS SOCATA equipments (weather radar, COM/NAV/GPS, optional Modifications n° OPT 70-23-019, OPT Traffic Advisory System). 70-23-018, OPT 70-34-047 and OPT 70-34- 040.The installation can be performed only by EADS SOCATA technical staff according to t 10029243 SOCATA P-EASA.A.S.03962 REV. 4 TB 20 TB 21 Installation of Garmin G500 EFIS Interfaced with a dual Garmin GNS430W/530W communication and navigation system, for IFR B-RNAV/P-RNAVoperations with coupling to autopilot.Revision 3 of the STC including the extent to RNP LNAV and LPV approachoperations.Re 10040655 SOCATA DHC-6 SERIES 300 Avionics upgrade based on Garmin G600 EFIS and GNS 430 W system,according to SOCATA modification file n° STC.00.001.11 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. 18.05.2012 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. 21.08.2012 The modified airplane must be equipped with:- an attitude indicator, an airspeed indicator, an altitude indicator, amagnetic heading indicator and a radionavigation indicator independentfrom the G500 EFIS,- a third radionavigation or radiocommunciati This design change is limited to airplanes s/n 292, 298, 300, 730 and745. Initial installation must be performed by authorised Socata technicalpersonel. This avionics installation is approved for IFR operations in BRNAV,PRNAV, RNP approach LNAV and LPV app 10042727 SOCATA TB20, TB21 Installation of TAS Garmin GTS800 This STC is not applicable to airplanes equipped with a 14 V electricalsystem.Initial Installation of this design change must be performed byauthorized SOCATA personal.Modified airplanes must be equipped with Socata modification No.34-001-009 approved unde 10028245 SOCATA SAS P-EASA.A.S.03961 REV. 2 TBM 700 N Installation of a Honeywell HF KHF 1050 communication system on aircraftTBM 700 N equipped with Garmin 1000 Glass Cockpit System - Update forICA inclusion 30.01.2008 20.07.2006 06.02.2008 Prior to installation of this modification it 23.10.2012 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 17.07.2012 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. Prior to installation of this modification it 14.12.2012 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. 26.08.2010 04/01/2013 Page 412/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10036696 SOCATA SAS AS 355 F2 Installation of Provisions for WESCAM MX-10 Serial Numbers 5026, 5299, 5298, 5156 only Configuration is limited to the installation 30.09.2011 Camera installation of the following defined asprovisions:- UHF FM antenna for DR 3000 UHF relay;- GPS antenna for WESCAM camera MX-10;- The remote screen display is removed but its mounting bracket isinstalled;- Footswitch - is re 10014399 SOCIETE AIR FRANCE EASA.A.S.01693 REV. 1 BOEING 767 Cabin Reconfiguration from Eva Air to Aeroflot FAA STC SA5950NM (Door 2 Aft Galley Standard Installation) is not included in this approval. 10014463 SOCIETE AIR FRANCE EASA.A.S.02524 BOEING 777-200 Air France B777-200 "Ulysse" cabin Limited to Aircraft serial numbers as defined in modification with Contour (CAS B777-04-003) Air France document CAS B777-04-003 and or BEA business class seats (CAS B777-05- 015). CAS B777-05-015 10014465 SOCIETE AIR FRANCE EASA.A.S.02526 AIRBUS A320-211 Photo-luminescent EEPM system installation This STC is limited to the A320 MSN's 211, 215 and 270 10014501 SOCIETE AIR FRANCE EASA.A.S.02568 A320 Cabin Reconfiguration in bi-classes on LAN 1. Limited to installation on MSN 1304, 1332, A320 1351 and 1355.2. Compatibility of this design change with other previously approved modifications must be determined by the installer. 10014531 SOCIETE AIR FRANCE EASA.A.S.02617 BOEING 737-300 ATC Mode S-Enhanced Surveillance-Provision 1. Limited to installation on Boeing 737-300/- BOEING 737-500 and Activation on Boeing 737-300/-50 in 500.2. Compatibility of this design change with accordance with the Modification File MF-B737- other previously approved modifications must 06-004, Rev 00, dated 11 October 2006. be determined by the installer. 10014611 SOCIETE AIR FRANCE EASA.A.S.02738 AIRBUS A340-300 THY A340 Cabin Retrofit Modification 16.05.2007 10014663 SOCIETE AIR FRANCE EASA.A.S.02820 REV 1 BOEING 737-300 Installation of elementary surveillance Dual 1. Limited to installation on Boeing 737-300/- 23.10.2006 BOEING 737-500 ATC Mode S on B737-300/-500 in accordance 500.2. Compatibility of this design change with with the Modification File MDF-B737-04-004, other previously approved modifications must Rev 01, dated 11 October 2006. be determined by the installer. 10027295 SOCIETE AIR FRANCE P-EASA.A.S.03975 REV. 2 A320 Cabin Reconfiguration from Dragon Aviation Leasing to Juneyao Standard(DKH) Revision of the EASA STC 10027295 to remove EWIS limitation 10032363 SOCIETE AIR FRANCE A340-211, A340-212 A340 Royal Jordanian - New IFE and Cabin reconfigurationThis STC consists in a cabin reconfiguration by installing newecoconomic class seat and a new In-Flight Entertainment (IFE) system(Sicma Aero IFE SiT). 17.07.2006 03.11.2006 06.06.2006 30.10.2006 23.10.2006 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 23.11.2010 This STC is applicable to the following aircraft MSNs :,,- MSN 14,,- MSN 22,,- MSN 38,,- MSN 43 10038157 SOCIETE AIR FRANCE 777-200 Alitalia Cabin Reconfiguration 777-200 MSN as defined in Change approval sheet CAS-B777-11-003 10042281 SOCIETE AIR FRANCE 747-400 CorsairFly cabin reconfiguration and SiT IFE installation.Cabin refurbishment and new IFE system installation. 10042639 SOCIETE AIR FRANCE A319-111, A319-113, A320-211, A320-212, A321-111, A321-212. Installation of the ACARS (Aircraft Communication Addressing andReporting System) CMU-900 to replace the Teledyne MUA45B Prior to installation of this modification it 29.10.2010 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 24.01.2012 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 Before installation of this STC, EASA STC No. EASA.IM.A.S.00677 must beincorporated.Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or 21.11.2012 This approval is applicable to the following Prior to installation of this modification it 12.12.2012 MSN:61 ; 63 ; 102 ; 115 ; 144 ; 145 ; 155 ; 186 must be determined thatthe ; 187 ; 214 ; 227 ; 236 ;237 ; 239 ; 270 ; 278 ; interrelationship between this modification 285 ; 286 ; 287 ; 337 ; 352 ; 377 ; 491 ; 498 and any other previouslyinstalled ;509 ; 521 ; 529 ; 544 ; 598 ; 600 ; 608; 618 ; modification and/ or repair will introduce 625 ; 637 ; 777 ; 7 no adverse effectupon the airworthiness of the product. 10014926 SOCIETE D'ETUDE ET DE GESTION EASA.A.S.03176 BEECH 200 Installation of a support base for a stretcher. 08.10.2007 04/01/2013 Page 413/462
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04/01/2013 Page 1/462 - EASA

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