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 10015129 CHRISTEN-AIRTECH AG EASA.A.S.03480 CESSNA P210N Avionics upgradeBy removing:-NSD 360 HISSA-832B Slaving BoxACK A-30 mod 8 Altitude EncoderGMA-340 Audio PanelAnd installingSN-3500 E-HISSAC 7-35 Airdada ComputerKG-102A Remote GyroGMA-347 Audio Panel Reg.: HB-CZB S/N: P-210-0780 05.03.2008 10015262 CHRISTEN-AIRTECH AG EASA.A.S.03720 CESSNA 210 Avionics UpgradeBy removing the existing:- Prior to installation of this modification the 11.12.2008 COM/NAV 1 + 2- DME - Mode A/C installer must determine that the Transponder- Audio Panel And install the new interrelationship between this modification and Avionics Systems:- GNS 530W any other previously installed modification will COM/NAV/GPS 1- GNS 430W introduce no adverse effect upon the COM/NAV/GPS 2 with GI106A GPS/NAV Indicator- KN 62A DME - GTX 330 Mode S Transponderairworthiness of the product. The install 10031914 CHRISTEN-AIRTECH AG TBM 700 A Avionics Upgrade Out: Dual COM-NAV Bendix- Reg.: D-FIRE,,S/N: 137 The approval holder shall fulfil the 21.09.2010 King KX-165A, GPS Apollo MNS2101, MFD obligations of Part 21, ApolloMX20, Encoder Shadin 8800-T In: COM- Paragraph21.A109. Prior to installation of NAV-GPS Garmin GNS-530W & 430W, MFD this modification it must be determined Garmin GMX-200, Encoder ACKA-30 Mod. 8 thatthe interrelationship between this serial modification and any other previouslyinstalled modification and/ or repai 10036867 CHRISTEN-AIRTECH AG 414A Inst.Traffic alerting S/N: 414A-0233,,,,D-IMUB The approval holder shall fulfill the 13.10.2011 system/StormscopeRemoved:- NIL Installed:- obligations of Part 21, §21.A118A.Prior Garmin GTS800 Traffic Alerting System- L-3 to installation of this modification it must WX500 Stormscope System be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will 10015968 CIRRUS DESIGN CORPORATION EASA.IM.A.S.02119 SA01355WI-D CIRRUS SR20 Validation of FAA STC SA01355WI-D – “Installation of Bendix/King KR87 ADF and/ or KN 62A DME” 10016118 CITATION TECH EASA.IM.A.S.02310 FAA STC ST01395WI CESSNA 500 Installation of Dual Honeywell AM-250 Digital CESSNA 501 Altimeter and Skylight Avionics Air Data CESSNA 550 Interface Adapter ADC-602 AIU and CESSNA 551 associatedequipment to obtain RVSM REIMS AVIATION CESSNA F 177 approval. RG 10016006 CLIPPER AVIATION, Inc. EASA.IM.A.S.02170 FAA STC ST02318NY BOEING 747-400 FREIGHTER Upper Deck seating arrangement for B747- 400BCF as defined in Weber Aircraft installation drawing No. 860014 and Clipper Aviation CLI-2006-003 Rev. A, Master Data List B747-400BCF 10036123 CLIPPER AVIATION, Inc. FAA STC ST02318NY B747-400 Installation of seating configuration on Upper Deck of B747-400 Boeingconverted Special Freighter 10015822 COLUMBIA AVIONICS & AIRCRAFT EASA.IM.A.S.01894 ST01128 BEECH 200 BEECH 200C BEECH 200CT BEECH 200T BEECH 300 BEECH 300LW BEECH B200 BEECH B200CT BEECH B200T BEECH B300 BEECH B300C Installation of Honeywell MK-VIII Enhanced Ground Proximity Warning System (with or without optional EFIS-85B/14 Display). 1. The installer must determine, if this design is compatible with previously approved modifications. If the holder agrees to permit another person to use this certification or alter a product, the holder must give the other person written evidence of t This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraphs "Description" and “Associated Technical Documentation”. Compatibility with other aircraft/engine configurations shall be determined 15.05.2007 04.07.2007 04.04.2007 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. 12.08.2011 04/01/2013 Page 156/462 28.09.2006
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015860 COLUMBIA AVIONICS & AIRCRAFT EASA.IM.A.S.01973 FAA STC SA01156WI CESSNA 501 Installation of dual RVSM compliant IS&S or J2 1. Prior to installation of this modification the 12.02.2009 CESSNA 551 (Kollsman) air data system. 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.2. 10016271 COLUMBIA AVIONICS & AIRCRAFT EASA.IM.A.S.02555 FAA STC ST01149WI CESSNA 500 Installation of IS&S or J2 (Kollsman) Air Data 27.08.2007 CESSNA 550 Systemwith Reduced Vertical Separation CESSNA 560 CESSNA S550 Minimum (RVSM) 10016272 COLUMBIA AVIONICS & AIRCRAFT EASA.IM.A.S.02557 FAA STC ST01252WI CESSNA 560 Vertical Separation Minimum (RVSM) group 1. Prior to installation of this modification the 27.08.2007 CESSNA S550 airworthiness approval of Cessna Modell S550 installer must determine that the and 560 Citation Aircraft interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The i 10016320 COLUMBIA AVIONICS & AIRCRAFT EASA.IM.A.S.02629 REV. 1 FAA STC ST01162WI CESSNA 500 Vertical Separation Minimum (RVSM) group 1. Prior to installation of this modification the 19.03.2009 CESSNA 501 airworthiness approval of Cessna Models 500, installer must determine that the CESSNA 550 501, 550 and 551 Citation Aircraft interrelationship between this modification and CESSNA 551 any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2. 10016321 COLUMBIA AVIONICS & AIRCRAFT EASA.IM.A.S.02630 FAA STC ST01084WI Installation of Collins TCAS-4000 TCAS II System (with or without optional Avidyne Flight Max 800 MFD. 03.06.2008 10015895 COMMUTER AIR TECHNOLOGY EASA.IM.A.S.02015 REV. 1 FAA STC SA00184LA BEECH 200 Installation of Alternate Main Landing Gear Prior to installation of this modification the 10.02.2009 BEECH 200C Tires, Michelin P/N 026-335-0.Revision 1 installer must determine that the BEECH 200CT issued to add models B200GT and B200CGT. interrelationship between this modification and BEECH 200T any other previously installed modification will BEECH A200 introduce no adverse effect upon the BEECH A200C BEECH A200CT BEECH B200 BEECH B200C BEECH B200CT BEECH B200T airworthiness of the product. 10016204 COMMUTER AIR TECHNOLOGY EASA.IM.A.S.02446 FAA STC SA10370SC RAYTHEON A36 Installation of exhaust gas extractors on Pratt & Note that the airspeed and shaft horsepower Whitney Canada PT6A-21, -27, -28, -29, -34, - limits listed in the original Airplane Flight 21.05.2007 34B, -135, or 135A turboprop engines. Manuals are still applicable (see TC DataSheet No. 3A20). Compatibility of this design change with previously approved modifications must be determined by the install 10029892 COMPAGNIE FRANCE AVIATION P-EASA.A.S.03869 GARDAN GY80-160 Installation of Aspen Avionics EFD1000 PRO, 1 Garmin GMA340, 1 GarminGNS 430 and 1 Kannad 406MHZ AF Compact in the GARDAN GY-80 series. 10033572 COMPAGNIE FRANCE AVIATION P-EASA.A.S.03031 R2160 FA 07/2007 Edition 1 - Installation malonnier sur R2160 10015540 COMTEK ADVANCED STRUCTURES Ltd. 10034405 COMTRAN INTERNATIONAL, INC. P- EASA.IM.A.S.02963 None. Prior to installation of this modification it must be determined thatthe interrelationship between this and any other previously installedand/ or repair will introduce no adverse upon the EASA.IM.A.S.01424 - DORNIER D328-100 Replacement of trolley stowage unit panels 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. FAA STC SA00664DE DORNIER 328-300 Cabin Interior Re-Configuration Domier 328- 300 10015738 CONCORDE BATTERY CORPORATION EASA.IM.A.S.01762 FAA STC ST00640LA HAWKER 1000 Installation of Cocorde Battery Model No RG- 380E/60K sealed lead acid batteries 10016315 CONCORDE BATTERY CORPORATION EASA.IM.A.S.02620 FAA STC NO. ST01173WI LEARJET 45 Installation of Concorde RG-443 Lead Acid Battery. 30.04.2010 Limited to S/N 154 airworthiness of theproduct. 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. 28.07.2009 18.07.2005 None Prior to installation of this modification the 29.07.2009 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. The installati -- 06.04.2006 04/01/2013 Page 157/462 05.02.2008
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04/01/2013 Page 1/462 - EASA

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