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 10016015 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02181 FAA STC SA2684CE BOEING DC-9-81 (MD-81) Installation of Dual Collins Mode S None.Registration (if applicable):-Serialnumber 04.01.2007 BOEING DC-9-82 (MD-82) BOEING DC-9-83 (MD-83) BOEING DC-9-87 (MD-87) BOEING MD-88 DC-9-81 (MD-81) Transponders. (if applicable):- 10016059 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02236 ST01580AT-D BOEING 747-400 Installation of radio panels and Collins VHF ¿ Data package containing the following 08.08.2007 transceivers with 8.33 khz spacing in documents, and additional supporting data:¿ accordance with Collins Master Data List MDL- MDL 01237, rev. M: MDL Collins VHF700V/ - 01237, revision M, dated August 9, 2005, or 900B in B747-400.¿ CFG-01296: installation later FAA approved revisions. of Collins VHF-700B communications system on B747-400 for Air France.¿ ENG-0 10016060 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02237 REV. 1 FAA STC ST02410CH-D BAE 125 SERIES 800A Installation of Rockwell Collins Pro Line 21 IDS (Integrated Display System) with IFIS-5000 (Integrated Flight Information System) and Engine Instrument Display. 10016077 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02261 REV. 1 FAA STC ST01901LA BOEING 767-200 BOEING 767-300 10016202 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02444 FAA STC SA01267WI-D BEECH 300 BEECH B300 BEECH B300C 10016212 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02460 FAA STC ST01119WI-D CESSNA 750 FALCON 10 FALCON 900 FALCON 900EX GULFSTREAM IV GULFSTREAM 1159 (G-II) GULFSTREAM 1159 A( G-II) GULFSTREAM 1159 B( G-II) HAWKER HS 125-700A HAWKER HS 125-700B MYSTERE FALCON 50 10016249 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02526 FAA STC ST00040WI-D AIRBUS A320-111 AIRBUS A320-211 AIRBUS A320-212 AIRBUS A320-231 AIRBUS A320-232 10016273 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02558 FAA ST00392AT BOEING 767-200 SERIES BOEING 767-300 SERIES 10016275 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02562 REV. 1 FAA STC ST01470LA-D 737-600, 737-700 737-800, 737-900 10016287 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02582 REV. 1 FAA STC ST01927LA BOEING 757-200 BOEING 757-300 10016378 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02702 FAA STC ST01454WI-D BOMBARDIER CL-600-2B19 BOMBARDIER CL-600-2C10 BOMBARDIER CL-600-2D15 BOMBARDIER CL-600-2D24 Installation of ARINC 718A MODE S Transponder Activation of Elementary and Enhanced Surveillance Capabilities. Installation of Collins Pro Line 21 Avionics System. Modification of Collins TDR-94 or TDR-94D Mode S Transponder System installation with stand-alone Collins TRU-4210 or RTU-4220 Radio Tuning Unit(s) to a Flight ID capable Collins TDR-94 or TDR-94D Mode S Transponder System installation with standalone Col Installation of Collins Traffic Alert and Collision Avoidance System (TCAS II). Installation of Collins Duel TPR-720 Mode S Transponders. 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. 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. The install (1) Approval of this change in type design applies to the above model aircraft only.(2) Compatibility of this design change with previously approved modifications must be determined by the installer.(3) A copy of this Certificate and FAA Approved Model Lis Installation of a Collins TPR-720, TPR 900 or TPR-901 Mode S Transponder is a prerequisite to this modification. 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. The install 28.02.2008 30.06.2008 02.10.2008 26.10.2007 15.10.2007 02.11.2007 Installation of Rockwell Collins WXR-2100 Multi- None. Prior to installation of this modification the 08.07.2008 scan (TM) Weather RadarSystem(Revision to installer must determinethat the the existing STC EASA.IM.A.S.02562 to interrelationship between this modification change the STC holdername and to add more and any otherpreviously installed models and correct the equipment reference modification will introduce no adverse name) effect uponthe airworthiness of the product.The installatio Installation of ARINC Characteristics 718A for Prior to installation of this modification the 15.10.2007 Mode S Transponder Activation of Elementary installer must determine that the and Enhanced Surveillance Capabilities. interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install Modification of a Collins Control Display Unit, Installation, Type CDU-4100 1. Prior installation and approval of a Collins Control Display Unit, type CDU-4100, is a prerequisite to this STC.2. Prior to installation of this modification the installer must determine that the interrelationship between this modification andany other 04/01/2013 Page 370/462 28.07.2008
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016379 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02703 FAA STC ST01431WI-D SEE ATTACHED EASA Modification of a Collins DBU-4000 or DBU- Prior to installation of this modification the 15.10.2008 APPROVED TYP 4100 Data Base Unit installation to a Collins installer must determine that the DBU-5000 installation interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install 10016395 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02724 FAA STC ST01452WI-D Modification of Collins FMS-5000 or FMS 6000 A prior installation and approval of a Collins and installation in Part 25 Airplanes i.a.w. FMS type FMS-5000 or FMS 6000 is a Drawing index as listed in AML Nr. ST01452WI- prerequisite to this STC. Refer to Collins D Rev- pr mater approved revisions approved Installation Instructions RCA-2447 in its latest by EASA i.a.w. EASA ED decision 2004/04/CF revision for approved FMC substitues. (or subsequent revision of this de 10016396 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02725 FAA STC ST00643WI-D BOEING 747-200B BOEING 747-200C BOEING 747-200F BOEING 747-300 10016397 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02726 FAA STC SA01430WI-D BEECH 390 BEECH B200 BEECH B200C BEECH B300 BEECH B300C PIAGGIO P 180 SEE ATTACHED EASA APPROVED TYP 10016398 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02727 FAA STC SA01453WI-D BEECH 300 BEECH 390 BEECH B200 BEECH B300 BEECH B300C CESSNA 525 CESSNA 525A CESSNA 525B PIAGGIO P 180 10016517 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02888 FAA STC SA01434WI-D BEECH 390 BEECH B200 BEECH B200C CESSNA 525 CESSNA 525A CESSNA 525B PIAGGIO P 180 Modification of Collins 618M-3A VHF COMM R/T System Installation to Collins VHF-900B VHF COMM R/T System. Modification of a Collins DBU-4000 or DBU- 4100 Data Base Unit installation to a Collins DBU-5000 Installation. Modification of a Collins Flight Management System type FMS-3000 Installed in Part 23 Aircraft. Modification of Collins GPS-4000 or GPS- 4000A Global Positioning Sensor (GPS) system installation to a Collins GPS-4000S Global Positioning Sensor (GPS) system installation 10016518 ROCKWELL COLLINS, Inc. EASA.IM.A.S.02889 FAA STC ST01433WI-D BEECH 400 Modification of Collins GPS-4000 or GPS- BOMBARDIER BD-100-1A10 4000A Global PositioningSensor installation to (CHALLE BOMBARDIER CL-600-2A12 (CL- 601 BOMBARDIER CL-600-2B16 (CL- 604 BOMBARDIER CL-600-2C10 BOMBARDIER CL-600-2D24 (SERIES CESSNA 560 FALCON 2000 FAN JET FAN JET FALCON SERIES C FAN JET FALCON SERIES D FAN JET FALCON SERIES E FAN JET FALCON SERIES F FAN JET FALCON SERIES G GULFSTREAM 200 GULFSTREAM G150 HAWKER 800 XP HAWKER 850 XP HAWKER 900 XP LEARJET 60 MYSTERE FALCON 20-C5 MYSTERE FALCON 20-D5 MYSTERE FALCON 20-E5 MYSTERE FALCON 20-F5 MYSTERE FALCON 50 a Collins GPS-4000S installation This STC is approved only for the product configuration as defined in the approved design data. Compatibility with other aircraft/engine configurations shall be determined by the installer. 1. Prior installation of Collins DBU-4000 part numbers 622-9865-001/-002 or DBU-4100 part numbers 822-0014-101/-102/-103/-104 is a prerequisite to this STC.2. Prior to installation of this modification the installer must determine that the interrelationshi 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. This STC does not approve WAAS LPVPrior FAA approved installation of Collins GPS-4000 part numbers 822-0931-001/-002/-003 or GPS- 4000A part number 822-1377-001 is a prerequisite to this STCPrior to installation of this modification the installer must deter 04/01/2013 Page 371/462 25.03.2008 20.03.2008 15.10.2008 06.11.2008 04.02.2009 24.07.2008
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04/01/2013 Page 1/462 - EASA

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