04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
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<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10<strong>01</strong>6<strong>01</strong>5 ROCKWELL COLLINS, Inc. <strong>EASA</strong>.IM.A.S.02181 FAA STC SA2684CE BOEING DC-9-81 (MD-81) Installation of Dual Collins Mode S<br />
None.Registration (if applicable):-Serialnumber<br />
<strong>04</strong>.<strong>01</strong>.2007<br />
BOEING DC-9-82 (MD-82)<br />
BOEING DC-9-83 (MD-83)<br />
BOEING DC-9-87 (MD-87)<br />
BOEING MD-88<br />
DC-9-81 (MD-81)<br />
Transponders.<br />
(if applicable):-<br />
10<strong>01</strong>6059 ROCKWELL COLLINS, Inc. <strong>EASA</strong>.IM.A.S.02236 ST<strong>01</strong>580AT-D BOEING 747-400 Installation of radio panels and Collins VHF ¿ Data package containing the following<br />
08.08.2007<br />
transceivers with 8.33 khz spacing in<br />
documents, and additional supporting data:¿<br />
accordance with Collins Master Data List MDL- MDL <strong>01</strong>237, rev. M: MDL Collins VHF700V/ -<br />
<strong>01</strong>237, revision M, dated August 9, 2005, or 900B in B747-400.¿ CFG-<strong>01</strong>296: installation<br />
later FAA approved revisions.<br />
of Collins VHF-700B communications system<br />
on B747-400 for Air France.¿ ENG-0<br />
10<strong>01</strong>6060 ROCKWELL COLLINS, Inc. <strong>EASA</strong>.IM.A.S.02237 REV. 1 FAA STC ST02410CH-D BAE 125 SERIES 800A Installation of Rockwell Collins Pro Line 21 IDS<br />
(Integrated Display System) with IFIS-5000<br />
(Integrated Flight Information System) and<br />
Engine Instrument Display.<br />
10<strong>01</strong>6077 ROCKWELL COLLINS, Inc. <strong>EASA</strong>.IM.A.S.02261 REV. 1 FAA STC ST<strong>01</strong>9<strong>01</strong>LA BOEING 767-200<br />
BOEING 767-300<br />
10<strong>01</strong>6202 ROCKWELL COLLINS, Inc. <strong>EASA</strong>.IM.A.S.02444 FAA STC SA<strong>01</strong>267WI-D BEECH 300<br />
BEECH B300<br />
BEECH B300C<br />
10<strong>01</strong>6212 ROCKWELL COLLINS, Inc. <strong>EASA</strong>.IM.A.S.02460 FAA STC ST<strong>01</strong>119WI-D CESSNA 750<br />
FALCON 10<br />
FALCON 900<br />
FALCON 900EX<br />
GULFSTREAM IV<br />
GULFSTREAM 1159 (G-II)<br />
GULFSTREAM 1159 A( G-II)<br />
GULFSTREAM 1159 B( G-II)<br />
HAWKER HS 125-700A<br />
HAWKER HS 125-700B<br />
MYSTERE FALCON 50<br />
10<strong>01</strong>6249 ROCKWELL COLLINS, Inc. <strong>EASA</strong>.IM.A.S.02526 FAA STC ST00<strong>04</strong>0WI-D AIRBUS A320-111<br />
AIRBUS A320-211<br />
AIRBUS A320-212<br />
AIRBUS A320-231<br />
AIRBUS A320-232<br />
10<strong>01</strong>6273 ROCKWELL COLLINS, Inc. <strong>EASA</strong>.IM.A.S.02558 FAA ST00392AT BOEING 767-200 SERIES<br />
BOEING 767-300 SERIES<br />
10<strong>01</strong>6275 ROCKWELL COLLINS, Inc. <strong>EASA</strong>.IM.A.S.02562 REV. 1 FAA STC ST<strong>01</strong>470LA-D 737-600, 737-700<br />
737-800, 737-900<br />
10<strong>01</strong>6287 ROCKWELL COLLINS, Inc. <strong>EASA</strong>.IM.A.S.02582 REV. 1 FAA STC ST<strong>01</strong>927LA BOEING 757-200<br />
BOEING 757-300<br />
10<strong>01</strong>6378 ROCKWELL COLLINS, Inc. <strong>EASA</strong>.IM.A.S.02702 FAA STC ST<strong>01</strong>454WI-D BOMBARDIER CL-600-2B19<br />
BOMBARDIER CL-600-2C10<br />
BOMBARDIER CL-600-2D15<br />
BOMBARDIER CL-600-2D24<br />
Installation of ARINC 718A MODE S<br />
Transponder Activation of Elementary and<br />
Enhanced Surveillance Capabilities.<br />
Installation of Collins Pro Line 21 Avionics<br />
System.<br />
Modification of Collins TDR-94 or TDR-94D<br />
Mode S Transponder System installation with<br />
stand-alone Collins TRU-4210 or RTU-4220<br />
Radio Tuning Unit(s) to a Flight ID capable<br />
Collins TDR-94 or TDR-94D Mode S<br />
Transponder System installation with standalone<br />
Col<br />
Installation of Collins Traffic Alert and Collision<br />
Avoidance System (TCAS II).<br />
Installation of Collins Duel TPR-720 Mode S<br />
Transponders.<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product.<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
(1) Approval of this change in type design<br />
applies to the above model aircraft only.(2)<br />
Compatibility of this design change with<br />
previously approved modifications must be<br />
determined by the installer.(3) A copy of this<br />
Certificate and FAA Approved Model Lis<br />
Installation of a Collins TPR-720, TPR 900 or<br />
TPR-9<strong>01</strong> Mode S Transponder is a<br />
prerequisite to this modification.<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
28.02.2008<br />
30.06.2008<br />
02.10.2008<br />
26.10.2007<br />
15.10.2007<br />
02.11.2007<br />
Installation of Rockwell Collins WXR-2100 Multi- None. Prior to installation of this modification the 08.07.2008<br />
scan (TM) Weather RadarSystem(Revision to<br />
installer must determinethat the<br />
the existing STC <strong>EASA</strong>.IM.A.S.02562 to<br />
interrelationship between this modification<br />
change the STC holdername and to add more<br />
and any otherpreviously installed<br />
models and correct the equipment reference<br />
modification will introduce no adverse<br />
name)<br />
effect uponthe airworthiness of the<br />
product.The installatio<br />
Installation of ARINC Characteristics 718A for Prior to installation of this modification the<br />
15.10.2007<br />
Mode S Transponder Activation of Elementary installer must determine that the<br />
and Enhanced Surveillance Capabilities. interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
Modification of a Collins Control Display Unit,<br />
Installation, Type CDU-4100<br />
1. Prior installation and approval of a Collins<br />
Control Display Unit, type CDU-4100, is a<br />
prerequisite to this STC.2. Prior to installation<br />
of this modification the installer must determine<br />
that the interrelationship between this<br />
modification andany other<br />
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28.07.2008