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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 />

<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 370/<strong>462</strong><br />

28.07.2008

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