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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>5620 GENERAL AEROSPACE INC <strong>EASA</strong>.IM.A.S.<strong>01</strong>572 FAA STC ST03138AT BOEING 737-200<br />

Installation of Honeywell Enhanced Ground According to FAA STC ST03138AT 03.03.2006<br />

BOEING 737-300<br />

Proximity Warning System according to FAA<br />

BOEING 737-400<br />

BOEING 737-500<br />

STC ST03138AT<br />

10<strong>01</strong>5639 GENERAL AEROSPACE INC <strong>EASA</strong>.IM.A.S.<strong>01</strong>602 FAA STC ST03126AT BOEING 737-100<br />

Installation of a honeywell RESCU 406AF According to FAA STC ST03126AT 29.11.2005<br />

BOEING 737-200<br />

Emergency locator transmitter (ELT) System<br />

BOEING 737-300<br />

BOEING 737-400<br />

BOEING 737-500<br />

according to FAA STC STO3126AT<br />

10<strong>01</strong>6072 GENERAL AEROSPACE INC <strong>EASA</strong>.IM.A.S.02253 FAA STC ST<strong>01</strong>792AT BOEING 757-200 TCAS and Duel Mode-S Transponders<br />

Installation.<br />

17.10.2007<br />

10<strong>01</strong>6466 GENERAL AEROSPACE INC <strong>EASA</strong>.IM.A.S.02812 FAA STC ST03486AT BOEING 737-200<br />

Installation of a Haneywell ARINC 717 Flight<br />

19.03.2008<br />

BOEING 737-300<br />

Data Acquisition Management System<br />

BOEING 737-400<br />

BOEING 737-500<br />

(FDAMS).<br />

10035023 GENERAL AEROSPACE INC <strong>EASA</strong>.IM.A.S.02759 FAA STC SA3169SO B737-200, B737-300<br />

Installation of a Collins Traffic Alert an Collision A copy of this STC must be included in the Prior to installation of this modification the 30.07.2009<br />

B737-400, B737-500<br />

Avoidance Systemand Dual Mode-S<br />

permanent record of theaircraft.<br />

installer must determinethat the<br />

Transponders.<br />

interrelationship between this modification<br />

and any otherpreviously installed<br />

modification will introduce no adverse<br />

effect uponthe airworthiness of the<br />

product. The installati<br />

10<strong>01</strong>6948 GENEVA AVIATION, INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>343 REV. 1 FAA STC SH4747NM EUROCOPTER FRANCE AS 350 Installation of consoles, toggle switches, circuit 1. Prior to installation of this modification the<br />

25.11.2008<br />

B<br />

breakers, and replacement wiring harnesses in installer must determine that the<br />

EUROCOPTER FRANCE AS 350 accordance with MDL GA107.This STC is the interrelationship between this modification and<br />

B1<br />

validation of FAA STC SH4747NM (issued on any other previously installed modification will<br />

EUROCOPTER FRANCE AS 350 July 26, 1989 and last amended August 8, introduce no adverse effect upon the<br />

B2<br />

EUROCOPTER FRANCE AS 350<br />

B3<br />

EUROCOPTER FRANCE AS 350<br />

BA<br />

EUROCOPTER FRANCE AS 350<br />

D<br />

2008).<br />

airworthiness of the product.2.<br />

10<strong>01</strong>6960 GENEVA AVIATION, INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>357 FAA STC SR0<strong>04</strong>74SE EUROCOPTER FRANCE AS 350 Modular Equipment Rack installation per MDL This STC provides approval for structural<br />

03.<strong>04</strong>.2008<br />

B<br />

GA179.<br />

provisions only. A separate approval is required<br />

EUROCOPTER FRANCE AS 350<br />

for the installation of any equipment inthe<br />

B1<br />

EUROCOPTER FRANCE AS 350<br />

B2<br />

EUROCOPTER FRANCE AS 350<br />

B3<br />

EUROCOPTER FRANCE AS 350<br />

BA<br />

EUROCOPTER FRANCE AS 350<br />

C<br />

EUROCOPTER FRANCE AS 350<br />

D<br />

EUROCOPTER FRANCE AS 350<br />

D1<br />

EUROCOPTER FRANCE AS<br />

355E<br />

EUROCOPTER FRANCE AS<br />

355F<br />

EUROCOPTER FRANCE AS<br />

355F1<br />

EUROCOPTER FRANCE AS<br />

355F2<br />

modular equipment rack.<br />

<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 231/<strong>462</strong>

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