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>4323 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.<strong>01</strong>576 BOEING 727 SERIES Introduction of Terrain Awareness & Warning<br />
System (TAWS)<br />
25.<strong>01</strong>.2006<br />
10<strong>01</strong>4358 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.<strong>01</strong>623 BOEING 757-200 Introduction of Enhanced Mode S Transponder 18.<strong>01</strong>.2006<br />
10<strong>01</strong>4372 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.<strong>01</strong>646 BOEING 747-200 Introduction of a Litton 72R INS in a Boeing<br />
747-200 series aircraft<br />
A copy of this Certificate and the <strong>EASA</strong><br />
Approved Flight Manual Supplement (AFMS)<br />
must be maintained as part of the permanent<br />
records for the modified aircraft.<br />
10<strong>01</strong>4499 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.02564 REV. 1 PARTENAVIA P68C Camera Port Installation -- 13.12.2006<br />
10<strong>01</strong>4594 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.02706 BAE 146 Noneywell TCAS II 05.07.2006<br />
10<strong>01</strong>4595 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.02712 Installation of Honeywell MKVII EGPWS. Compatibility of this design with previously<br />
approved modifications must be determined by<br />
the installer.<br />
31.05.2007<br />
10<strong>01</strong>4633 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.02775 BAE 146 Installation of dual AlliedSignal GNS-XLS Flight Restricted to VH-JJY ASN E2113.<br />
Management System<br />
10.05.2007<br />
10<strong>01</strong>4660 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.02817 BOEING 737-300<br />
Mode 'S' Transponder System for Elementary In accordance with Paragraphs 3, 9, 10, 13 & Prior to installation of this modification the 20.07.2009<br />
BOEING 737-400<br />
and EnhancedSurveillanceRevison to 16 of the ModificationSummary ATL/737/M556 installer must determinethat the<br />
BOEING 737-500<br />
<strong>EASA</strong>.A.S.02617 (B737-400 added to existing Issue 1, dated 9th October 2006Compatibility interrelationship between this modification<br />
STC)<br />
of this design change with other previously and any other previouslyinstalled<br />
approvedmodifications must be determined by modification will introduce no adverse<br />
the installer.<br />
effect upon the airworthiness ofthe<br />
product. The installati<br />
10<strong>01</strong>4707 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.02879 BOEING 747-400 SERIES Installation of a Bendix / King CAS-81 TCAS II Prior to installation of the STC Boeing SB 747-<br />
System in B747-400 in accordance with Master 34-2309 must be installed.<br />
Drawing List Drawing No. 699-50021, initial<br />
release and Dual Bendix / King TRA-67 Mode<br />
S Transponder in accordance with Master<br />
Drawing List, Drawing 699-50020, init<br />
10<strong>01</strong>4708 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.02880 BOEING 747-400 SERIES RTA-44D VHF Data Radio System. This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph 4:<br />
Specification Aircraft/Modification.<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer<br />
10<strong>01</strong>4709 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.02881 BOEING 747-400 Certification of Collins Data Link ACARS<br />
Installation in the B747-400<br />
MDL 94-24<strong>Page</strong> Avjet Master Drawing List for<br />
installation of Collins ACARS Part No 622-<br />
9717-00X on B747-400 series aircraft.<br />
10<strong>01</strong>4734 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.02917 BOEING 757-200 238 PAX LOPA Installation 21.03.2007<br />
10<strong>01</strong>4757 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.02945 BOEING 757 2<strong>01</strong>PAX LOPA Installation 03.<strong>04</strong>.2007<br />
10<strong>01</strong>4887 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.03116 BAE 146/AVRO 146 SERIES 95 Passenger LOPA Installation. 05.09.2007<br />
10<strong>01</strong>4940 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.03198 148 Pax LOPA Installation Compatibility of this design change with other<br />
previously approved modifications must be<br />
determined by the installer.<br />
05.09.2008<br />
10<strong>01</strong>4942 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.032<strong>01</strong> BOEING 757-2Q8 219 PAX LOPA Installation. This STC is limited to aircraft s/n 26270. 21.08.2007<br />
10<strong>01</strong>4963 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.03234 BOMBARDIER CL-600-2B16 Introduction of Honeywell Mark V EGPWS. Aviation Traders Ltd Modification ATL/600/003<br />
(<strong>EASA</strong>.A.S.03244) must be embodied prior to,<br />
or concurrently with, Modification<br />
ATL/600/002.Prior to installation of this<br />
modification the installer must determine that<br />
the interrelationship between this modific<br />
18.07.2008<br />
10<strong>01</strong>4967 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.03244 BOMBARDIER CL-600-2B16 EFIS, GPS approach scaling and EGPWS<br />
display<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 />
10<strong>01</strong>4994 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.03291 REV. 2 B757-200 Passenger/ Cargo Combi Configuration This STC is limited to a/c serial number 25621 Prior to installation of this modification it<br />
onlyATL Minor Modification MOD/11630/00003 must be determined thatthe<br />
07.02.2<strong>01</strong>1<br />
must be installed concurrentlywith this STC. interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product<br />
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19.06.2006<br />
22.03.2007<br />
<strong>01</strong>.02.2007<br />
31.<strong>01</strong>.2007<br />
18.07.2008