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 />
10039242 AVIATION SUPPORT GmbH 0<strong>01</strong>0<strong>01</strong>2<strong>01</strong>0-0<strong>01</strong> FOCA STC 25-70-<strong>01</strong>2 EC135 T2 Installation of an external Ski Basket<br />
None Prior to installation of this modification it 19.<strong>04</strong>.2<strong>01</strong>2<br />
Equipment P/N AV 115.00<br />
must be determined thatthe<br />
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 />
10<strong>01</strong>5418 AVIATION TECHNICAL SERVICES, Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>141 FAA STC ST00988SE-D BOEING 757-200 Installation of an Interior Arrangement, Avionics 1. This STC is approved only for the product<br />
& Ozone Converters.<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
10<strong>01</strong>5543 AVIATION TECHNICAL SERVICES, Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>428 ST00299SE-D BOEING 737-300<br />
BOEING 737-400<br />
BOEING 737-500<br />
Modification of an 87MCU FMC Tray to accept<br />
a 4MCU FMC LRU according to FAA STC<br />
ST00299SE-D<br />
10<strong>01</strong>6147 AVIATION TECHNICAL SERVICES, Inc. <strong>EASA</strong>.IM.A.S.02348 FAA STC SA7030NM-D BOEING 737-300 Installation of Allied Signal p/n 967-<strong>01</strong>02-0<strong>01</strong><br />
Digital Flight Data Acquisition Unit (DFDAU)<br />
and necessary sensors and wiring to record<br />
Twenty Two (22) Parameters of data per<br />
Tramco Incorporated Master Drawing List 95-<br />
180 Sheet 1 Revision A dated January 12<br />
10<strong>01</strong>6176 AVIATION TECHNICAL SERVICES, Inc. <strong>EASA</strong>.IM.A.S.02405 FAA STC SA5115NM BOEING 737-300 Installation of a Collins Traffic Alert and<br />
Collision Avoidance System (TCAS II)<br />
Transmitter/Receiver with Honeywell<br />
TA/RA/IVSI´s.<br />
10<strong>01</strong>6177 AVIATION TECHNICAL SERVICES, Inc. <strong>EASA</strong>.IM.A.S.02406 US FAA STC SA4978NM BOEING 737-300 Installation of Traffic Alert and Collision<br />
Avoidance System (TCAS) provisions<br />
10029541 AVIATION TECHNICAL SERVICES, Inc. P-<br />
<strong>EASA</strong>.IM.A.S.02553<br />
10029850 AVIATION TECHNICAL SERVICES, Inc. P-<br />
<strong>EASA</strong>.IM.A.S.02613<br />
FAA STC ST00051SE BOEING 737-400 Installation of a Collins Traffic Alert and<br />
Collision Avoidance System(TCAS II)<br />
Transmitter/Receiver per Goodrich ATS, Inc<br />
Top Drawing 93<strong>04</strong>6Revision F dated 05<br />
January 20<strong>01</strong>.<br />
FAA STC ST00631SE-D B737-800 Interior Reconfiguration - Installation of an<br />
Interior Arrangement,Entertainment System<br />
Components and Avionics Components.<br />
11.<strong>04</strong>.2005<br />
According to FAA STC ST00299SE-D 29.09.2005<br />
1. Approval of this change in Type Design<br />
applies to the above model aircraft only. This<br />
approval should not be extended to other<br />
aircraft of this model on which other previously<br />
approved modifications are incorporated<br />
unless it is determined that the<br />
27.02.2007<br />
1. 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.2.<br />
22.<strong>04</strong>.2009<br />
This approval is applicable only to the electrical<br />
provisions for TCAS and does not approve the<br />
actual TCAS installation or any TCAS<br />
equipment.<br />
12.07.2007<br />
None. Prior to installation of this modification it<br />
must be determined thatthe<br />
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 />
30.03.2<strong>01</strong>0<br />
Not Applicable Prior to installation of this modification it<br />
must be determined thatthe<br />
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 />
26.<strong>04</strong>.2<strong>01</strong>0<br />
10<strong>01</strong>40<strong>01</strong> AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.<strong>01</strong>038 BOEING 757-200 Installation of Enhanced Mode S Transponders 17.03.2005<br />
10<strong>01</strong>4002 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.<strong>01</strong>039 BOEING 737-700 Installation of Enhanced Mode S Transponders 17.03.2005<br />
10<strong>01</strong>4003 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.<strong>01</strong><strong>04</strong>0 BOEING 737-300 Installation of Enhanced Mode S Transponders 17.03.2005<br />
10<strong>01</strong>4163 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.<strong>01</strong>295 Installation of Teledyne Flight Data Acquisition<br />
Unit P/N 2233000-811 to provide parameters<br />
to the FDR<br />
22.11.2005<br />
10<strong>01</strong>4175 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.<strong>01</strong>310 COMMANDER AIRCRAFT 114B Wing auxiliary Spar Repair 13.10.2005<br />
10<strong>01</strong>4254 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.<strong>01</strong>479 BOEING 707-300 Avionics Upgrade 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 />
15.10.2008<br />
10<strong>01</strong>4322 AVIATION TRADERS LIMITED - ATL <strong>EASA</strong>.A.S.<strong>01</strong>575 REV. 1 AIRBUS A300 B4 Introduction of Enhanced Mode S Transponder This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 93/<strong>462</strong><br />
14.09.2006
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