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>04</strong>2309 ASSOCIATED AIR CENTER, L.P. FAA STC ST10913SC A319-133 Validation of FAA STC ST10913SC - This modification is applicable to MSN 4992. Prior to installation of this modification it 22.11.2<strong>01</strong>2<br />
Installation of an Executive interior.<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>6730 ASTEC HELICOPTER SERVICES AS <strong>EASA</strong>.IM.R.S.<strong>01</strong><strong>04</strong>8 - S-61N Installation of Honeywell MST 67A Mode S<br />
Transponder<br />
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 />
10<strong>01</strong>7091 ASTEC HELICOPTER SERVICES AS <strong>EASA</strong>.R.S.<strong>01</strong>002 REV. 1 AS 332L, AS 332L1, AS 332L2 Skywatch SKY-497 Traffic Advisory System 1. 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 />
10<strong>01</strong>7092 ASTEC HELICOPTER SERVICES AS <strong>EASA</strong>.R.S.<strong>01</strong>003 REV. 1 Techtest CPI-503 ELT 1. 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 />
10<strong>01</strong>6500 ASTRONICS ADVANCED ELECTRONIC <strong>EASA</strong>.IM.A.S.02862 FAA STC ST02535AT BOEING 747-400 Installation of a General Dynamics EmPower Prior to installation of this modification the<br />
AC In-Seat powerSupply System on a Boeing installer must determine that the<br />
747-400 type aircraft in accordance with interrelationship between this modification and<br />
Master Drawing list MDL1091-3, Rev. C, dated any other previously installed modification will<br />
August 6, 2002, or later FAA approved revision introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
10<strong>01</strong>4147 ATELIER CHABORD <strong>EASA</strong>.A.S.<strong>01</strong>266 APEX DR 400/100<br />
APEX DR 400/120<br />
APEX DR 400/120A<br />
APEX DR 400/120D<br />
APEX DR 400/125<br />
APEX DR 400/2+2<br />
10037356 ATELIER CHABORD F150F, F150G, F150H, F150J<br />
F150K, F150L, F150M<br />
FA150K, FA150L, FA150M<br />
10039166 ATELIER CHABORD REV. 1 CESSNA 172R, 172S Exhaust system and silencer for general<br />
aviation aeroplanes<br />
10<strong>01</strong>6626 ATLANTIC AERO INC <strong>EASA</strong>.IM.A.S.03061 FAA STC ST00026AT CESSNA 208 Installation of Passenger Interior And Cargo<br />
Door Modification inCessna Caravan (Cargo<br />
Conversion)<br />
10<strong>01</strong>6627 ATLANTIC AERO INC <strong>EASA</strong>.IM.A.S.03062 FAA STC SA00<strong>01</strong>54AT CESSNA 208<br />
CESSNA 208A<br />
CESSNA 208B<br />
22.11.2005<br />
18.11.2005<br />
15.11.2005<br />
23.07.2008<br />
nstallation of exhaust system and silencer 02.12.2005<br />
STC CESSNA150-11-<strong>01</strong> Rev E - Dispositif de Tout Reims Aviation Cessna F150F a M. Prior to installation of this modification it 22.11.2<strong>01</strong>1<br />
boite de réchauffagecarburateur additionnel sur FA150K a M modifié selon le STC38-SF-00<strong>01</strong> must be determined thatthe<br />
ensemble collecteur d'échappement et ou toute révision ultérieure.<br />
interrelationship between this modification<br />
silencieux.<br />
and any other previouslyinstalled<br />
modification and/or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
Installation of Cabin Windows in the Cargo<br />
versions of Cessna 208 series<br />
10028652 ATLANTIC AERO, Inc. FAA STC ST02635AT LEARJET 35, 35A, 36, 36A Deactivation of Aeronca (Learjet) Thrust<br />
Reversers<br />
10029557 ATLANTIC AERO, Inc. FAA STC SA<strong>01</strong>539AT-D 206, P206, P206A, P206B, P206D Installation of a Remote Mounted Oil Cooler in<br />
P206E, TP206A, TP206C, accordance with AtlanticAero Inc. Master<br />
TP206D<br />
Drawing List 166930<strong>01</strong>, Rev. Basic, dated<br />
TU206C, TU206D, TU206E, December 5,1997 or later FAA approved<br />
TU206F<br />
revision in accordance with FAA<br />
TU206G<br />
U206, U206A, U206B, U206C,<br />
U206D, U206E, U206F, U206G,<br />
STCSA<strong>01</strong>539AT-D<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 />
23.<strong>04</strong>.2<strong>01</strong>2<br />
- 16.12.2008<br />
15.12.2008<br />
Not Applicable Not Applicable <strong>01</strong>.02.2<strong>01</strong>0<br />
None None <strong>01</strong>.<strong>04</strong>.2<strong>01</strong>0<br />
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