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 />
10039855 AMERICAN EUROCOPTER<br />
FAA STC SR09137RC-D EC 135 P2, EC 135 P2+<br />
Installation of an Extended Right Hand side none Prior to installation of this modification it 30.05.2<strong>01</strong>2<br />
CORPORATION<br />
EC 135 T1, EC 135 T2<br />
Instrument Panel inaccordance with AEC<br />
must be determined thatthe<br />
EC 135 T2+, EC 135 P1<br />
Drawing List 135A82-8020.This <strong>EASA</strong> STC is<br />
interrelationship between this modification<br />
based on validation of FAA STC SR09137RC-<br />
and any other previouslyinstalled<br />
D (Amdt.10-May-2<strong>01</strong>2) iaw the TIP.<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>04</strong>1261 AMERICAN EUROCOPTER<br />
CORPORATION<br />
10<strong>01</strong>6415 AMERICAN PROPELLER SERVICE <strong>EASA</strong>.IM.A.S.02747 FAA STC SA5896NM CESSNA 210F<br />
CESSNA 210G<br />
CESSNA 210H<br />
CESSNA 210J<br />
CESSNA 210K<br />
CESSNA 210L<br />
CESSNA 210M<br />
10<strong>01</strong>4425 AMES - AEROSPACE AND<br />
MECHANICAL<br />
10<strong>01</strong>4680 AMES - AEROSPACE AND<br />
MECHANICAL<br />
10<strong>01</strong>4681 AMES - AEROSPACE AND<br />
MECHANICAL<br />
10<strong>01</strong>4818 AMES - AEROSPACE AND<br />
MECHANICAL<br />
10<strong>01</strong>5009 AMES - AEROSPACE AND<br />
MECHANICAL<br />
10<strong>01</strong>53<strong>01</strong> AMES - AEROSPACE AND<br />
MECHANICAL<br />
10027678 AMES - AEROSPACE AND<br />
MECHANICAL<br />
10035593 AMES - AEROSPACE AND<br />
MECHANICAL<br />
10036300 AMES - AEROSPACE AND<br />
MECHANICAL<br />
FAA STC SR091<strong>04</strong>RC-D EC135 P1, P2, P2+, T1, T2, T2+ Installation of a pulsed engine and gearbox chip None Prior to installation of this modification it 03.09.2<strong>01</strong>2<br />
detector system inaccordance with AEC<br />
must be determined thatthe<br />
Drawing List 135A82-8009.<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 />
<strong>EASA</strong>.A.S.02470 CESSNA 208<br />
CESSNA 208A<br />
CESSNA 208B<br />
Installation of a McCauley D3A34C4<strong>04</strong>/80VA-0 As defined in FAA STC SA5896NM1 Prior to<br />
Propeller.<br />
installation of this modification the installer must<br />
determine that the interrelationship between<br />
this modification and any other previously<br />
installed modification will introduce no<br />
adverse effect upon th<br />
Mount assembly for external side loads for<br />
Cessna 208 models<br />
<strong>EASA</strong>.A.S.02841 CESSNA 550 Supplemental Type Certificate for Cargo Net CRI A-02; Registration: OE-GAD; S/N C550-<br />
Installation on C550 MSN 00<strong>01</strong>-0626 0071<br />
<strong>EASA</strong>.A.S.02842 CESSNA 551 Supplemental Type Certificate for Cargo Net CRI A-02Registration (if applicable): OE-<br />
Installation on C551 MSN 00<strong>01</strong>-0549 FADSerial number (if applicable): C551-<strong>04</strong>96<br />
<strong>EASA</strong>.A.S.03026 REV. 2 A320 Installation of an In-Flight Entertainment<br />
System (Live TV) on AirbusA320 Aircraft<br />
02.10.2008<br />
07.06.2006<br />
12.02.2007<br />
13.<strong>04</strong>.2007<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 />
05.11.2<strong>01</strong>0<br />
<strong>EASA</strong>.A.S.03311 BEECH 400A Activation of Garmin MX-20 Multifunction<br />
Display.<br />
None. 13.08.2008<br />
<strong>EASA</strong>.A.S.03862 FALCON 2000 Falcon 2000 MSN209 Interior Refurbishment. 1. Limited to A/C Falcon 2000, MSN 209.2.<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 up<br />
11.05.2009<br />
P-<strong>EASA</strong>.A.S.03803 REV. 1 A330-223 Airbus A330 - 200 B/C ISPSS Installation This STC is limited to the following Serial<br />
Numbers:MSN 403, 432, 444, 454, 469, 476,<br />
493<br />
REV. 1 737-700 AND 737-800 B737-800/-700 Live TV System Removal / This STC is only applicable for aircraft which<br />
Major Change to <strong>EASA</strong> STC 10035593to have been previouslymodified with FAA<br />
implement B737-700 as effective aircraftAMES Supplemental Type Certificate ST02887AT.<br />
will use FAA approved Live TV documentation<br />
such as but not limitedto: Drawings, Structural<br />
substantiation reports, ELA and W&B fo<br />
767-300 B767-300 Astronics EMPower 110VAC<br />
activation.<br />
Prior to installation of this modification it 25.05.2<strong>01</strong>0<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 />
Prior to installation of this modification it 09.11.2<strong>01</strong>2<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 />
<strong>EASA</strong> STC <strong>EASA</strong>.IM.A.S.<strong>01</strong>257 must be Prior to installation of this modification it 29.08.2<strong>01</strong>1<br />
installed prior to the accomplishmentof the must be determined thatthe<br />
changes of this approval, andThe installation of interrelationship between this modification<br />
the In-Seat components is not covered with and any other previouslyinstalled<br />
thisapproval and must be approved prior to the modification and/ or repair will introduce<br />
accomplishment of the changesdetailed no adverse effectupon the airworthiness<br />
of the product.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 74/<strong>462</strong>
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