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 />
10033778 GAMA ENGINEERING Ltd. P-<strong>EASA</strong>.A.S.03724 CESSNA 310 Introduction of a GDC31 autopilot roll steering None Prior to installation of this modification it 27.07.2009<br />
converter<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. The in<br />
10034337 GAMA ENGINEERING Ltd. SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
10034531 GAMA ENGINEERING Ltd. SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
10034814 GAMA ENGINEERING Ltd. SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
100377<strong>01</strong> GAMA ENGINEERING Ltd. SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
10037800 GAMA ENGINEERING Ltd. A) BN2A-8, BN2A-9, BN2A-20<br />
A) BN2A-21, BN2A-26<br />
A) BN2A-27, BN2B-20, BN2B-21<br />
A) BN2B-26, BN2B-27, BN2T<br />
A) BN2T-4R, BN2T-4S<br />
B) BN2A MARK III-3<br />
B) BN2A MARK III, III-1, III-2<br />
10039502 GAMA ENGINEERING Ltd. BN.2A MARK III TRISLANDER,<br />
BN.2A MARK III-1 TRISLANDER,<br />
BN.2A MARK III-2 TRISLANDER,<br />
BN.2A MARK III-3 TRISLANDER.<br />
Navigation/Communications Upgrade. 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 />
25.03.2<strong>01</strong>1<br />
Installation of Garmin G500 EFIS PFD/ND. 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 />
11.<strong>04</strong>.2<strong>01</strong>1<br />
Navigation/ communications upgrade 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 />
03.05.2<strong>01</strong>1<br />
GNS-W Navigation System Qualification 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 />
16.12.2<strong>01</strong>1<br />
GNS-W Navigation System Qualification in<br />
accordance with MDL-1275, Issue2.<br />
Installation of Aspen EFD1000 Electronic<br />
Primary Flight Display<br />
None None 22.12.2<strong>01</strong>1<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 />
08.05.2<strong>01</strong>2<br />
10<strong>04</strong>1163 GAMA ENGINEERING Ltd. P2006T Wingtip pyrotechnics & LED lights. As per: Flight manual supplement AFMS -1306 As per: Flight manual supplement AFMS - 24.08.2<strong>01</strong>2<br />
& Instructions for ContinuedAirworthiness ICA- 1306 & Instructions for<br />
1306.<br />
ContinuedAirworthiness ICA-1306. Prior<br />
to installation of this modification it must<br />
be determined thatthe interrelationship<br />
between this modification and any other<br />
previouslyinstalled modifica<br />
10<strong>01</strong>5372 GARMIN INTERNATIONAL, Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>023 SA<strong>01</strong>254WI DIAMOND DA-40 Installation of Garmin G1000 in the DA40 and<br />
DA40F airplane<br />
1. Hartzell Propeller STC <strong>EASA</strong>.IM.A.S.<strong>01</strong>644<br />
must be installed2. Diamond Aircraft Inductries<br />
Modifications listed in Garmin Drawing 005-<br />
003<strong>04</strong>-00 Rev 10 or later approved revision<br />
must be installed<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 229/<strong>462</strong><br />
11.08.2006
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