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>4615 AVIONIK STRAUBING ENTWICKLUNGS <strong>EASA</strong>.A.S.02744 PIPER PA-46-310P<br />
Installation of COM/NAV/GS/GPS GNS430, This STC is approved only for the product<br />
07.05.2007<br />
GmbH<br />
PIPER PA-46-350P<br />
with GDC31 Roll Steering<br />
configuration as defined in the approved design<br />
Converter.Installation of Diversity Mode S data referred to in the paragraphs "Description"<br />
XPDR Garmin GTX330D.Installation of TCAS and “Associated Technical Documentation”.<br />
Avidyne TAS610.<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined<br />
10<strong>01</strong>4705 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10<strong>01</strong>4772 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10<strong>01</strong>4773 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10<strong>01</strong>4802 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10<strong>01</strong>4811 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10<strong>01</strong>5159 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10<strong>01</strong>5229 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
<strong>EASA</strong>.A.S.02876 BEECH 65-90<br />
BEECH 65-A90<br />
BEECH B90<br />
BEECH C90<br />
BEECH C90A<br />
BEECH E90<br />
<strong>EASA</strong>.A.S.02964 FAIRCHILD SWEARINGEN SA<br />
226-AT<br />
FAIRCHILD SWEARINGEN SA<br />
226-T<br />
FAIRCHILD SWEARINGEN SA<br />
226-T(<br />
FAIRCHILD SWEARINGEN SA<br />
227-AT<br />
Dual Installation of COM/NAV/GS/GPS Prior to installation of this modification the<br />
GNS430, with GDC31 Roll Steering Converter; installer must determine that the<br />
Installation of Stormscope WX500 and TCAS interrelationship between this modification and<br />
Avidyne TAS610.<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
Installation of Mode S XPDR Diversity Garmin<br />
GTX 330D with now top Antenna.<br />
Prior to installation of this modification the<br />
installer msut 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.<br />
<strong>EASA</strong>.A.S.02965 CESSNA 525 Installation of one Garmin GNS530 in a Cessna Prior to installation of this modification the<br />
525.<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 installa<br />
<strong>EASA</strong>.A.S.03005 CESSNA 525<br />
CESSNA 525A<br />
<strong>EASA</strong>.A.S.03<strong>01</strong>6 CESSNA 525A Installation of single/ dual Garmin GTX<br />
330DModel: Cessna 525A, S/N 00<strong>01</strong> and on<br />
<strong>EASA</strong>.A.S.03528 FAIRCHILD SWEARINGEN SA<br />
226-AT<br />
FAIRCHILD SWEARINGEN SA<br />
226-T<br />
FAIRCHILD SWEARINGEN SA<br />
226-T(<br />
FAIRCHILD SWEARINGEN SA<br />
226-TC<br />
FAIRCHILD SWEARINGEN SA<br />
227-AC<br />
FAIRCHILD SWEARINGEN SA<br />
227-BC<br />
FAIRCHILD SWEARINGEN SA<br />
227-DC<br />
<strong>EASA</strong>.A.S.03647 CESSNA 5<strong>01</strong><br />
CESSNA 551<br />
Installation of Garmin GTX330D single/dual. Limited to Cessna 525, SN 00<strong>01</strong>-<br />
0359.Compatibility of this modification with<br />
other previously approved modifications must<br />
be determined by the installer.<br />
Installation of honeywell Mark VI EGPWS -<br />
Optional installation of Comant CI4<strong>01</strong>-220 GPS<br />
Antenna.<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 />
Installation of COM/NAV/GS/GPS Garmin 1. Prior to installation of this modification the<br />
GNS430W (AW) or COM/NAV/GS/GNS530W installer must determine that the<br />
(AW).<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 />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 102/<strong>462</strong><br />
12.07.2007<br />
16.10.2007<br />
19.09.2008<br />
08.02.2007<br />
21.06.2007<br />
06.05.2008<br />
18.11.2008
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