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 />
10035456 AVIONIK STRAUBING ENTWICKLUNGS<br />
F406 Cockpit Upgrade basing on dual Garmin G600 Only applicable for Aircraft S/N 097 and up A third, fully independent COMM device 24.06.2<strong>01</strong>1<br />
GmbH<br />
and GNS430W<br />
must have been already installed.Prior to<br />
installation of this modification it must be<br />
determined thatthe interrelationship<br />
between this modification and any other<br />
previouslyinstalled modification and/ or<br />
repair will<br />
10036102 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10036149 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10036230 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10036231 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10036587 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10036677 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10036784 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10036858 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
REV. 1 DA 40, 40D, 40F Installation of PFD Aspen EFD1000 PRO. 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 />
17.08.2<strong>01</strong>1<br />
REV. 1 1. PA-31-325, PA-31-350,<br />
1. PA-31, PA-31-300,<br />
2. PA-31P, PA-31P-350,<br />
2. PA-31T, PA-31T1,<br />
2. PA-31T2, PA-31T3<br />
SR20, SR22 Installation of a Primary Function Display<br />
Avidyne EXP5000<br />
The aircraft must have been already equipped<br />
with suitable GPS system.<br />
Prior to installation of this modification it 16.08.2<strong>01</strong>1<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 />
5<strong>01</strong>, 551 Installation of a TAS SystemL3 Communication The aircraft must have been already equipped Prior to installation of this modification it 23.08.2<strong>01</strong>1<br />
SKY899<br />
with a suitableMultifunction Display.<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 />
208, 208B Installation of a Satellite Antenna Chelton HGA- none Prior to installation of this modification it 23.08.2<strong>01</strong>1<br />
7000<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 />
Installation of one or more Avionik Straubing<br />
Heater Control Unit(s)HCU200.<br />
60, A60, B60 Installation of a Traffic Advisory System<br />
Avidyne TAS 605/615/620,Ryan<br />
9900BX<br />
BEECH 60, A60, AND B60 Installation of Garmin G600 System with<br />
Synthetic Vision Technology(SVT).<br />
60, A60, B60 Installation of a Satellite Data Link System<br />
Garmin GSR56.<br />
None. The HCU200 as approved together with<br />
this STC must be produced andqualified<br />
in accordance with Avionik Straubing<br />
Declaration of Design andPerformance<br />
(DDP) ASR-1038-HCU200-002-DDP-<br />
02.Prior to installation of this modification<br />
it must be determined thatthe<br />
<strong>04</strong>.10.2<strong>01</strong>1<br />
None The aircraft must already have been<br />
equipped with a suitableMultifunction<br />
Display.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or re<br />
28.09.2<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 />
06.10.2<strong>01</strong>1<br />
None. The aircraft must already have been<br />
equipped with a suitableMultifunction<br />
Display.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or re<br />
12.10.2<strong>01</strong>1<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 105/<strong>462</strong>
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