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 />
10029947 AVIONIK STRAUBING ENTWICKLUNGS<br />
CESSNA 340, 340A Installation of Thommen AD32 Air Data None Prior to installation of this modification it 05.05.2<strong>01</strong>0<br />
GmbH<br />
Display/Altimeter and AvionikStraubing Altitude<br />
must be determined thatthe<br />
Preselect System APS4A<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 />
10030025 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
1003<strong>04</strong><strong>04</strong> AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10031180 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10032176 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10033937 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
100346<strong>01</strong> AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10034991 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10035162 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
PA-31-325, PA31-350<br />
PA-31P, PA-31T, PA-31T1,<br />
PA-31T2, PA-31T3, PA-31,<br />
REV. 1 1. PA-31, PA-31-325, PA-31-350<br />
2. PA-31P, PA-31T, PA-31T1<br />
2. PA-31T2<br />
REV. 1 1. PA-32-260, PA-32-300<br />
1. PA-32R-300, PA-32RT-300<br />
1. PA-32R-3<strong>01</strong>T, PA-32-3<strong>01</strong><br />
1. PA-32RT-300T, PA-32R-3<strong>01</strong><br />
2. PA-32-3<strong>01</strong>XTC, PA-32-3<strong>01</strong>FT<br />
REV. 1 31<strong>01</strong>,3102,3103,3107,3108<br />
3109,3110,3112,3116,32<strong>01</strong><br />
3202,3206,3207,3212,3216,3217<br />
Installation of Avidyne TAS 610/620/9900BX,<br />
Transponder Couplers andBottom/Top TAS<br />
Antennas<br />
EC 120 B Panel Modification including position change of<br />
ApolloMX20(GarminGMX200),HSI Indicator KI<br />
525 and installation of new Attitude Indicator<br />
and Moving Terrain MT-Vision MFD.<br />
210, 210-5, -5A<br />
210A, B, C, D, E, F, G, H, J<br />
210K, L, M, N, R<br />
P210N, R<br />
T210F, G, H, J, K, L, M, N, R<br />
SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
PA-28-150, -160, -235, -2<strong>01</strong>T<br />
PA-28-180, -181, -161, -140<br />
PA-28-236, -151<br />
PA-28R-180, -200, -2<strong>01</strong>, -2<strong>01</strong>T<br />
PA-28RT-2<strong>01</strong>, -2<strong>01</strong>T<br />
Dual/Single installation of Garmin<br />
GNS430(A)W/530(A)W with GPS<br />
AntennaGarmin GA35 and Roll Steering<br />
Converter DAC GDC31.<br />
Dual/Single Installation of Garmin<br />
GNS430(A)W / GNS530(A)W<br />
Dual/Single Installation of Garmin<br />
GNS430(A)W I GNS530(A)W and<br />
optionalInstallation of Marker Receiver<br />
Honeywell (Bendix/King) KMR675<br />
Dual/Single Installation of Garmin<br />
GNS430(A)W / GNS530(A)W.<br />
Restricted to aircraft which have Avidyne<br />
EX500/600 MFD, Garmin GDU620PFD,<br />
Garmin GNS430(A)W or Garmin<br />
GNS530(A)W system installed in orderto<br />
display the information.<br />
Prior to installation of this modification it 12.05.2<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 />
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 />
15.06.2<strong>01</strong>0<br />
none Prior to installation of this modification the 13.09.2<strong>01</strong>0<br />
installer must determinethat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product.The installatio<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 />
18.10.2<strong>01</strong>0<br />
none Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other<br />
previouslyinstalledmodification and/or<br />
repair will introduce no adverse effect<br />
upon theairworthiness of the product.<br />
24.02.2<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 />
14.<strong>04</strong>.2<strong>01</strong>1<br />
Installation of PFD Aspen EFD1000 PRO. None. The Installation of the Avionik Straubing<br />
Altitude Preselect SystemAPS4A is<br />
optional.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<br />
Installation of dual GPS/NAV/COMM Garmin<br />
GNS430/530(A)W.<br />
None. Dual installation of Garmin GNS<br />
430/530(A)W requires a third<br />
independentCOMM device or an<br />
independent NAV/DME or ADF/DME<br />
combination.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and an<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 1<strong>04</strong>/<strong>462</strong><br />
18.05.2<strong>01</strong>1<br />
31.05.2<strong>01</strong>1
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