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>5244 AVIONIK STRAUBING ENTWICKLUNGS <strong>EASA</strong>.A.S.03679 CESSNA 4<strong>01</strong><br />
Installation of Single or Dual Garmin G600 1) Prior to installation of this modification the<br />
15.06.2009<br />
GmbH<br />
CESSNA 4<strong>01</strong>A<br />
Avionics System and dual Garmin<br />
installer must determine that the<br />
CESSNA 4<strong>01</strong>B<br />
GNS4/530(A)W GPS/COMM/NAV<br />
interrelationship between this modification<br />
CESSNA 402<br />
andany other previously installed modification<br />
CESSNA 402A<br />
will introduce no adverse effect upon the<br />
CESSNA 402B<br />
CESSNA 402C<br />
CESSNA 4<strong>04</strong><br />
CESSNA 406<br />
CESSNA 411<br />
CESSNA 411A<br />
CESSNA 414<br />
CESSNA 414A<br />
CESSNA 421<br />
CESSNA 421A<br />
CESSNA 421B<br />
CESSNA 421C<br />
CESSNA 425<br />
CESSNA 441 SERIES<br />
CESSNA F406<br />
airworthiness of the product.2) The ins<br />
10026784 AVIONIK STRAUBING ENTWICKLUNGS P-<strong>EASA</strong>.A.S.03917 REV. 1 PIPER PA-46-310P<br />
Installation of Single or Dual Garmin G500 / This STC is limited to the configuration of Prior to installation of this modification the 23.<strong>04</strong>.2<strong>01</strong>0<br />
GmbH<br />
PIPER PA-46-350P<br />
G600 Avionics System(including SVS) and aircraft, equipment type,and functions as listed installer must determinethat the<br />
PIPER PA-46-500TP<br />
Dual Garmin GNS4/530(A)W<br />
in <strong>EASA</strong> approved Instructions for<br />
interrelationship between this modification<br />
PIPER PA-46R-350T<br />
GPS/COMM/NAV.<br />
Installation,Doc. No. ASR-2009-075-IFI-10-00, and any otherpreviously installed<br />
Amdt. Level 00, dated 18-Jun-2009,especially modification will introduce no adverse<br />
as mentioned in Item 2. of this docume effect uponthe airworthiness of the<br />
product. The installati<br />
10026941 AVIONIK STRAUBING ENTWICKLUNGS P-<strong>EASA</strong>.A.S.03675 BEECH 60, A60, B60 Installation of Garmin GNS430W /<br />
None 1) Prior to installation of this modification 25.08.2009<br />
GmbH<br />
GNS430AW / GNS430 / GNS530W /<br />
the installer mustdetermine that the<br />
GNS530AW/ GNS530, with Installation of<br />
interrelationship between this modification<br />
Garmin GA35/GA56 GPS Antenna.<br />
and anyother previously installed<br />
modification will introduce no adverse<br />
effectupon the airworthiness of the<br />
product. 2) The inst<br />
10028197 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10028486 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10028816 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10029814 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
10029856 AVIONIK STRAUBING ENTWICKLUNGS<br />
GmbH<br />
P-<strong>EASA</strong>.A.S.03875 B90, C90, C90A, C90GT, C90GTI,<br />
E90, F90<br />
P-<strong>EASA</strong>.A.S.03916 MOONEY M20 C, E, F, G, J, K<br />
MOONEY M20 L, M, R, S<br />
Installation of an FMS System Universal UNS-<br />
1Lw and an EGPWS KGP 560<br />
None The installation of an LP/LPV Monitor is<br />
optional<br />
08.12.2009<br />
SEE ATTACHED MODEL LIST Installation of an Aspen EFD-1000 ProSystem. None. Prior to installation of this modification the 15.<strong>01</strong>.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.<br />
PA-46-310P, -350P,<br />
PA-46-500TP, PA-46R-350T<br />
1) M20C, M20E, M20F, M20G,<br />
1) M20J, M20K, M20L,<br />
2) M20M, M20R, M20S<br />
Installation of Aspen EFD1000 PRO System. None. Prior to installation of this modification the 11.02.2<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.<br />
Installation of a Stormscope Avidyne TWX670 None This STC is also applicable to Turbine<br />
Converted Aircraft (PA46-310-DLX,PA46-<br />
350DLX) according to FAA STC<br />
ST00541SE. Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other previous<br />
22.<strong>04</strong>.2<strong>01</strong>0<br />
Installation of a Garmin G500 System 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 />
26.<strong>04</strong>.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 103/<strong>462</strong>
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