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 />
10037583 AVIONIK STRAUBING ENTWICKLUNGS<br />
1. PA-31-350<br />
Installation of Garmin G600 System with None A suitable Garmin GPS System must 08.12.2<strong>01</strong>1<br />
GMBH<br />
1. PA-31, PA-31-300, PA-31-325 Synthetic Vision (SVT)<br />
have been already installed. This STC<br />
2. PA-31P, PA-31P-350<br />
includes the optional installation of<br />
2. PA-31T, PA-31T1, PA-31T2<br />
Avionik StraubingEmergency Power Unit<br />
2. PA-31T3<br />
EPU6A5 and/or Standby Attitude Gyro<br />
AIM 505 and/orAvionik Straubing Altitude<br />
Preselector APS4A. Prior to ins<br />
10037817 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10038943 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10<strong>04</strong><strong>04</strong>68 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10<strong>04</strong>1<strong>04</strong>9 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10<strong>04</strong>1441 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10<strong>04</strong>2720 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10<strong>04</strong>2753 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
10<strong>04</strong>2880 AVIONIK STRAUBING ENTWICKLUNGS<br />
GMBH<br />
1. M20, M20A, M20B, M20C,<br />
M20D<br />
1. M20E, M20F, M20G, M20J<br />
1. M20K, M20L, M20S<br />
2. M20M, M20R<br />
SR20<br />
SR22<br />
Dual/Single Installation of Garmin<br />
GPS/COMM/NAV<br />
GNS430(A)W/GNS530(A)W<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 />
22.12.2<strong>01</strong>1<br />
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 />
23.03.2<strong>01</strong>2<br />
PA-42, PA-42-720, PA-42-1000 Installation of Garmin G600 System with<br />
Synthetic Vision (SVT)<br />
DA40, DA40D, DA40F Dual/Single Installation of Garmin<br />
GPS/COMM/NAV GNS430W / GNS530W.<br />
REV. 1 650 Dual Installation of Flight management System<br />
Universal UNS-1Lw<br />
none A suitable Garmin GPS System must<br />
have been already installed.This STC<br />
includes the optional installation of<br />
Avionik StraubingAltitude Preselector<br />
APS4A and/or Standby Altitude Indicator<br />
Sigmatec5000B-40 and/or Standby<br />
Altitude Indicator United Instruments<br />
05.07.2<strong>01</strong>2<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 />
17.08.2<strong>01</strong>2<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 />
20.09.2<strong>01</strong>2<br />
SC7 SERIES 3 Installation of PFD ASPEN EFD1000 C3 None. This STC includes the optional installation 14.12.2<strong>01</strong>2<br />
of a multifunction displayASPEN<br />
EFD1000 MFD. 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<br />
525, 525A Single Installation of GPS/COMM/NAV System<br />
Garmin GTN725/750.<br />
B200, B200C, B200GT, B200CGT Installation of Flight Management System<br />
Universal UNS-1Lw<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 />
17.12.2<strong>01</strong>2<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 />
21.12.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 106/<strong>462</strong>
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