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>4810 AVIONITEC Ltd. <strong>EASA</strong>.A.S.03<strong>01</strong>5 CESSNA 5<strong>01</strong> Replacement of XPDR to GARMIN GTX 330D<br />
Diversity Mode S and change of GPS interface<br />
29.<strong>01</strong>.2008<br />
10<strong>01</strong>4846 AVIONITEC Ltd. <strong>EASA</strong>.A.S.03067 PIPER PA-31T1 Replacing of existing avionics by newer<br />
generation of avionics in accordance with Unit<br />
change overview Nr. 063247-050.<br />
Limited to S/N 31T-79<strong>04</strong><strong>01</strong>4 17.<strong>01</strong>.2008<br />
10<strong>01</strong>4858 AVIONITEC Ltd. <strong>EASA</strong>.A.S.03082 PIPER PA-60-6<strong>01</strong>P Avionics retrofitOut. Radar system Bendix RDR-Reg.:<br />
HB-LIN S/N: 571-7963248/<br />
150; VHF-COM King KY-196; VHF-NAV King<br />
KN-53, Indicators KI-252A, KI-2<strong>04</strong>, and KI-226;<br />
ADF system King KR-87 incl. Antenna KA-44B,<br />
obsolete ADF antenna Collins ANT-650A and<br />
adapter ADA-650, Moving map Eventide A<br />
08.10.2007<br />
10<strong>01</strong>4864 AVIONITEC Ltd. <strong>EASA</strong>.A.S.03088 MOONEY M20J Installation of replaced Avionics according CP<br />
No. 073372<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<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.<br />
10<strong>01</strong>4916 AVIONITEC Ltd. <strong>EASA</strong>.A.S.03162 PIPER PA-28R-2<strong>01</strong>T Replacing of existing avionics by newer<br />
generation of avionics in accordance with Unit<br />
change overview Nr. 073528-050, Rev 0,<br />
dated11.06.07.<br />
Limited to S/N T21059922. 08.05.2008<br />
10<strong>01</strong>4986 AVIONITEC Ltd. <strong>EASA</strong>.A.S.03278 REV. 1 Avionics TetrofitOut: King Mode A/C<br />
Transponder KT-76A, king Audio Panel KMA-<br />
24, Autopilot Badin Crouzet.In: Garmin Mode S<br />
Transponder GTX-330, Garmin Audio Panel<br />
GMA-340, Autopilot S-Tec System 55X.<br />
Reg.: HB-DCE, S/N 420. 06.09.2007<br />
10<strong>01</strong>5064 AVIONITEC Ltd. <strong>EASA</strong>.A.S.03390 CESSNA T210L Replacing of existing avionics by newer<br />
generation of avionics in accordance with Unit<br />
change overview Nr. 073775-050, Rev 0,<br />
dated05.12.07.<br />
10<strong>01</strong>51<strong>04</strong> AVIONITEC Ltd. <strong>EASA</strong>.A.S.03447 BEECH F90 Avionics replacing: Garmin GTX330D XPDR<br />
and Weather Radar System RDR 2000.<br />
10<strong>01</strong>5163 AVIONITEC Ltd. <strong>EASA</strong>.A.S.03534 PIPER PA-46-350P Avionics upgrade to GNS 430, Removed<br />
Equipment:- KX-165 NAV/COM 2- KI-206 NAV<br />
2 IndicatorInstalled Equipment- GNS-430<br />
NAV/COM/GPS 2- GI-106A NAV/GPS<br />
Indicator 2- GA-56 GPS 2 Antenna<br />
21.11.2008<br />
Limited to S/N T21059922. 27.02.2008<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 installa<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.Reg.: HB-PPH<br />
10<strong>01</strong>5191 AVIONITEC Ltd. <strong>EASA</strong>.A.S.03575 COMMANDER AIRCRAFT RC114 Avionics Retrofit Removed Equipment: - KMA 1. Prior to installation of this modification the<br />
23.12.2008<br />
20 Audio Panel- Isocom Intercom - Dual KX installer must determine that the<br />
155 COM/NAV- KI 203 NAV #2 Indicator- GPS interrelationship between this modification and<br />
#1, Garmin GPS 100 incl. Antenna- OEM any other previously installed modification will<br />
vacuum Directional Gyro- KT 76A Transponder- introduce no adverse effect upon the<br />
Narco ELT 10 New installed Equipment:- GMA airworthiness of the product. The i<br />
340<br />
10<strong>01</strong>5278 AVIONITEC Ltd. <strong>EASA</strong>.A.S.03794 PIPER PA-46-350P (MALIBU Installation Weather avoidance systems and Reg.: HB-POY, SN: <strong>462</strong>2090 10.03.2009<br />
MIRAG<br />
TAS and ME406 ELT by installation of:-<br />
Avidyne MFD EX 500- Avidyne Traffic Advisory<br />
system TAS 610- Avidyne Tactical Weather<br />
detection System TWX 670- Avidyne Iridium<br />
Data Link Transceiver MLX 770- Artex ME406<br />
ELT<br />
10033155 AVIONITEC Ltd. T303 Avionics RetrofitRemoved: -Garmin GNS 430 Limited to: HB-LUV, S/N T30300058 The approval holder shall fulfil the 21.12.2<strong>01</strong>0<br />
NAV/COM/GPS-King KX 165 NAV/COM with<br />
obligations of Part 21,<br />
King KI 206 Indicator-ARC RTA 476A DME-<br />
Paragraph21.A109. Prior to installation of<br />
ARC R-446A ADF with ARC IN 346A<br />
this modification it must be determined<br />
IndicatorInstalled:-Garmin GNS 530W<br />
thatthe interrelationship between this<br />
NAV/COM/GPS (upgrade from a Garmin GNS<br />
modification and any other<br />
430)-Garmin GNS 430W NAV/COM/GP<br />
previouslyinstalled modification and/ or<br />
repai<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 107/<strong>462</strong><br />
23.09.2008<br />
30.06.2008
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