04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
<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>5096 AIRPLUS MAINTENANCE GmbH <strong>EASA</strong>.A.S.03433 BEECH B200 Installation of SKY899 Transmitter Receiver<br />
Computer and Directional Antenna NY164<br />
Installation.<br />
14.02.2008<br />
10<strong>01</strong>5219 AIRPLUS MAINTENANCE GmbH <strong>EASA</strong>.A.S.03634 PIPER PA-42 Installation of the Garmin GNS530, Junction Prior to installation of this modification the<br />
<strong>04</strong>.05.2009<br />
Boxes, GMA 340, EX-500 and GTX330D in installer must determine that the<br />
Piper PA-42 Series.<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 />
10<strong>01</strong>5240 AIRPLUS MAINTENANCE GmbH <strong>EASA</strong>.A.S.03667 KING AIR 200 Installation of Dual Garmin COMM/NAV/GPS<br />
GNS430AW or GNS430Wand/or<br />
Avidyne EX500 MFD interfaced with existing<br />
WX Radarand/or L3-Com A100S<br />
1. Restricted to aircraft which have already<br />
approved antenna locations for thenew<br />
equipment.GNS430(A)W installations<br />
restricted to aircraft which have already the<br />
Cockpit Voice Recorderand/or Single followingequipment installed, completely<br />
Counter Pointer Drum Altimeter<br />
independend from the Garmin GNS430(A)W<br />
units:VHF tr<br />
10028933 AIRPLUS MAINTENANCE GmbH P-<strong>EASA</strong>.A.S.03609 PA-46-310P Installation of Garmin GNS530W, GNS430W None Prior to installation of this modification the 19.02.2<strong>01</strong>0<br />
and GMA347.<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 installati<br />
100290<strong>04</strong> AIRPLUS MAINTENANCE GmbH CESSNA 5<strong>01</strong>, 551 Installation of Avidyne TAS 620 and Honeywell None Prior to installation of this modification it 25.02.2<strong>01</strong>0<br />
KGP 860<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 />
10029265 AIRPLUS MAINTENANCE GmbH P-<strong>EASA</strong>.A.S.03811 REV. 1 SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
Enabeling of SVT Functionalities on Garmin<br />
G5/600 System (Revision of<strong>EASA</strong> STC<br />
10029265)<br />
10029716 AIRPLUS MAINTENANCE GmbH P-<strong>EASA</strong>.A.S.03907 REV. 1 SEE APPROVED MODEL LIST Enabling of SVT Functionalities on Garmin<br />
G5/600 Avionics System(Revision of <strong>EASA</strong><br />
STC 10029716)<br />
The aircraft must have been already equipped<br />
with Garmin G5/600System(s) according to<br />
<strong>EASA</strong> STC 10029265.<br />
The aircraft must have been already equipped<br />
with Garmin G5/600System(s) according to<br />
<strong>EASA</strong> STC 10029716<br />
11.03.2009<br />
Prior to installation of this modification it 19.12.2<strong>01</strong>2<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 />
Prior to installation of this modification the<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 />
10032902 AIRPLUS MAINTENANCE GmbH SC <strong>01</strong>, SC <strong>01</strong>B Inspection Program to increase operating None<br />
product.<br />
Prior to installation of this modification it 07.12.2<strong>01</strong>0<br />
hoursMM Modification of chapter IV<br />
must be determined thatthe<br />
Airworthiness Limitations - Implementationof<br />
interrelationship between this modification<br />
Inspection Program to increase operating hours<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10034024 AIRPLUS MAINTENANCE GmbH <strong>EASA</strong> APPROVED MODEL LIST Dual Installation of Garmin GNS 430<br />
(A)W/GNS 530 (A)W (TAWS).<br />
10034382 AIRPLUS MAINTENANCE GmbH 1.BEECH 58, 58A, G58<br />
2.BEECH 58P, 58PA, 58TC,<br />
58TCA<br />
Dual Installation of Garmin GNS430(A)W /<br />
GNS530(A)W(TAWS)<br />
03.12.2<strong>01</strong>2<br />
None The antenna installation is not covered by 28.02.2<strong>01</strong>1<br />
this STC. The aircraft musthave been<br />
already equipped with suitable antennas.<br />
Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other prev<br />
None The antenna installation is not covered by 30.03.2<strong>01</strong>1<br />
this STC.The aircraft must have been<br />
already equipped with suitable antennas.<br />
Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other prev<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 68/<strong>462</strong>
Change language