04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10039496 AVIONICS INTEGRATION &<br />
35A/36A Replacement of UNS-1M by UNS-1Fw MMMS None Prior to installation of this modification it 08.05.2<strong>01</strong>2<br />
ENGINEERING<br />
(UASC)<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 />
10<strong>04</strong>1282 AVIONICS INTEGRATION &<br />
ENGINEERING<br />
CL-600-2B16 CPDLC System Capability CPDLC system not compliant with<br />
Commission Regulation (EC) 29/2009<br />
10<strong>01</strong>4074 AVIONICS MOBILE DESIGN SERVICES <strong>EASA</strong>.A.S.<strong>01</strong>166 BAE JETSTREAM 31<br />
Installation of Airborne Collision Avoidance<br />
BAE JETSTREAM 32<br />
System (ACASII)<br />
10<strong>01</strong>4139 AVIONICS MOBILE DESIGN SERVICES <strong>EASA</strong>.A.S.<strong>01</strong>252 CESSNA 550<br />
Installation of an Airborne Collision Avoidance<br />
CESSNA 650<br />
System (ACAS II)<br />
10<strong>01</strong>4184 AVIONICS MOBILE DESIGN SERVICES <strong>EASA</strong>.A.S.<strong>01</strong>322 CN 235M-100 Installation of a Ground Proximity Warning Aircraft Registration A40-CU and A40-<br />
10<strong>01</strong>4198 AVIONICS MOBILE DESIGN SERVICES <strong>EASA</strong>.A.S.<strong>01</strong>341 BAE 125-800<br />
system (GPWS) & Terrain Awareness Warning CVSerial numbers C062 and C063<br />
System (TAWS)<br />
Installation of an Airborne Collision Avoidance<br />
System (ACAS II)<br />
10<strong>01</strong>4215 AVIONICS MOBILE DESIGN SERVICES <strong>EASA</strong>.A.S.<strong>01</strong>376 CESSNA 550 SERIES<br />
Avionics Mobile Services Modification<br />
CESSNA 560 SERIES<br />
AM/1478. Installation of an Airborne Collision<br />
Avoidance System (ACAS II)<br />
10<strong>01</strong>4303 AVIONICS MOBILE DESIGN SERVICES <strong>EASA</strong>.A.S.<strong>01</strong>547 PIPER PA-31T2 Certification of FAA Approved field modificains<br />
for the issue of an <strong>EASA</strong> C of A.Avionics<br />
Mobile Services AFM supplement Part 21-008<br />
<strong>01</strong>4 GNS-530,Avionics Mobile Services AFM<br />
supplement Part 21-008 <strong>01</strong>5 KMH-<br />
880Avionics Mobile Services AFM supplement<br />
Part 21-<br />
Applicable to s/n 5<strong>04</strong>2 onlyPrior to<br />
installation of this modification it must be<br />
determined thatthe interrelationship<br />
between this modification and any other<br />
previouslyinstalled modification and/ or<br />
repair will introduce no adverse<br />
effectupon the airworthi<br />
10<strong>01</strong>4431 AVIONICS MOBILE DESIGN SERVICES <strong>EASA</strong>.A.S.02479 1124A WESTWIND II Installation of Airborne Collision Avoidance<br />
System (ACAS II)<br />
13.03.2006<br />
10<strong>01</strong>4480 AVIONICS MOBILE DESIGN SERVICES <strong>EASA</strong>.A.S.02543 REV 2 HAWKER HS 125-700 SERIES Installation of an Airborne Collision Avoidance This STC is approved only for the product<br />
09.10.2006<br />
REV 2<br />
System (ACASII)Amendment of the above to configuration as defined in the approved design<br />
include installation variations for alternate data referred to in the paragraph "Description".<br />
aircraft with regard to the Downlink Aircraft Compatibility with other aircraft/engine<br />
Parameters (DAP's) for Mode-S Enhanced configurations shall be determined by the<br />
Surveillance (EHS)<br />
installer.<br />
10<strong>01</strong>4481 AVIONICS MOBILE DESIGN SERVICES <strong>EASA</strong>.A.S.02544 HS 125-700 SERIES Installation of a Digital Air Data Display System -- 06.<strong>04</strong>.2006<br />
10<strong>01</strong>5654 AVIONICS MOBILE DESIGN SERVICES <strong>EASA</strong>.IM.A.S.<strong>01</strong>63<br />
REVISION 1<br />
10<strong>01</strong>5663 AVIONICS MOBILE DESIGN SERVICES <strong>EASA</strong>.IM.A.S.<strong>01</strong>64<br />
REVISION 1<br />
10036511 AVIONICS MOBILE DESIGN SERVICES<br />
(AM<br />
REV 1 HS 125-700 SERIES Installation of a Rockwell Collins TCAS-4000<br />
Traffic Alert and Collision Avoidance System<br />
(TCAS-II)<br />
REV 1 - HS 125-700 SERIES Installation of a Ground Proximity Warning<br />
System (GPWS) and Terrain Awareness<br />
Warning System (TAWS)<br />
10<strong>01</strong>5345 AVIONICS SUPPORT GROUP, INC. <strong>EASA</strong>.IM.A.S.0<strong>04</strong>46 FAA STC ST02900AT BOEING 747-200<br />
BOEING 747-300<br />
HAWKER 800XP Installation of a Flight Data Recorder (FDR)<br />
System.<br />
T2CAS provisions on Boeing 747-200 & -300<br />
Series Aircraft.<br />
<strong>04</strong>.09.2<strong>01</strong>2<br />
17.03.2005<br />
08.<strong>04</strong>.2005<br />
29.11.2005<br />
06.10.2005<br />
26.07.2005<br />
18.11.2005<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
09.06.2006<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
09.06.2006<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 />
16.09.2<strong>01</strong>1<br />
1. Subject to compliance with the provisions of<br />
Part 21 Subpart E, this STC and associated<br />
shall remain valid until surrendered, withdrawn<br />
or otherwise terminated.2. If transfer of this<br />
STC is requested under Part 21A.116, the<br />
STC will be reissued.3. This<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 100/<strong>462</strong><br />
21.12.20<strong>04</strong>
Change language