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>3957 AIRBUS S.A.S. <strong>EASA</strong>.A.S.00514 REV. 3 A310-3<strong>04</strong> - <strong>EASA</strong> STC <strong>EASA</strong>.A.S.00514 revision 3- The N/A - The STC <strong>EASA</strong>.A.S.0<strong>04</strong>03 is a pre- 19.02.2<strong>01</strong>0<br />
STC <strong>EASA</strong>.A.S.00514 allowed the installation<br />
requisite for the embodiment of theSTC<br />
of the Air to AirRefuelling kit provision, on the<br />
<strong>EASA</strong>.A.S.00514 (original and<br />
A310-3<strong>04</strong> aircraft model converted in aMulti<br />
subsequent issues) - Prior to installation<br />
Role Transport version, called ‘Polaris’<br />
of this modification it must be determined<br />
configuration.- Revision 1 introduc<br />
thatthe interrelationship between this<br />
modification and any other pr<br />
10<strong>01</strong>3960 AIRBUS S.A.S. <strong>EASA</strong>.A.S.00634 REV. 6 A310-203/-221/-222<br />
A310-3<strong>04</strong>/-308/-324/-325<br />
<strong>EASA</strong> STC 10<strong>01</strong>3960 Revision 6 (A310-200<br />
series and -300 seriesaeroplanes, Passenger<br />
to Freighter conversion)(Ref. to former<br />
Luftfahrt Bundesamt STC TA0383 Issue 9)-<br />
The STC <strong>EASA</strong>.A.S.00634 has covered the<br />
transfer of the STC TA0383Issue 9 (original<br />
Aviation<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 />
27.06.2<strong>01</strong>2<br />
10<strong>01</strong>3966 AIRBUS S.A.S. <strong>EASA</strong>.A.S.00685 REV. 1 AIRBUS A321-231 VIP cabin modification in accordance with<br />
Modification Approval Sheet (MAS) ref. SOG-<br />
792 issue 1, dated March 31st, 2005<br />
This STC is limited to A321-231 MSN 1202 <strong>04</strong>.06.2008<br />
10<strong>01</strong>3972 AIRBUS S.A.S. <strong>EASA</strong>.A.S.00767 REV. 1 AIRBUS A320-214 LIVE TV Installation This STC is limited to A320-213 MSN 2165 <strong>04</strong>.07.2008<br />
10<strong>01</strong>3973 AIRBUS S.A.S. <strong>EASA</strong>.A.S.00769 REV. 1 AIRBUS A320-214 Avionic Rack 9100 VU Installation This STC is limited to A320-214 MSN 2165 <strong>04</strong>.07.2008<br />
10<strong>01</strong>3974 AIRBUS S.A.S. <strong>EASA</strong>.A.S.00772 REV. 1 AIRBUS A320-214 NAS VIP Cabin Modification This STC is limited to A320-214 MSN 2165 <strong>04</strong>.07.2008<br />
10<strong>01</strong>4023 AIRBUS S.A.S. <strong>EASA</strong>.A.S.<strong>01</strong>078 REV. 1 AIRBUS A319-133 AL SALAM Master Modification This STC is limited to A319-133 CJ MSN 2421 02.07.2008<br />
10<strong>01</strong>4127 AIRBUS S.A.S. <strong>EASA</strong>.A.S.<strong>01</strong>237 REV. 1 AIRBUS A321-231 Satcom in accordance with Morification<br />
Approval Sheet (MAS) ref. : SOG-00-794 issue<br />
3, dated March 18, 2005.<br />
This STC is limited to A321-231 MSN 1202 <strong>04</strong>.07.2008<br />
10<strong>01</strong>4140 AIRBUS S.A.S. <strong>EASA</strong>.A.S.<strong>01</strong>253 REV. 1 AIRBUS A340-541 DA WLAT Qatar Airways Modifications in The applicability of this STC is limited to MSN<br />
<strong>04</strong>.07.2008<br />
accordance with Modification Approval Sheet 495No more than 10 Laptops equipped with<br />
Ref. SOG-<strong>01</strong>-0648<br />
WiFi system are allowed in the cabin<br />
10<strong>01</strong>4164 AIRBUS S.A.S. <strong>EASA</strong>.A.S.<strong>01</strong>296 REV. 1 AIRBUS A340-541 DA WLAT Qatar Airways Live TV Modifications The applicability of this STC is limited to MSN<br />
in accordance with Modification Approval Sheet 495<br />
Ref. SOG-23-690<br />
10<strong>01</strong>4197 AIRBUS S.A.S. <strong>EASA</strong>.A.S.<strong>01</strong>340 REV. 1 AIRBUS A330-200 Installation of a more powerful air heater (3kg<br />
W) inside the private cabin washroom<br />
10<strong>01</strong>4231 AIRBUS S.A.S. <strong>EASA</strong>.A.S.<strong>01</strong>394 REV. 1 AIRBUS A340-212 VIP Cabin and systems upgrade in accordance<br />
with Sogerma Modification Approval Sheet<br />
(MAS) SOG-00-0977 issue 3 dated 03/02/06<br />
1.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.2. The limitations and<br />
The approval of this modification is limited to<br />
the Airbus A340-212 MSN 061<br />
10<strong>01</strong>4233 AIRBUS S.A.S. <strong>EASA</strong>.A.S.<strong>01</strong>396 REV. 1 AIRBUS A319-133 Avionics Rack 9100 VU installation 1. This STC is limited to A319-133 CJ MSN<br />
2421<br />
<strong>04</strong>.07.2008<br />
10<strong>01</strong>4234 AIRBUS S.A.S. <strong>EASA</strong>.A.S.<strong>01</strong>397 REV. 1 AIRBUS A319-133 Live TV system provision This STC is limited to A319-133 CJ MSN 2421 <strong>04</strong>.07.2008<br />
10<strong>01</strong>4408 AIRBUS S.A.S. <strong>EASA</strong>.A.S.<strong>01</strong>703 AIRBUS A300-600ST MODEL F4-<br />
608<br />
Installation of ISIS on A300-600STInstallation<br />
of two Integrated Stand-by Instrument System<br />
(ISIS) in replacement of the stand by speed,<br />
attitude and altitude.<br />
10<strong>01</strong>4419 AIRBUS S.A.S. <strong>EASA</strong>.A.S.<strong>01</strong>740 REV. 1 AIRBUS A320 SAT TV Tailwind 550 antenna installation in<br />
accordance with MAS SOG-53-1252 issue 2<br />
dated 27/07/06<br />
10<strong>01</strong>4686 AIRBUS S.A.S. <strong>EASA</strong>.A.S.02849 REV. 1 AIRBUS A319 Modification MOD SOG-53-1296 " A319-SAT<br />
TV Tailwind 550 Antenna Installation"<br />
10<strong>01</strong>4779 AIRBUS S.A.S. <strong>EASA</strong>.A.S.02977 REV. 1 LBA STC TA0<strong>01</strong>5 ISSUE 4 A300B2-1A/ -1C/ K-3C/ -203 - <strong>EASA</strong> STC <strong>EASA</strong>.A.S.02977 revision 1-<br />
A300B4-2C/ -103/ -203<br />
(Ref. to former Luftfahrt Bundesamt STC<br />
TA0<strong>01</strong>5 Issue 4)- The STC <strong>EASA</strong>.A.S.02977<br />
has covered the transfer of the STC<br />
TA0<strong>01</strong>5Issue 4 (original Aviation Authority<br />
reference) from the originalAviation Authority<br />
(LBA) to the<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in paragraph ‘Description’.<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
1. The installation is compatible with the<br />
installation of a VH3 antenna between Fr 51<br />
and Fr 52, and a Canadian Marconi Aero-H+<br />
antenna betweeen Fr 58 and Fr 61 (separately<br />
or simultaneously).2. The installation requires<br />
both ACT 1 and 2 be installed on A<br />
<strong>04</strong>.07.2008<br />
<strong>04</strong>.07.2008<br />
<strong>04</strong>.07.2008<br />
26.10.2006<br />
30.06.2008<br />
30.06.2008<br />
N/A 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 />
26.02.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 57/<strong>462</strong>
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