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>5287 AIRBUS S.A.S. P-<strong>EASA</strong>.A.S.03820 LBA STC NO. TA0228 A330-223 (Ref. to former Luftfarhrt Bundesamt STC Limited to MSN 240, 249, 253, 255, 262, 275, Prior to installation of this modification it 31.08.2<strong>01</strong>0<br />
TA0228)This <strong>EASA</strong> STC keeps the certificated 288, 291, and 366<br />
must be determined thatthe<br />
design of the LBA STC TA0228<br />
interrelationship between this modification<br />
whichconsisted in the aircraft cabin<br />
and any other previouslyinstalled<br />
reconfiguration, and reflects thechanges<br />
modification and/ or repair will introduce<br />
induced by the transfer of LBA STC TA0228<br />
no adverse effectupon the airworthiness<br />
from DaimlerChryslerA<br />
of the product.<br />
10<strong>01</strong>5288 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03821 LBA STC TA0261 AIRBUS A310-3<strong>04</strong> GLARE demonstrator panel<br />
installationRevision to Luftfahrt Bundesamt<br />
STC TA0261.This <strong>EASA</strong> STC keeps the<br />
certificated design of the LBA STC TA0261,<br />
whichconsisted in the installation of the Glare<br />
demonstrator panel fortesting purpose, and<br />
reflects the chang<br />
10028319 AIRBUS S.A.S. P-<strong>EASA</strong>.A.S.03500 REV. 1 A319-115, MSN 3243 ACJ Centre Modification CJ0300 Issue 1 (VIP<br />
Cabin Interior - ALF) -ACJ Centre Modification<br />
CJ0392 Issue 1 (Private to Public Conversion)<br />
10028791 AIRBUS S.A.S. <strong>EASA</strong>.A.S.00351 REV. 2 A310-3<strong>04</strong> - <strong>EASA</strong> STC <strong>EASA</strong>.A.S.00351 revision 2(Ref.<br />
to former Luftfahrt Bundesamt STC TA<strong>01</strong>75<br />
Issue 3)- The STC <strong>EASA</strong>.A.S.00351 has<br />
covered the transfer of the STC TA <strong>01</strong>75issue<br />
3 (Original Aviation Authority reference) from<br />
the originalAviation Authority (LBA) to the<br />
10028999 AIRBUS S.A.S. P-<strong>EASA</strong>.A.S.03735 REV. 1 A319-115 ACJ Centre Modification CJ<strong>04</strong>00 Issue 1 (VIP<br />
Cabin Interior - ACROPOLIS)<br />
1003<strong>01</strong>47 AIRBUS S.A.S. P-<strong>EASA</strong>.A.S.03949 A320-200 Airbus Corporate Jet Centre Modification<br />
CJ0531 Issue 1 - VIP KIT - RAFOProject<br />
10031829 AIRBUS S.A.S. P-<strong>EASA</strong>.A.S.03426 REV. 1 A310-3<strong>04</strong> Replacement of Cockpit Communication Unit<br />
(CCU) and Radio Control Unit(RCU) by<br />
Centralized Radio Control (CRC).This STC will<br />
modify the communication system by changing<br />
equipments,mating connectors, and wiring.<br />
10031840 AIRBUS S.A.S. P-<strong>EASA</strong>.A.S.03950 A320-232 Airbus Corporate Jet Centre Modification<br />
CJ0540 Issue 1 -VIP Interior - "QATAR"<br />
10033449 AIRBUS S.A.S. A319-133 Airbus Corporate Jet Centre Modification<br />
CJ0615 Issue 1 - VIP Interior -"HNA"<br />
Limited to MSN 484. 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 />
12.05.2<strong>01</strong>0<br />
This STC is limited to Airbus A319 MSN 3243 Operations under EU-OPS possible by<br />
application of ConversionInstruction<br />
(Aircraft in Public Configuration) Ref: CI<br />
00CJ002 Issue B Prior to installation of<br />
this modification it must be determined<br />
thatthe interrelationship between this<br />
1- Transmissions (transmission operation) in<br />
tactical/close air supportband [frequency range<br />
30-89 MHz] are prohibited on the military<br />
radiosV/UHF Cockpit and V/UHF FOS during<br />
flight.2- Aircraft Flight Manual Supplement for<br />
Airbus A310-3<strong>04</strong>, TemporaryRevisi<br />
modification and any<br />
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 />
17.12.2009<br />
19.02.2<strong>01</strong>0<br />
This STC is limited to Airbus A319 MSN 3826 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 />
25.02.2<strong>01</strong>0<br />
This STC is limited to Airbus A320-200 MSN<br />
3723 & MSN 4117<br />
The current STC needs specific aircraft<br />
configuration as a prerequisite:To install this<br />
STC on A310-3<strong>04</strong> aircraft models,<br />
embodiment of <strong>EASA</strong> STCref: 10<strong>01</strong>3946, Rev<br />
1 - previously referenced as <strong>EASA</strong> STC<br />
<strong>EASA</strong>.A.S.0<strong>04</strong>03-(or any further <strong>EASA</strong><br />
approved revision) i<br />
The VIP KIT shall be installed in<br />
accordance with the<br />
"ConversionInstruction" documentref. CI<br />
00CJ003 at the latest revision approved<br />
under DOA No.<strong>EASA</strong>.21J.031Prior to<br />
installation of this modification it must be<br />
determined thatthe interrelationship<br />
betwee<br />
28.05.2<strong>01</strong>0<br />
Prior to installation of this modification it 09.12.2<strong>01</strong>0<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 />
This STC is limited to A320-232 MSN 4170 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 />
17.09.2<strong>01</strong>0<br />
This STC is limited to A319-133 MSN 4<strong>04</strong>2 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.<strong>01</strong>.2<strong>01</strong>1<br />
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