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>4911 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03155 AIRBUS A320-214 Airbus Corporate Jet Centre Modification<br />
CJ<strong>01</strong>03 –VIP Interior - Shining Star No. 2<br />
03.03.2008<br />
10<strong>01</strong>5025 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03332 AIRBUS A320-214 Airbus Corporate Jet Centre Modification Prior to installation of this modification the<br />
12.12.2008<br />
CJ<strong>01</strong>45 Issue 1 -VIP Interior - Shining Star No. installer must determine that the<br />
1<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>5053 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03374 AIRBUS A319-115 Airbus Corporate Jet Centre Modification 1. Prior to installation of this modification the<br />
22.06.2009<br />
CJ0222 Issue 1VIP Interior - Residence installer must determine that the<br />
interrelationship between this modificationand<br />
any other previously installed modification<br />
will introduce no adverse effect upon the<br />
airworthiness of the produc<br />
10<strong>01</strong>5198 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03589 AIRBUS A320-214 Airbus Corporate Jet Centre Modification<br />
CJ0356 Issue 1 –AFM Supplement - VIP<br />
Interior: Shining Star No. 2<br />
10<strong>01</strong>5210 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03625 DGAC STC 180-SF-0227 AIRBUS A320 SERIES Installation of a cabin VIP (Aeroservices) in<br />
accordance with the Service Bulletin SOG-WD-<br />
00-00-<strong>01</strong> (or later approved revision)<br />
10<strong>01</strong>5211 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03626 DGAC FRANCE 180-SF-<strong>01</strong>87 AIRBUS A320 SERIES Cabin Conversion of one A319 corporate jet<br />
(A319 CJ)<br />
10<strong>01</strong>5212 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03627 DGAC FRANCE STC 180-SF-0212 AIRBUS A320 SERIES Cabin Conversion of one A319 Corporate Jet<br />
(A319 CJ)<br />
10<strong>01</strong>5281 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03813 LBA STC NO.2830/0009 ISSUE 1 A300C4-203 - Ref. to former Luftfarhrt Bundesamt STC<br />
2830/0009 Issue 1- This <strong>EASA</strong> STC keeps the<br />
certificated design of the LBA STC<br />
2830/0009Issue 1, which consisted in the<br />
installation of structure and systemprovisions to<br />
change the loading system to an integrated si<br />
10<strong>01</strong>5282 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03814 LBA STC NO.TA<strong>04</strong>66 A300F4-605R - Ref. to former Luftfahrt Bundesamt STC<br />
TA<strong>04</strong>66- This <strong>EASA</strong> STC keeps the<br />
certificated design of the LBA STC<br />
TA<strong>04</strong>66,which consisted in theretrofit of the<br />
Lower Deck Cargo Compartment (LDCC) -<br />
Cargo LoadingSystem (CLS), andreflects the<br />
changes induced by the<br />
06.06.2008<br />
<strong>04</strong>.07.2008<br />
07.07.2008<br />
07.07.2008<br />
Limited to MSN 212 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 />
Limited to the aircraft model operated by<br />
Federal Express (FedEX)<br />
Prior to installation of this modification it 26.02.2<strong>01</strong>0<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other<br />
previouslyinstalledmodification and/ or<br />
repair will introduce no adverse effect<br />
upon theairworthiness of the product.<br />
10<strong>01</strong>5283 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03816 LBA STC NO. TA0217 AIRBUS A319-132 Equipment / Furnishing - Passenger<br />
Limited to MSN 913. Prior to installation of this modification it 12.05.2<strong>01</strong>0<br />
Compartment - VIP-Kit for A319Kharafi Group<br />
must be determined thatthe<br />
KuwaitRevision to Luftfahrt Bundesamt STC<br />
interrelationship between this modification<br />
TA0217 Issue 2.This <strong>EASA</strong> STC keeps the<br />
and any other previouslyinstalled<br />
certificated design of the LBA STC TA0217<br />
modification and/ or repair will introduce<br />
issue2, which consisted in the aircraft VIP cabin<br />
no adverse effectupon the airworthiness<br />
reco<br />
of the product.<br />
10<strong>01</strong>5284 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03817 LBA STC NO. TA0265 AIRBUS A319-133 Equipment / Furnishings - Passenger<br />
Compartment - Install cabinfurnishing for<br />
Daimler Chrysler AviationRevision to Luftfahrt<br />
Bundesamt STC TA0265This <strong>EASA</strong> STC<br />
keeps the certificated design of the LBA STC<br />
TA0231 whichconsisted in the aircraft cabin<br />
reconfig<br />
10<strong>01</strong>5285 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03818 LBA STC NO. TA0269 AIRBUS A319-133 Equipment / Furnishing - Passenger<br />
Compartment - Install baggagecontainer for<br />
Daimlerchrysler Aviation.Revision to Luftfahrt<br />
Bundesamt STC TA0269 Issue 2.This <strong>EASA</strong><br />
STC keeps the certificated design of the LBA<br />
STC TA0269 Issue2 which consisted in the<br />
instal<br />
10<strong>01</strong>5286 AIRBUS S.A.S. <strong>EASA</strong>.A.S.03819 LBA STC NO. TA0231 AIRBUS A320-232 Equipment/ Furnishings - Passenger<br />
Compartment - VIP-kit for A320 Syria.Revision<br />
to Luftfahrt Bundesamt STC TA0231.This<br />
<strong>EASA</strong> STC keeps the certificated design of the<br />
LBA STC TA0231 whichconsisted in the<br />
aircraft cabin VIP reconfiguration, and reflects<br />
thec<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 />
12.05.2<strong>01</strong>0<br />
Limited to MSN 1053 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 />
Limited to MSN 886, 918, 1032, and 1075 Private used only (non-commercial<br />
transportationPrior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repair will introduce no adverse eff<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 58/<strong>462</strong><br />
12.05.2<strong>01</strong>0
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