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>6512 GULFSTREAM AEROSPACE<br />
<strong>EASA</strong>.IM.A.S.02879 FAA STC ST02524CH-D GULFSTREAM GIV-X Aircraft completion and cabin interior<br />
1. GIV-X Serial No. 4119 Only;2. Prior to<br />
07.08.2008<br />
CORPORATION<br />
installation Serial No 4119.<br />
installation of this modification the installer must<br />
determine that the interrelationship between<br />
this modification and any other previously<br />
installed modification will introduce no adverse<br />
effect upon the ai<br />
10<strong>01</strong>6513 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6514 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6515 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6520 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6521 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6534 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6539 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6547 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6548 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6560 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6561 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
<strong>EASA</strong>.IM.A.S.02882 FAA STC ST02583CH-D GULFSTREAM GV-SP Aircraft Serial No 5197 completion and cabin<br />
interior installation.<br />
<strong>EASA</strong>.IM.A.S.02884 FAA STC ST03570AT GULFSTREAM 200 Installation of an Auxiliary Power Unit (APU)<br />
Surge Control Valve Modification.<br />
<strong>EASA</strong>.IM.A.S.02886 FAA STC ST02578CH-D GULFSTREAM GV-SP Aircraft Serial No 5189 completion and cabin<br />
interior installation.<br />
<strong>EASA</strong>.IM.A.S.02892 FAA STC ST03565AT-D GULFSTREAM GIV-X Installation of Custom Cabin Interior and<br />
Aircraft Completion for Aircraft Serial 4122.<br />
<strong>EASA</strong>.IM.A.S.02893 FAA STC ST03449AT-D GULFSTREAM GV-SP Installation of Custom Cabin Interior and<br />
Aircraft Completion for Aircraft Serial 5155.<br />
<strong>EASA</strong>.IM.A.S.02911 FAA STC ST03579AT-D GULFSTREAM GIV-X Installation of Custom Cabin Interior and<br />
Aircraft Completion for Aircraft Serial 4123.<br />
<strong>EASA</strong>.IM.A.S.02916 FAA STC ST02089LA-D GULFSTREAM GV-SP Installation of Cabin Interior Modification for<br />
Aircraft Serial 5155.<br />
<strong>EASA</strong>.IM.A.S.02926 FAA STC ST02091LA-D GULFSTREAM GV-SP Installation of Custom Cabin Interior and<br />
Aircraft Completion for Aircraft Serial 5193.<br />
<strong>EASA</strong>.IM.A.S.02927 FAA STC ST02093LA-D GULFSTREAM GV-SP Installation of Custom Cabin Interior and<br />
Aircraft Completion for Aircraft Serial 5198.<br />
<strong>EASA</strong>.IM.A.S.02945 FAA STC ST03587AT-D GULFSTREAM GIV-X Installation of an Airplane Interior for Aircraft<br />
Serial 4130.<br />
<strong>EASA</strong>.IM.A.S.02946 FAA STC ST03592AT-D GULFSTREAM GV-SP Installation of Custom Cabin Interior and<br />
Aircraft Completion for Aircraft Serial 52<strong>01</strong>.<br />
1. Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification<br />
andany other previously installed modification<br />
will introduce no adverse effect upon the<br />
airworthiness of the product. The insta<br />
1. GV-SP Serial No. 5189 Only2. Prior to<br />
installation of this modification the installer must<br />
determine that the interrelationship between<br />
this modification andany other previously<br />
installed modification will introduce no adverse<br />
effect upon the airworthin<br />
27.10.2008<br />
02.07.2008<br />
17.09.2008<br />
Aircraft Serial Number 4122 only.The following<br />
06.08.2008<br />
STC's are a required part of this<br />
STC:ST03027AT-DST02987AT-DST03<strong>04</strong>7AT-<br />
DST02980AT-DST03290AT-DST03532AT-<br />
DST03238AT-DST02979AT-DIt is the<br />
installer's responsability to ensure these STC's<br />
are all <strong>EASA</strong> approved.<br />
Aircraft Serial Number 5155 only:the following<br />
05.08.2008<br />
STC's are a required part of this<br />
STC:ST02796AT-DST02697AT-DST02715AT-<br />
DST03290AT-DST<strong>01</strong>775LA-DST02696AT-<br />
DST00892LA In addition, this STC must be<br />
installed in conjunction with Cabin Modification<br />
STC ST02089LA-D<br />
1. Aircraft Serial Number 4123 only:2. The<br />
07.08.2008<br />
following STCs are a required part of this STC:-<br />
ST03027AT-D- ST02987AT-D-<br />
ST03<strong>04</strong>7AT-D- ST02980AT-D-<br />
ST03290AT-D- ST03532AT-D-<br />
ST03238AT-D- ST02979AT-DIt is the<br />
installer’s responsibi<br />
Aircraft Serial Number 5155 only. <strong>04</strong>.08.2008<br />
Aircraft Serial Number 5193 only.Prior to<br />
installation of this modification the installer must<br />
determine that the interrelationship between<br />
this modification and any other previously<br />
installed modification will introduce no adverse<br />
effect upon the airworth<br />
1. Aircraft Serial Number 5198 only.2. Prior to<br />
installation of this modification the installer must<br />
determine that the interrelationship between<br />
this modification andany other previously<br />
installed modification will introduce no adverse<br />
effect upon the air<br />
Aircraft Serial Number 4130 only.The following<br />
STCs are a required part of this<br />
STC:ST03027AT-D ST02987AT-D<br />
ST03<strong>04</strong>7AT-D ST02980AT-D ST03290AT-D<br />
ST03532AT-D ST02979AT-D It is the installers<br />
responsibility to ensure these STCs are all<br />
<strong>EASA</strong> approved.Prior to<br />
Prior to installation of this modification the<br />
installer must determine that the<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 install<br />
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02.09.2008<br />
30.09.2008<br />
16.10.2008<br />
<strong>04</strong>.11.2008