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 />
10032075 GULFSTREAM AEROSPACE<br />
REV. 1 FAA STC NO. ST03793AT-D GULFSTREAM GV-SP Installation of an Airplane Interior for aircraft This approval is limited to only the installation Prior to installation of this modification it 06.10.2<strong>01</strong>0<br />
CORPORATION<br />
S/N 5277<br />
made in Gulfstream,GV-SP, A/C 5277The must be determined thatthe<br />
following STC’s are a required part of this interrelationship between this modification<br />
STC:ST02696AT-D, ST02697AT-D,<br />
and any other previouslyinstalled<br />
ST03533AT-D, ST02796AT-D, ST02715AT-D, modification and/ or repair will introduce<br />
andST03290AT-DIt is the installers<br />
no adverse effectupon the airworthiness<br />
responsibility to en<br />
of the product.<br />
10032076 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10032077 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10032086 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10032609 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10032631 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10032651 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10032980 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10033988 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
REV. 1 FAA STC ST02292CH-D GV-SP Installation of the 115V AC/60Hz Outlets<br />
Multiple STC for GulfstreamGV-SP model<br />
aircraft.<br />
REV. 1 FAA STC ST03794AT-D GV-SP Installation of the Aircraft Cabin Compartment<br />
for Gulfstream GV-SPmodel aircraft.<br />
REV. 1 FAA STC ST03759AT-D GV-SP Installation of the Audio Video Distribution<br />
System (AVDS) Multiple STCfor Gulfstream<br />
GV-SP model aircraft.<br />
FAA STC ST<strong>04</strong>209AT-D GIV-X Aircraft Completion and Installation of an<br />
Airplane Interior<br />
FAA STC ST<strong>04</strong>213AT-D GIV-X Aircraft Completion and Installation of Airplane<br />
Interior.<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 />
23.02.2<strong>01</strong>2<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 />
23.02.2<strong>01</strong>2<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 />
23.02.2<strong>01</strong>2<br />
You may not use descriptive data about this The following STCs are a required part of<br />
design change to duplicateto other<br />
this STC: ST02979AT-D,ST02980AT-D,<br />
products.This approval is limited to aircraft ST02987AT-D, ST03027AT-D,<br />
Serial 4200.This STC does not permit ST03<strong>04</strong>7AT-D, ST03290ATmanufacturing<br />
of parts for multipleinstallations. D,ST03410AT-D, ST03532AT-D,<br />
ST03742AT-D and ST03647AT-D.Prior<br />
to installation of this modification it must<br />
be determined thatthe i<br />
You cannot use descriptive data about this<br />
design change to duplicate toother<br />
,,products.This approval is limited to<br />
Gulfstream GIV-X, Serial 4202.This STC does<br />
not permit manufacturing of parts for<br />
multipleinstallations.<br />
The following STC's are a required part<br />
of this STC: ST02979AT-D,<br />
,,ST02980AT-D, ST02987AT-D,<br />
ST03027AT-D, ST03<strong>04</strong>7AT-D,<br />
ST03290AT-D, ST03410AT-D,<br />
ST03532AT-D, ST03646AT-D,<br />
ST03647AT-D, andST03737AT-D.It is<br />
the installers responsibility to ensure the<br />
FAA STC ST03742AT-D GIV-X Installation of a Cabin/Baggage Compartment. None<br />
above<br />
Follow-On Installation Guide<br />
GC422<strong>04</strong>0214, Revision A, dated<br />
November <strong>01</strong>,2<strong>01</strong>0, or later FAA<br />
approved revision is to be used for<br />
subsequentinstallations. Prior to<br />
installation of this modification it must be<br />
determined thatthe interrelationship<br />
between this<br />
19.11.2<strong>01</strong>0<br />
FAA STC ST<strong>04</strong>215AT-D GIV-X Aircraft Completion and Installation of an You cannot use descriptive data about this The following STCs are a required part of 13.12.2<strong>01</strong>0<br />
Airplane Interior on AircraftSerial 4203. design change to duplicateother products. This this STC: ST03542AT-D,ST02<strong>04</strong>9CH-D,<br />
approval is limited to only the installation ST02979AT-D, ST02980AT-D,<br />
madein Gulfstream GIV-X, A/C 4203. This ST02987AT-D, ST03027AT-<br />
STC does not permit manufacturing ofparts for D,ST03<strong>04</strong>7AT-D, ST03290AT-D,<br />
multiple installations.<br />
ST03410AT-D, ST03532AT-D,<br />
ST03648AT-D andST03649AT-D.It is the<br />
installers responsibility to ensure the<br />
FAA STC ST<strong>04</strong>225AT-D GV-SP Aircraft Serial No 5302 completion and cabin<br />
interior installation<br />
17.11.2<strong>01</strong>0<br />
18.11.2<strong>01</strong>0<br />
GV-SP Serial No. 5302 Only 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 />
24.02.2<strong>01</strong>1<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 252/<strong>462</strong>
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