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>6568 GULFSTREAM AEROSPACE<br />
<strong>EASA</strong>.IM.A.S.02959 FAA STC ST03007AT-D GV Installation of Honeywell Integrate Avionics Prior to installation of this modification the<br />
02.10.2008<br />
CORPORATION<br />
Computers (IAC) with Software Version NZ installer must determine that the<br />
6.0.<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>6569 GULFSTREAM AEROSPACE<br />
<strong>EASA</strong>.IM.A.S.02960 FAA STC ST03074AT-D GV Installation of Honeywell NZ-2000 Third FMS Prior to installation of this modification the<br />
02.10.2008<br />
CORPORATION<br />
Computer with Software Version NZ 6.0. installer must determine that the<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>6596 GULFSTREAM AEROSPACE<br />
<strong>EASA</strong>.IM.A.S.03007 FAA STC ST03610AT-D GULFSTREAM G550<br />
Installation of Custom Cabin Interior and Prior to installation of this modification the<br />
24.11.2008<br />
CORPORATION<br />
GULFSTREAM GV-SP<br />
Aircraft Completion for Aircraft Serial 52<strong>04</strong>. 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 />
10<strong>01</strong>6597 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6602 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6607 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6608 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6613 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6621 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6639 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>6650 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
<strong>EASA</strong>.IM.A.S.03009 FAA STC ST03511AT-D GULFSTREAM G150 Installation of Concorde Valve Regulated Lead None.<br />
Acid Main Batteries.<br />
18.02.2009<br />
<strong>EASA</strong>.IM.A.S.03<strong>01</strong>6 FAA STC ST02097LA-D GULFSTREAM G550 Installation of Custom Cabin Interior and 1. Aircraft Serial Number 5203 only.2. Prior<br />
02.12.2008<br />
Aircraft Completion for Aircraft Serial 5203. to installation of this modification the installer<br />
must determine that the interrelationship<br />
between this modification and any other<br />
previously installed modification will introduce<br />
no adverse effect upon<br />
<strong>EASA</strong>.IM.A.S.03024 FAA STC ST03617AT-D GULFSTREAM GIV-X Installation of Export Modifications for Aircraft<br />
Serial 4091.<br />
<strong>EASA</strong>.IM.A.S.03025 FAA STC ST03477AT-D GULFSTREAM GIV-X Airplane Completion and Custom Cabin<br />
Installation for Aircraft Serial 4091.<br />
<strong>EASA</strong>.IM.A.S.03038 FAA STC ST03643AT-D GULFSTREAM GV-SP Aircraft completion and Installation of Airplane<br />
Interior for Aircraft Serial 5210.<br />
<strong>EASA</strong>.IM.A.S.03052 FAA STC ST02632CH-D GULFSTREAM GV-SP Aircraft completion and cabin interior<br />
installation for Serial No 5212.<br />
<strong>EASA</strong>.IM.A.S.03079 FAA FAA STC ST6870CH-T GULFSTREAM GV-SP Aircraft Serial No 5220 completion and cabin<br />
interior installation.<br />
<strong>EASA</strong>.IM.A.S.03095 FAA STC ST03542AT-D GULFSTREAM GIV-X Installation of an Aft Galley/Galley Annex<br />
Multiple STC.<br />
1. Aircraft Serial Number 4091 only.2. This<br />
STC must be installed in conjunction with<br />
Airplane Completion STC ST03477AT-D<br />
(<strong>EASA</strong>.IM.A.S.03025) to fully meet <strong>EASA</strong><br />
requirements. 3. It is the installers’<br />
responsibility to ensure these STC’s are all<br />
<strong>EASA</strong> approv<br />
Aircraft Serial Number 4091 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 />
ST02979AT-D ST00892LA Additionally, this<br />
STC must be installed in conjunction with<br />
Export Modification STC ST036<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 />
1. Serial No. 5212 Only2. Prior to installation of<br />
this modification the installer must determine<br />
that the interrelationship between this<br />
modification andany other previously installed<br />
modification will introduce no adverse effect<br />
upon the airworthiness of<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 />
1. This Aft Galley/Galley Annex Multiple STC,<br />
(FAA ref ST03542AT-D), does not approve the<br />
entire airplane interior installation andhas the<br />
following limitations as defined in document<br />
GC415400266.“Guidance for Follow on<br />
Installation, Aft Galley/Galley Anne<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 249/<strong>462</strong><br />
15.10.2008<br />
15.10.2008<br />
08.<strong>01</strong>.2009<br />
02.03.2009<br />
08.<strong>04</strong>.2009<br />
10.06.2009
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