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>04</strong>2377 GULFSTREAM AEROSPACE<br />
FAA STC ST<strong>01</strong>957CH-D GV, GV-SP Installation of an Airshow RF/IF Remote None If the holder agrees to permit another 28.11.2<strong>01</strong>2<br />
CORPORATION<br />
Controller<br />
person to alter the product, theholder<br />
must give the other person written<br />
evidence of that permission.Prior to<br />
installation of this modification it must be<br />
determined thatthe interrelationship<br />
between this modificatio<br />
10<strong>04</strong>2407 GULFSTREAM AEROSPACE<br />
FAA STC ST02518CH-D GV-SP Installation of a 16 Passenger Corporate This STC approval is limited to the installation JAR 25 Modifications: To meet <strong>EASA</strong> 29.11.2<strong>01</strong>2<br />
CORPORATION<br />
Aircraft Interior<br />
in GV-SP Serial NumberSN 5171<br />
Type Certificate DataSheet requirements,<br />
the following design changes are<br />
required:.Ashtrays to be installed in the<br />
interior of the lavatories, in additionto the<br />
ashtrays on the entry side of lavatories.<br />
(JAR §25.853(e))-<br />
10<strong>04</strong>2618 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>04</strong>2689 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>01</strong>5351 GULFSTREAM AEROSPACE<br />
CORPORATION.<br />
10<strong>01</strong>5593 GULFSTREAM AEROSPACE<br />
CORPORATION.<br />
10<strong>01</strong>5595 GULFSTREAM AEROSPACE<br />
CORPORATION.<br />
10<strong>01</strong>5596 GULFSTREAM AEROSPACE<br />
CORPORATION.<br />
10<strong>01</strong>5597 GULFSTREAM AEROSPACE<br />
CORPORATION.<br />
10<strong>01</strong>5598 GULFSTREAM AEROSPACE<br />
CORPORATION.<br />
10<strong>01</strong>5965 GULFSTREAM AEROSPACE<br />
CORPORATION.<br />
10<strong>01</strong>5966 GULFSTREAM AEROSPACE<br />
CORPORATION.<br />
10<strong>01</strong>5994 GULFSTREAM AEROSPACE<br />
CORPORATION.<br />
FAA STC ST<strong>04</strong>280AT-D GV-SP Installation of an Executive Completion 1. The installer must determine whether this<br />
design change is compatiblewith previously<br />
approved modifications.2. If the holder agrees<br />
to permit another person to use this<br />
certificateto alter the product, the holder shall<br />
give the other person writtenevide<br />
FAA STC ST<strong>04</strong>249AT-D G350 AND G450 Installation of a Cabin Interior and Airplane<br />
Completion.<br />
<strong>EASA</strong>.IM.A.S.00567 REV. 1 FAA STC ST10<strong>01</strong>6SC-D GULFSTREAM 200 Installation of BE Single (light weight) Seats<br />
Arrangement.<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>506 FAA STC ST399CH BOMBARDIER CL-600-2B16 Installation of a Honeywell FMZ-2000 Flight<br />
Management System<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>508 FAA STC SA589GL BOMBARDIER CL-600-2B16 Installation of Passenger Oxygen System and<br />
Modification of Crew Oxygen System<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>509 FAA STC SA3716SW BOMBARDIER CL-600-2B16 Installation of a baggage compartment smoke<br />
detector system<br />
1. The installer must determine whether this<br />
design change is compatiblewith previously<br />
approved modifications.2. The instructions<br />
contained in the Guidance for Follow-On<br />
Installation, GC422<strong>04</strong>0227, Revision A,<br />
dated January 19, 2<strong>01</strong>2 or later FAA appr<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
1. Canadair Part Numbers 600-34<strong>01</strong>2-73,<br />
located at B.L.6 06, and 600-34<strong>01</strong>2-71,<br />
located at B.L.13, 73, must be replaced if any<br />
cracksare detected during the inspections<br />
required at intervals of 1000 take-off/landing<br />
cycles with this modification installed2.<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>510 FAA STC SA4372SW BOMBARDIER CL-600-2B16 Installation of an emergency lighting system This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>511 FAA STC SA8353SW BOMBARDIER CL-600-2B16 Installation of a Loral F-1000 Flight Data<br />
Recorder<br />
<strong>EASA</strong>.IM.A.S.02114 FAA STC ST09639SC GULFSTREAM 200 Installation of an Allied Signal DFDR i.a.w.<br />
MDL30-11000007<br />
<strong>EASA</strong>.IM.A.S.02115 FAA STC ST09945SC GULFSTREAM 200 Installation of Lead Acid Batteries i.a.w. MDL30-<br />
1100<strong>01</strong>4<br />
<strong>EASA</strong>.IM.A.S.02148 FAA STC ST03270AT-D GULFSTREAM 200 Installation of a proective shroud around the<br />
60Hz inverter<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
For subsequent installations of this STC, 11.12.2<strong>01</strong>2<br />
the instructions contained indocument<br />
GC522<strong>04</strong>3062, Rev. -, dated 12th<br />
November 2<strong>01</strong>2, "Guidance forFollow-On<br />
Installation, Executive Completion" must<br />
be followed.<br />
The approved <strong>EASA</strong> Configurations and 13.12.2<strong>01</strong>2<br />
the compatible <strong>EASA</strong> export optionare<br />
defined in GC422<strong>04</strong>0234, "<strong>EASA</strong><br />
Validated Configuration ListsST<strong>04</strong>249AT-<br />
D", Revision "-", dated December 03,<br />
2<strong>01</strong>2 or later approvedrevision.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 255/<strong>462</strong><br />
<strong>04</strong>.12.2008<br />
12.09.2005<br />
12.09.2005<br />
12.09.2005<br />
12.09.2005<br />
12.09.2005<br />
16.10.2006<br />
16.10.2006<br />
21.11.2006
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