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>5581 GULFSTREAM AEROSPACE Corp. <strong>EASA</strong>.IM.A.S.<strong>01</strong>492 FAA STC ST09629SC GULFSTREAM 200 Installation of an Artex ELT (110-406 NAV) 1. For aircraft imported into the European<br />
06.10.2005<br />
Emergency Locator Transmitter Sytem with Union, changes per Gulfstream Aerospace<br />
NAV interface<br />
drawing CEB442310<strong>01</strong>, Rev A are required to<br />
be incorporated until Revision L os the<br />
Engineering document 30-110005 has been<br />
released.2. This STC is approved only for the<br />
prod<br />
10<strong>01</strong>5582 GULFSTREAM AEROSPACE Corp. <strong>EASA</strong>.IM.A.S.<strong>01</strong>493 FAA STC ST09747SC GULFSTREAM 200 Installation of a N°2 Allied Signal KHF-950 HF This STC is approved only for the product<br />
06.10.2005<br />
Communication System<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 />
10<strong>01</strong>5583 GULFSTREAM AEROSPACE Corp. <strong>EASA</strong>.IM.A.S.<strong>01</strong>494 FAA STC ST09748SC GULFSTREAM 200 Installation of a second 77 cubic-foot oxygen This STC is approved only for the product<br />
06.10.2005<br />
bottle in nose radome area, above existing configuration as defined in the approved design<br />
bottle<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
10<strong>01</strong>5584 GULFSTREAM AEROSPACE Corp. <strong>EASA</strong>.IM.A.S.<strong>01</strong>495 FAA STC ST09851SC GULFSTREAM 200 Installation of interior shell, forward cabinets, This STC is approved only for the product<br />
06.10.2005<br />
10<strong>01</strong>5585 GULFSTREAM AEROSPACE Corp. <strong>EASA</strong>.IM.A.S.<strong>01</strong>496 FAA STC ST09953SC GULFSTREAM 200<br />
card tables, lavatory partitions and door, curtain 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 />
Installation of B/E Aerospace, Aircraft Modular This STC is approved only for the product<br />
06.10.2005<br />
Products Forward/Rearward Facing Single configuration as defined in the approved design<br />
Seat, model 2524.546.<strong>01</strong> ( )<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
10<strong>01</strong>5586 GULFSTREAM AEROSPACE Corp. <strong>EASA</strong>.IM.A.S.<strong>01</strong>497 FAA STC ST09954SC GULFSTREAM 200 Installation of an Oxygen Filler Panel with This STC is approved only for the product<br />
06.10.2005<br />
Pressure Gauge<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 />
10<strong>01</strong>5749 GULFSTREAM AEROSPACE Corp. <strong>EASA</strong>.IM.A.S.<strong>01</strong>782 REV 2 FAA STC ST103<strong>01</strong>SC-D GULFSTREAM 200 Installation of Executive Cabin Interior in Compatibility of this design change with<br />
03.03.2008<br />
accordance with Index List GA222<strong>04</strong>80<strong>01</strong>, Rev previously approved modifications must be<br />
A, dated 3-23-2005 or later revisions of the<br />
above listed documents approved by <strong>EASA</strong> in<br />
accordance with <strong>EASA</strong> ED Decision<br />
20<strong>04</strong>/<strong>04</strong>/CF (or subsequent revisions of this<br />
dec<br />
determined by the installer.<br />
10<strong>01</strong>5750 GULFSTREAM AEROSPACE Corp. <strong>EASA</strong>.IM.A.S.<strong>01</strong>783 FAA STC ST103<strong>04</strong>SC-D GULFSTREAM 200 Installation of Forward R/H Galley Compatibility of this design change with<br />
previously approved modifications must be<br />
determined by the installer.<br />
14.03.2006<br />
10<strong>01</strong>5751 GULFSTREAM AEROSPACE Corp. <strong>EASA</strong>.IM.A.S.<strong>01</strong>784 FAA STC ST02847AT-D GULFSTREAM 200 Installation of Safe Flight Instrument Corp Auto Compatibility of this design change with<br />
14.03.2006<br />
Power Automatic Throttle Control System previously approved modifications must be<br />
determined by the installer<br />
10<strong>01</strong>5382 GULFSTREAM AEROSPACE<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>069 FAA STC ST<strong>01</strong>220LA-D GULFSTREAM GV S/N 641 Aircraft Serial No. 641 completion and cabin 1. GV Serial No. 641 only 17.07.2007<br />
CORPORATION<br />
interior installation.<br />
10<strong>01</strong>5388 GULFSTREAM AEROSPACE<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>085 FAA STC ST<strong>01</strong>671LA-D GULFSTREAM GV-SP Cabin Interior Installation 1. This STC is approved only for the product<br />
25.<strong>01</strong>.2005<br />
CORPORATION<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 />
10<strong>01</strong>5389 GULFSTREAM AEROSPACE<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>086 FAA STC ST<strong>01</strong>376LA-D GULFSTREAM GV-SP Installation of Aerospace Technologies Group 1. This STC is approved only for the product<br />
25.<strong>01</strong>.2005<br />
CORPORATION<br />
(ATG) Cabin Window<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 />
10<strong>01</strong>5390 GULFSTREAM AEROSPACE<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>087 FAA STC ST<strong>01</strong>373LA-D GULFSTREAM GV-SP Installation of Securaplane External Camera 1. This STC is approved only for the product<br />
25.<strong>01</strong>.2005<br />
CORPORATION<br />
System<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 />
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