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>0608 GULFSTREAM AEROSPACE<br />
FAA STC ST03779AT-D GIV-X Installation of an AirCell High Speed Internet <strong>EASA</strong> STC number <strong>EASA</strong>.IM.A.S.02633 is Prior to installation of this modification it 13.07.2<strong>01</strong>2<br />
CORPORATION<br />
System<br />
required for installation of thisSTC<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 />
10<strong>04</strong>0627 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>04</strong>1062 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>04</strong>1063 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>04</strong>11<strong>01</strong> GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>04</strong>1234 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>04</strong>1649 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>04</strong>1900 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
10<strong>04</strong>2374 GULFSTREAM AEROSPACE<br />
CORPORATION<br />
FAA STC ST00803LA-D GV Installation of Satcom Antenna (Racal). 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. If the<br />
16.07.2<strong>01</strong>2<br />
FAA STC ST03771AT-D GV-SP Installation of an Airplane Interior Limitations are defined in document<br />
Prior to installation of this modification it 20.08.2<strong>01</strong>2<br />
GC522<strong>04</strong>0593, "Follow-On InstallationGuide", must be determined thatthe<br />
Revision NC, dated May 5, 2<strong>01</strong><strong>01</strong>. The installer interrelationship between this modification<br />
must determine whether this design change is and any other previouslyinstalled<br />
compatiblewith previously approved<br />
modification and/ or repair will introduce<br />
modifications.2. If the holder agrees to permit a no adverse effectupon the airworthiness<br />
of the product.<br />
FAA STC ST02884AT-D GV Installation of a Transponder Flight<br />
Identification<br />
FAA STC ST<strong>04</strong>263AT-D GV-SP Executive Completion, Multiple STC. Limitations are defined in document<br />
GC522<strong>04</strong>3055, "Follow-On InstallationGuide",<br />
Revision NC, dated August 7, 2<strong>01</strong>2 1.,,The<br />
installer must determine whether this design<br />
change iscompatible with previously approved<br />
modifications.2.,,If the holder agrees to pe<br />
FAA STC ST<strong>01</strong>105LA-D GV Installation of a 13 Passenger Cabin Interior The approval of this modification applied only<br />
to Model GV S/N 622<br />
FAA STC ST<strong>01</strong>822AT-D GV AND GV-SP Installation of APU Fire Bottle 1- The installer must determine whether this<br />
design change is compatiblewith previously<br />
approved modifications2- If the holder agrees<br />
to permit another person to alter the<br />
product,the holder must give the other person<br />
written evidence of thatpermission.<br />
REV. 1 FAA STC ST00673LA-D GV Installation of Honeywell TCAS 2000 TCAS II<br />
System<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.If the<br />
20.08.2<strong>01</strong>2<br />
Prior to installation of this modification it 21.08.2<strong>01</strong>2<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 />
Prior to installation of this modification it 31.08.2<strong>01</strong>2<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.If the<br />
Prior to installation of this modification it <strong>04</strong>.10.2<strong>01</strong>2<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 />
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.If the<br />
23.10.2<strong>01</strong>2<br />
FAA STC ST<strong>01</strong>751LA-D GV-SP Installation of EROS Convertible MLD20 Series None Prior to installation of this modification it 28.11.2<strong>01</strong>2<br />
Crew Oxygen Mask -Regulator with<br />
must be determined thatthe<br />
Detachable Smoke Goggles<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.If the<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 254/<strong>462</strong>
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