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>6586 DASSAULT FALCON JET <strong>EASA</strong>.IM.A.S.02991 FAA STC ST09313SC-D FALCON 900EX <strong>EASA</strong> Validation of FAA STC ST09313SC-D 1. Prior to installation of this modification the<br />
02.<strong>04</strong>.2009<br />
Revision 1, <strong>01</strong>st October 2002Installation of installer must determine that the<br />
Standby Horizon System Modifications in interrelationship between this modification and<br />
accordance with Drawing List Report No. F9EX-any<br />
other previously installed modification will<br />
<strong>01</strong>035 Revision B dated 25 September 2002 or introduce no adverse effect upon the<br />
later revisions approved by <strong>EASA</strong> i.a.w. EAS airworthiness of the product.2.<br />
10<strong>01</strong>6587 DASSAULT FALCON JET <strong>EASA</strong>.IM.A.S.02992 FAA STC ST09311SC-D FALCON 900EX <strong>EASA</strong> Validation of FAA STC ST09311SC-<br />
DInstallation of the Inertial Reference System<br />
Modification in accordance with Drawing List<br />
Report No. F9EX-<strong>01</strong>033 Revision NC dated<br />
<strong>04</strong>th May 2000 or later revisions approved by<br />
<strong>EASA</strong> i.a.w. <strong>EASA</strong> ED Decisions 2007/0<strong>01</strong>/C<br />
1. 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.2.<br />
10<strong>01</strong>6588 DASSAULT FALCON JET <strong>EASA</strong>.IM.A.S.02994 FAA STC SA8291SW-D FALCON 900EX<br />
a<br />
<strong>EASA</strong> Validation of FAA STC SA8291SW- 1. The F9EX-<strong>01</strong>003-503 and F9EX-<strong>01</strong>003-507<br />
DInstallation of the Battery Installations i.a.w. installations are limited to aircraft serial number<br />
Drawing List Report No. F9EX-<strong>01</strong>0003 <strong>04</strong>9.2. Prior to installation of this modification<br />
Revision F dated 14 September 2000 or later the installer must determine that the<br />
revisions approved by <strong>EASA</strong> i.a.w. <strong>EASA</strong> ED interrelationship between this modificationand<br />
Decisions 2007/0<strong>01</strong>/C and 20<strong>04</strong>/<strong>04</strong>/CF (or<br />
subseque<br />
any other previously ins<br />
10<strong>01</strong>6640 DASSAULT FALCON JET <strong>EASA</strong>.IM.A.S.03080 FAA STC ST09293SC-D FALCON 900EX <strong>EASA</strong> Validation of FAA STC ST09293SC-D 1. Prior to installation of this modification the<br />
Revision 10, 22nd December 20<strong>04</strong>Installation installer must determine that the<br />
of the FMZ-2000 Flight Management System in interrelationship between this modification<br />
accordance with Data List Report No. F9EX- andany other previously installed modification<br />
<strong>01</strong>026 Revision G dated 20 December 20<strong>04</strong> or will introduce no adverse effect upon the<br />
later revisions approved by <strong>EASA</strong> i.a.w. <strong>EASA</strong> airworthiness of the product.2. The ins<br />
10<strong>01</strong>6643 DASSAULT FALCON JET <strong>EASA</strong>.IM.A.S.03084 FAA STC ST09715SC-D FALCON 900EX - <strong>EASA</strong> Validation of FAA STC ST09715SC-<br />
D- Installation of the Control Wheel<br />
Modifications in accordance with Drawing List<br />
Report No. F9EX-<strong>01</strong>032<br />
10035<strong>01</strong>7 DASSAULT FALCON JET FAA STC ST10657SC-D 1. FALCON 2000EX<br />
2. FALCON 900EX<br />
10028268 DASSAULT FALCON JET - WILMINGTON P-<br />
<strong>EASA</strong>.IM.A.S.03109<br />
Assist Handle Installation:Configuration -5<strong>01</strong>:<br />
Main entry door assist handle<br />
installationConfiguration -503: Aft lavatory<br />
assist handle installationValidation of FAA STC<br />
N°ST10657SC-D<br />
1. Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification<br />
andany other previously installed modification<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.2. The ins<br />
20.03.2009<br />
18.03.2009<br />
07.<strong>04</strong>.2009<br />
11.05.2009<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 />
19.05.2<strong>01</strong>1<br />
FAA STC ST<strong>01</strong>795NY-D F900EX <strong>EASA</strong> Validation of FAA STC ST<strong>01</strong>795NY- This design change is applicable to Dassault Prior to installation of this modification it 14.12.2009<br />
DInstallation of Decrane Aircraft Seating Aviation Mystere Falcon 900aircraft which have must be determined thatthe<br />
Company, Inc, Model 80A42S2three place previously been equipped with Dassault interrelationship between this modification<br />
partial berthing divan installation in accordance AviationModification M3000 (Falcon 900EX and any other previouslyinstalled<br />
withDassault Falcon Jet-Wilmington Master definition)<br />
modification and/ or repair will introduce<br />
Drawing List, 1979009<strong>04</strong> RevisionB, dated<br />
no adverse effectupon the airworthiness<br />
29th<br />
of the product.<br />
10<strong>01</strong>5465 DASSAULT FALCON JET - WILMINGTON <strong>EASA</strong>.IM.A.S.<strong>01</strong>217 FAA STC ST<strong>01</strong>156NY-D MYSTERE FALCON 900 Validation of FAA STC ST<strong>01</strong>156NY-D:<br />
CO<br />
Installation of a Honeywell Mark V Enhanced<br />
Ground Proximity Warning System (EGPWS)<br />
upgrade iaw Master Drawing List 027670321,<br />
Rev. - dtd Jan 26, 20<strong>01</strong>.<br />
10<strong>01</strong>5466 DASSAULT FALCON JET - WILMINGTON <strong>EASA</strong>.IM.A.S.<strong>01</strong>218 FAA STC ST<strong>01</strong>157NY-D MYSTERE FALCON 900 Validation of FAA STC No ST<strong>01</strong>157NY-D:<br />
CO<br />
Installation of a Honeywell Electronic Flight<br />
Instrument System (EFIS) EDZ-820 Software<br />
Upgrade iaw Master Drawing List 027670320,<br />
Rev. - dtd. Jan. 26, 20<strong>01</strong>.<br />
10<strong>01</strong>5467 DASSAULT FALCON JET - WILMINGTON <strong>EASA</strong>.IM.A.S.<strong>01</strong>219 FAA STC ST<strong>01</strong>775NY-D MYSTERE FALCON 900 Validation of FAA STC No ST<strong>01</strong>775-NY-D:<br />
CO<br />
Update of Dual Rockwell Collins TCR-94<br />
Transponder for Elementary Surveillance iaw<br />
Master Drawing List 126980303, Rev.- dtd.<br />
Oct. 15, 20<strong>04</strong>.<br />
1. 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. 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. 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>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 170/<strong>462</strong><br />
31.05.2005<br />
31.05.2005<br />
31.05.2005
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