04/01/2013 Page 1/462 - EASA

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EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016586 DASSAULT FALCON JET EASA.IM.A.S.02991 FAA STC ST09313SC-D FALCON 900EX EASA Validation of FAA STC ST09313SC-D 1. Prior to installation of this modification the 02.04.2009 Revision 1, 01st October 2002Installation of installer must determine that the Standby Horizon System Modifications in interrelationship between this modification and accordance with Drawing List Report No. F9EX-any other previously installed modification will 01035 Revision B dated 25 September 2002 or introduce no adverse effect upon the later revisions approved by EASA i.a.w. EAS airworthiness of the product.2. 10016587 DASSAULT FALCON JET EASA.IM.A.S.02992 FAA STC ST09311SC-D FALCON 900EX EASA Validation of FAA STC ST09311SC- DInstallation of the Inertial Reference System Modification in accordance with Drawing List Report No. F9EX-01033 Revision NC dated 04th May 2000 or later revisions approved by EASA i.a.w. EASA ED Decisions 2007/001/C 1. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2. 10016588 DASSAULT FALCON JET EASA.IM.A.S.02994 FAA STC SA8291SW-D FALCON 900EX a EASA Validation of FAA STC SA8291SW- 1. The F9EX-01003-503 and F9EX-01003-507 DInstallation of the Battery Installations i.a.w. installations are limited to aircraft serial number Drawing List Report No. F9EX-010003 049.2. Prior to installation of this modification Revision F dated 14 September 2000 or later the installer must determine that the revisions approved by EASA i.a.w. EASA ED interrelationship between this modificationand Decisions 2007/001/C and 2004/04/CF (or subseque any other previously ins 10016640 DASSAULT FALCON JET EASA.IM.A.S.03080 FAA STC ST09293SC-D FALCON 900EX EASA Validation of FAA STC ST09293SC-D 1. Prior to installation of this modification the Revision 10, 22nd December 2004Installation installer must determine that the of the FMZ-2000 Flight Management System in interrelationship between this modification accordance with Data List Report No. F9EX- andany other previously installed modification 01026 Revision G dated 20 December 2004 or will introduce no adverse effect upon the later revisions approved by EASA i.a.w. EASA airworthiness of the product.2. The ins 10016643 DASSAULT FALCON JET EASA.IM.A.S.03084 FAA STC ST09715SC-D FALCON 900EX - EASA Validation of FAA STC ST09715SC- D- Installation of the Control Wheel Modifications in accordance with Drawing List Report No. F9EX-01032 10035017 DASSAULT FALCON JET FAA STC ST10657SC-D 1. FALCON 2000EX 2. FALCON 900EX 10028268 DASSAULT FALCON JET - WILMINGTON P- EASA.IM.A.S.03109 Assist Handle Installation:Configuration -501: Main entry door assist handle installationConfiguration -503: Aft lavatory assist handle installationValidation of FAA STC N°ST10657SC-D 1. Prior to installation of this modification the installer must determine that the interrelationship between this modification andany other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2. The ins 20.03.2009 18.03.2009 07.04.2009 11.05.2009 none Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 19.05.2011 FAA STC ST01795NY-D F900EX EASA Validation of FAA STC ST01795NY- This design change is applicable to Dassault Prior to installation of this modification it 14.12.2009 DInstallation of Decrane Aircraft Seating Aviation Mystere Falcon 900aircraft which have must be determined thatthe Company, Inc, Model 80A42S2three place previously been equipped with Dassault interrelationship between this modification partial berthing divan installation in accordance AviationModification M3000 (Falcon 900EX and any other previouslyinstalled withDassault Falcon Jet-Wilmington Master definition) modification and/ or repair will introduce Drawing List, 197900904 RevisionB, dated no adverse effectupon the airworthiness 29th of the product. 10015465 DASSAULT FALCON JET - WILMINGTON EASA.IM.A.S.01217 FAA STC ST01156NY-D MYSTERE FALCON 900 Validation of FAA STC ST01156NY-D: CO Installation of a Honeywell Mark V Enhanced Ground Proximity Warning System (EGPWS) upgrade iaw Master Drawing List 027670321, Rev. - dtd Jan 26, 2001. 10015466 DASSAULT FALCON JET - WILMINGTON EASA.IM.A.S.01218 FAA STC ST01157NY-D MYSTERE FALCON 900 Validation of FAA STC No ST01157NY-D: CO Installation of a Honeywell Electronic Flight Instrument System (EFIS) EDZ-820 Software Upgrade iaw Master Drawing List 027670320, Rev. - dtd. Jan. 26, 2001. 10015467 DASSAULT FALCON JET - WILMINGTON EASA.IM.A.S.01219 FAA STC ST01775NY-D MYSTERE FALCON 900 Validation of FAA STC No ST01775-NY-D: CO Update of Dual Rockwell Collins TCR-94 Transponder for Elementary Surveillance iaw Master Drawing List 126980303, Rev.- dtd. Oct. 15, 2004. 1. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 1. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 1. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 04/01/2013 Page 170/462 31.05.2005 31.05.2005 31.05.2005
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10027110 DASSAULT FALCON JET CORP P- FAA STC SA8300SW-D FALCON 900EX EASA Validation of FAA STC SA8300SW- See those of original FAA STC SA8300SW-D Prior to installation of this modification it 07.09.2009 EASA.IM.A.S.02993 D:Installation of the Automatic Cabin Electrical must be determined thatthe Load Shed System inaccordance with Drawing interrelationship between this modification List Report No. F9EX-01023, Revision E and any other previouslyinstalled dated28th September 2000 or later revisions modification and/ or repair will introduce approved by EASA in accordancewith EASA no adverse effectupon the airworthiness ED De of the product 10027112 DASSAULT FALCON JET CORP P- EASA.IM.A.S.02997 FAA STC SA8283SW-D FALCON 900EX EASA Validation of FAA STC SA8283SW- D:Installation of the Auxiliary Light Modifications in accordance withDrawing List Report No. F9EX-1011, dated 16th October 1996 or laterrevisions approved by EASA in accordance with EASA ED Decision2004/04/CF (or subseq 10016044 DASSAULT FALCON JET CORP. EASA.IM.A.S.02215 ST09737SC-D FALCON 900EX Bracket Installation for Mid Cabin Door i.a.w. Drawing List Report " F90-01093 10016216 DASSAULT FALCON JET CORP. EASA.IM.A.S.02464 FAA STC SA8312SW-D FALCON 50 Installation of the Automatic Cabin Electrical 1. As per FAA STC No. SA8312SW-D2. Load Shed System in accordance with Drawing Prior to installation of this modification the List Report No. F50-01182 Revision A, dated installer must determine that the 27th September 1999 or later approved interrelationship between this modification and revisions. any other previously installed modification will introduce no adverse effect upon the 10016217 DASSAULT FALCON JET CORP. EASA.IM.A.S.02465 FAA STC SA8299SW-D FALCON 50 Installation of Auxiliary Battery System in accordance with Drawing List Report No. F50- 01173, Revision E dated 19th September 2001or later approved revisions. 10016218 DASSAULT FALCON JET CORP. EASA.IM.A.S.02466 FAA STC SA8222SW-D FALCON 50 Installation of the GWS Satellite Data Communication System in accordance with Drawing List Report No. F50-01159, Revision NC, dated 21st July 1993 or later approved revisions. See those of original FAA STC SA8283SW-D Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product 07.09.2009 1. As per FAA STC No. SA8299SW-D.2. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the 1. As per FAA STC No. SA8222SW-D.2. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the 10016219 DASSAULT FALCON JET CORP. EASA.IM.A.S.02467 FAA STC SA7300SW-D FALCON 50 Installation of the Service and Indirect Lighting 1. As per FAA STC No. SA7300SW-D.2. System in accordance with Drawing List Report Prior to installation of this modification the No. F50-01145, Revision L, dated 25October installer must determine that the 2000 or later approved revisions. interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the 10016220 DASSAULT FALCON JET CORP. EASA.IM.A.S.02468 FAA STC ST09316SC-D FALCON 50 Installation of the Standby Instrument Systemn in accordance with Drawing List Report No. F50-01172, Revision B, dated 12th October2000 or later approved revisions. 10016221 DASSAULT FALCON JET CORP. EASA.IM.A.S.02469 FAA STC SA7260SW-D FALCON 50 Installation of the Auxiliary Equipment Rack in accordance with Drawing List Report No. F50- 01116, Revision N, dated 2nd June 1993 or later approved revisions. 10016222 DASSAULT FALCON JET CORP. EASA.IM.A.S.02470 FAA STC SA7069SW-D FALCON 50 Installation of the Centralized Water System in accordance with Drawing List Report No. F50- 01095-2, Revision A, dated 6th September 1999 or later approved revisions. 10016524 DASSAULT FALCON JET CORP. EASA.IM.A.S.02897 FAA STC SA7049SW-D MYSTERE FALCON 900 Installation of Electrical FeedThru in Pressure Vessel. 1. FAA STC No. ST09316SC-D2. Limited to Falcon 50EX version aircraft.3. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification wi 1. As per FAA STC No. SA7260SW-D2. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the 1. As per FAA STC No. SA7069SW-D.2. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. 04/01/2013 Page 171/462 19.12.2006 19.07.2007 09.07.2007 19.07.2007 17.07.2007 19.07.2007 19.07.2007 19.07.2007 23.06.2008
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04/01/2013 Page 1/462 - EASA

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