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 10016525 DASSAULT FALCON JET CORP. EASA.IM.A.S.02898 FAA STC SA7056SW-D MYSTERE FALCON 900 Installation of Automatic Cabin Electrical Load Prior to installation of this modification the 23.06.2008 Shed System. 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. 10016526 DASSAULT FALCON JET CORP. EASA.IM.A.S.02899 REV 1 FAA STC SA7060SW-D MYSTERE FALCON 900 Installation of Basic Interior Furnishings. 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. 23.06.2008 10016527 DASSAULT FALCON JET CORP. EASA.IM.A.S.02900 REV 1 FAA STC SA7062SW-D MYSTERE FALCON 900 Installation of Basic Oxygen System. 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. 23.06.2008 10016528 DASSAULT FALCON JET CORP. EASA.IM.A.S.02901 REV 1 FAA STC SA7085SW-D MYSTERE FALCON 900 Installation of Avionics Rack. 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. 23.06.2008 10016529 DASSAULT FALCON JET CORP. EASA.IM.A.S.02902 REV 1 FAA STC SA7123SW-D MYSTERE FALCON 900 Installation of APU Fault Panel Installation. 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. 23.06.2008 10016530 DASSAULT FALCON JET CORP. EASA.IM.A.S.02903 REV 1 FAA STC SA7239SW-D MYSTERE FALCON 900 Installation of Emergency Power Supply Prior to installation of this modification the 23.06.2008 System. 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. 10016531 DASSAULT FALCON JET CORP. EASA.IM.A.S.02904 REV 1 FAA STC SA7227SW-D MYSTERE FALCON 900 Installation of Air Distribution System Prior to installation of this modification the 23.06.2008 Modification. 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. The install 10016532 DASSAULT FALCON JET CORP. EASA.IM.A.S.02905 REV 1 FAA STC ST09308SC-D MYSTERE FALCON 900 Installation of FMZ-2000 Flight Management System. 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. 10016533 DASSAULT FALCON JET CORP. EASA.IM.A.S.02906 REV 1 FAA STC ST09309SC-D MYSTERE FALCON 900 Installation of Universal Bracket Attachments. 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. 10016585 DASSAULT FALCON JET CORP. EASA.IM.A.S.02990 FAA STC SA8271SW-D FALCON 900EX EASA Validation of FAA STC SA8271SW- Prior to installation of this modification the DInstallation of the APU Fault Panel Installation installer must determine that the i.a.w. Drawing List Report No. F9EX-01007 interrelationship between this modification and dated 08th October 1996 or later revisions any other previously installed modification will approved by EASA i.a.w. EASA ED Decisions introduce no adverse effect upon the 2007/001/C and 2004/04/CF (or subsequent re airworthiness of the product.¿ The 10016589 DASSAULT FALCON JET CORP. EASA.IM.A.S.02995 FAA STC ST09312SC-D FALCON 900EX EASA Validation of FAA STC ST09312SC- DInstallation of the Engine Instrument Display System Modification in accordance with Drawing List Report No. F9EX-1034 Revision NC dated 04th May 2000 or later revisions approved by EASA i.a.w. EASA ED Decisions 2007/0 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 172/462 23.06.2008 23.06.2008 27.03.2009 24.03.2009
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016641 DASSAULT FALCON JET CORP. EASA.IM.A.S.03082 FAA STC ST09301SC-D FALCON 900EX EASA Validation of FAA STC ST09301SC- Prior to installation of this modification the 31.03.2009 DInstallation of the Service and Indirect Lighting installer must determine that the System in accordance with Drawing List report interrelationship between this modification and No. F9EX-01027, Revision B dated any other previously installed modification 28September 2000 or later revisions approved will introduce no adverse effect upon the by EASA i.a.w. EASA ED Decisions 2007/001/C airworthiness of the product. 10016642 DASSAULT FALCON JET CORP. EASA.IM.A.S.03083 FAA STC ST09738SC-D FALCON 900EX EASA Validation of FAA STC ST09738SC- Prior to installation of this modification the 31.03.2009 DInstallation of the HF Radio Master System in installer must determine that the accordance with Drawing List Report No. F9EX-interrelationship between this modification and 01044 Revision NC dated 16 September 2002 any other previously installed modification or later revisions approved by EASA i.a.w. will introduce no adverse effect upon the EASA ED Decisions 2007/001/C and 2004/04/C airworthiness of the product. 10016215 DASSAULT FALCON JET EASA.IM.A.S.02463 REV. 1 FAA STC ST09304SC-D MYSTERE FALCON 50 (MF50) Installation of the Inertial Reference System As per FAA STC ST09304SC-D Prior to installation of this modification the 04.05.2012 CORPORATION Modifications(installation of Securaplane XL- installer must determinethat the 245 batteries in lieu of Saft batteriesto provide interrelationship between this modification backup power) in accordance with Drawing List and any otherpreviously installed report No.F50-01188 Revision NC dated 23rd modification will introduce no adverse July 1999 or later approve effect uponthe airworthiness of the product. The installati 10016224 DASSAULT FALCON JET EASA.IM.A.S.02472 FAA STC ST10423SC-D FALCON 900EX Installation of the Service and Indirect Lighting 1. As per FAA STC ST10423SC-D.2. 26.09.2007 CORPORATION System (EMTEQ) in accordance with Data List Applicable to Falcon 900EX EASy aircraft Report No. F9EX-01048 Revision A dated 07th version.3. F900EX EASy designation does October 2005 or later revisions of the above not correspond to a new MF900 model listed documents approved by EASA in designation but is a commercial designation for accordance with EASA ED Decision 200 airplanes onwhich the specific Dassault modificat 10027395 DASSAULT FALCON JET P- FAA STC SA8279SW-D MF900, F900EX EASA Validation of FAA STC SA8279SW- This design change is also applicable on the Prior to installation of this modification it 28.09.2009 CORPORATION EASA.IM.A.S.03264 D:Installation of the Auxiliary Battery System in Falcon 900C designation asdefined on EASA must be determined thatthe accordance with DrawingList Report No. F9EX- TCDS.A.062 interrelationship between this modification 01008, Revision K dated 26th September 2002 and any other previouslyinstalled orlater revisions approved by EASA in modification and/ or repair will introduce accordance with EASA ED no adverse effectupon the airworthiness Decision2004/04/CF ( of the product. 10028777 DASSAULT FALCON JET CORPORATION 10029434 DASSAULT FALCON JET CORPORATION 10035016 DASSAULT FALCON JET CORPORATION 10035018 DASSAULT FALCON JET CORPORATION 10035461 DASSAULT FALCON JET CORPORATION EASA.IM.A.S.02998 FAA STC SA8275SW-D FALCON 900EX 16.07.2009 P- EASA.IM.A.S.02996 FAA STC SA8285SW-D FALCON 900EX EASA Validation of FAA STC SA8285SW-D None. Prior to installation of this modification it 24.03.2010 Revision1:Installation of the Security System must be determined thatthe (Structural Provisions) inaccordance with interrelationship between this modification Drawing List Report No. F9EX-01021, Revision and any other previouslyinstalled B dated13th June 1997 or later revisions modification and/ or repair will introduce approved by EASA in accordance withEASA no adverse effectupon the airworthiness ED D of the product. FAA STC N° ST10262SC-D F2000EX Oxygen system installation.Installation of added As per FAA STC N° ST10262SC-D, Revision portion of the continuous flow, dropout typeoxygen system for the cabin and lavatory. This system connects to theexisting TC aircraft oxygen system.Validation of FAA STC N° ST10262SC-D, Revision 2 Issue date 2 Issue date April 14, 2011. FAA STC N° ST10584SC-D F2000EX & F900EX Console table installation.Installation of a Console Table in the main cabin area of the aircraftside ledge. This table design will typically be located between twosingle seats and is not designed to be installed in front of theemergency escape hatch.Valid FAA STC N° ST10583SC-D 1. F2000EX 2. F900EX Galley pocket door installationValidation of FAA STC N°ST10583SC-D Prior to installation of this modification it 19.05.2011 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 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 Approval is limited to the "-501" configuration. 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 24.06.2011 04/01/2013 Page 173/462
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04/01/2013 Page 1/462 - EASA

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