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>6641 DASSAULT FALCON JET CORP. <strong>EASA</strong>.IM.A.S.03082 FAA STC ST093<strong>01</strong>SC-D FALCON 900EX <strong>EASA</strong> Validation of FAA STC ST093<strong>01</strong>SC- Prior to installation of this modification the<br />
31.03.2009<br />
DInstallation of the Service and Indirect Lighting installer must determine that the<br />
System in accordance with Drawing List report interrelationship between this modification and<br />
No. F9EX-<strong>01</strong>027, Revision B dated<br />
any other previously installed modification<br />
28September 2000 or later revisions approved will introduce no adverse effect upon the<br />
by <strong>EASA</strong> i.a.w. <strong>EASA</strong> ED Decisions<br />
2007/0<strong>01</strong>/C<br />
airworthiness of the product.<br />
10<strong>01</strong>6642 DASSAULT FALCON JET CORP. <strong>EASA</strong>.IM.A.S.03083 FAA STC ST09738SC-D FALCON 900EX <strong>EASA</strong> Validation of FAA STC ST09738SC- Prior to installation of this modification the<br />
31.03.2009<br />
DInstallation of the HF Radio Master System in installer must determine that the<br />
accordance with Drawing List Report No. F9EX-interrelationship<br />
between this modification and<br />
<strong>01</strong><strong>04</strong>4 Revision NC dated 16 September 2002 any other previously installed modification<br />
or later revisions approved by <strong>EASA</strong> i.a.w. will introduce no adverse effect upon the<br />
<strong>EASA</strong> ED Decisions 2007/0<strong>01</strong>/C and<br />
20<strong>04</strong>/<strong>04</strong>/C<br />
airworthiness of the product.<br />
10<strong>01</strong>6215 DASSAULT FALCON JET<br />
<strong>EASA</strong>.IM.A.S.02463 REV. 1 FAA STC ST093<strong>04</strong>SC-D MYSTERE FALCON 50 (MF50) Installation of the Inertial Reference System As per FAA STC ST093<strong>04</strong>SC-D Prior to installation of this modification the <strong>04</strong>.05.2<strong>01</strong>2<br />
CORPORATION<br />
Modifications(installation of Securaplane XL-<br />
installer must determinethat the<br />
245 batteries in lieu of Saft batteriesto provide<br />
interrelationship between this modification<br />
backup power) in accordance with Drawing List<br />
and any otherpreviously installed<br />
report No.F50-<strong>01</strong>188 Revision NC dated 23rd<br />
modification will introduce no adverse<br />
July 1999 or later approve<br />
effect uponthe airworthiness of the<br />
product. The installati<br />
10<strong>01</strong>6224 DASSAULT FALCON JET<br />
<strong>EASA</strong>.IM.A.S.02472 FAA STC ST1<strong>04</strong>23SC-D FALCON 900EX Installation of the Service and Indirect Lighting 1. As per FAA STC ST1<strong>04</strong>23SC-D.2.<br />
26.09.2007<br />
CORPORATION<br />
System (EMTEQ) in accordance with Data List Applicable to Falcon 900EX EASy aircraft<br />
Report No. F9EX-<strong>01</strong><strong>04</strong>8 Revision A dated 07th version.3. F900EX EASy designation does<br />
October 2005 or later revisions of the above not correspond to a new MF900 model<br />
listed documents approved by <strong>EASA</strong> in designation but is a commercial designation for<br />
accordance with <strong>EASA</strong> ED Decision 200 airplanes onwhich the specific Dassault<br />
modificat<br />
10027395 DASSAULT FALCON JET<br />
P-<br />
FAA STC SA8279SW-D MF900, F900EX <strong>EASA</strong> Validation of FAA STC SA8279SW- This design change is also applicable on the Prior to installation of this modification it 28.09.2009<br />
CORPORATION<br />
<strong>EASA</strong>.IM.A.S.03264<br />
D:Installation of the Auxiliary Battery System in Falcon 900C designation asdefined on <strong>EASA</strong> must be determined thatthe<br />
accordance with DrawingList Report No. F9EX- TCDS.A.062<br />
interrelationship between this modification<br />
<strong>01</strong>008, Revision K dated 26th September 2002<br />
and any other previouslyinstalled<br />
orlater revisions approved by <strong>EASA</strong> in<br />
modification and/ or repair will introduce<br />
accordance with <strong>EASA</strong> ED<br />
no adverse effectupon the airworthiness<br />
Decision20<strong>04</strong>/<strong>04</strong>/CF (<br />
of the product.<br />
10028777 DASSAULT FALCON JET<br />
CORPORATION<br />
10029434 DASSAULT FALCON JET<br />
CORPORATION<br />
10035<strong>01</strong>6 DASSAULT FALCON JET<br />
CORPORATION<br />
10035<strong>01</strong>8 DASSAULT FALCON JET<br />
CORPORATION<br />
10035461 DASSAULT FALCON JET<br />
CORPORATION<br />
<strong>EASA</strong>.IM.A.S.02998 FAA STC SA8275SW-D FALCON 900EX 16.07.2009<br />
P-<br />
<strong>EASA</strong>.IM.A.S.02996<br />
FAA STC SA8285SW-D FALCON 900EX <strong>EASA</strong> Validation of FAA STC SA8285SW-D None. Prior to installation of this modification it 24.03.2<strong>01</strong>0<br />
Revision1:Installation of the Security System<br />
must be determined thatthe<br />
(Structural Provisions) inaccordance with<br />
interrelationship between this modification<br />
Drawing List Report No. F9EX-<strong>01</strong>021, Revision<br />
and any other previouslyinstalled<br />
B dated13th June 1997 or later revisions<br />
modification and/ or repair will introduce<br />
approved by <strong>EASA</strong> in accordance with<strong>EASA</strong><br />
no adverse effectupon the airworthiness<br />
ED D<br />
of the product.<br />
FAA STC N° ST10262SC-D F2000EX Oxygen system installation.Installation of added As per FAA STC N° ST10262SC-D, Revision<br />
portion of the continuous flow, dropout<br />
typeoxygen system for the cabin and lavatory.<br />
This system connects to theexisting TC aircraft<br />
oxygen system.Validation of FAA STC N°<br />
ST10262SC-D, Revision 2 Issue date<br />
2 Issue date April 14, 2<strong>01</strong>1.<br />
FAA STC N° ST10584SC-D F2000EX & F900EX Console table installation.Installation of a<br />
Console Table in the main cabin area of the<br />
aircraftside ledge. This table design will<br />
typically be located between twosingle seats<br />
and is not designed to be installed in front of<br />
theemergency escape hatch.Valid<br />
FAA STC N° ST10583SC-D 1. F2000EX<br />
2. F900EX<br />
Galley pocket door installationValidation of<br />
FAA STC N°ST10583SC-D<br />
Prior to installation of this modification it 19.05.2<strong>01</strong>1<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<br />
19.05.2<strong>01</strong>1<br />
Approval is limited to the "-5<strong>01</strong>" configuration. 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 />
24.06.2<strong>01</strong>1<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 173/<strong>462</strong>
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