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 />
10028563 DASSAULT FALCON SERVICE P-<strong>EASA</strong>.A.S.03652 MYSTERE FALCON 900 Mode S dual transponder installation with This <strong>EASA</strong> approval is applicable on those Prior to installation of this modification it 22.<strong>01</strong>.2<strong>01</strong>0<br />
elementary and enhancedsurveillance Basic Mystere Falcon 900aircraft previously must be determined thatthe<br />
capabilities<br />
equipped with:- Dual ATC Transponders interrelationship between this modification<br />
Honeywell MST-67A P/N 066-<strong>01</strong>143-06<strong>01</strong> and any other previouslyinstalled<br />
withantenna diversity installation- 2 IRS and 2 modification and/ or repair will introduce<br />
ADC AZ 810As per DFS Change Approval no adverse effectupon the airworthiness<br />
Sheet DFS<br />
of the product.<br />
10028776 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.03729 FALCON 900 20.07.2009<br />
10029669 DASSAULT FALCON SERVICE P-<strong>EASA</strong>.A.S.03764 FALCON 900EX F900EX Serial Number 111 aircraft completion This <strong>EASA</strong> design change airworthiness Prior to installation of this modification it 12.<strong>04</strong>.2<strong>01</strong>0<br />
definition<br />
approval is applicable on Falcon900EX serial must be determined thatthe<br />
number aircraft 111<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 />
10032131 DASSAULT FALCON SERVICE MF50 AND FALCON 50EX Stretchers installation.Provide the ability to<br />
install in the aircraft one or two stretchers forair<br />
ambulance according to two configurations:-<br />
One stretcher is installed in the LH side instead<br />
of the two LH fwdseats. - Two stretchers are<br />
installed in the<br />
10032163 DASSAULT FALCON SERVICE MF900 & F900EX 230VAC electrical distribution for galley.An<br />
inverter and a GFI are installed to provide<br />
230AC power on one outletin the galley.<br />
100322<strong>04</strong> DASSAULT FALCON SERVICE F900EX F900EX S/N 086 Cabin Layout<br />
Modification.New interior cabin configuration<br />
features a 12-passenger and 3crewaccommodation.<br />
10033835 DASSAULT FALCON SERVICE P-<strong>EASA</strong>.A.S.03935 FALCON 900EX Falcon 900EX aircraft serial numbers 065 and<br />
073 - CompletionDefinition.<br />
10034125 DASSAULT FALCON SERVICE FAA STC ST02863CH MF50, FALCON 50EX Stretchers installation for medical<br />
evacuation.Provide the ability to install in the<br />
aircraft one or two stretchers forair ambulance<br />
operations.<br />
10034893 DASSAULT FALCON SERVICE F2000, F2000EX 115VAC electrical distribution for<br />
galley.DFSD144 A consists in installing a<br />
28VDC/115VAC inverter, the<br />
associatedprotections and an outlet in the<br />
galley area.<br />
10035568 DASSAULT FALCON SERVICE REV. 1 F900EX, F900C, MF900 B WiFi activation on Falcon 900 non Easy<br />
aircraftThis Major Change to <strong>EASA</strong> STC<br />
10035568 approves the extension<br />
ofapplicability to MF900B aircraft.<br />
This modification is applicable on Mystère<br />
Falcon 50 and Falcon 50EXaircraft equipped<br />
with four seats installed in the LH side and two<br />
seatsand a sofa installed in the RH side as<br />
defined in the Modification SheetDFS5691.This<br />
installation does not cover any<br />
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 />
12.10.2<strong>01</strong>0<br />
Modification applicable to MF900, F900EX Prior to installation of this modification it 13.10.2<strong>01</strong>0<br />
aircraft with :- 1400W available on A4 bus, and- must be determined thatthe<br />
Master switch in cockpit to switch off<br />
interrelationship between this modification<br />
components electricallysupplied in Galley area, and any other previouslyinstalled<br />
and- Master switch in cockpit to switch off all modification and/ or repair will introduce<br />
115/230VAC distributioncircuit<br />
no adverse effectupon the airworthiness<br />
of the product<br />
Modification applicable to F900EX S/N 086<br />
with a pre mod configurationas described in<br />
DFS Modification Sheet DFS9613, Issue A.<br />
Prior to installation of this modification it 15.10.2<strong>01</strong>0<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 />
This <strong>EASA</strong> design change airworthiness Prior to installation of this modification it<br />
approval is applicable only onFalcon 900EX must be determined thatthe<br />
aircraft serial numbers 065 and 073.Associated interrelationship between this modification<br />
limitation: Non commercial air transportation and any other previouslyinstalled<br />
use.<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
This STC does not cover the qualification of<br />
the installed stretcher. Itis to be used in<br />
conjunction with <strong>EASA</strong> STC covering the<br />
validation ofFAA STC ST02863CH.This<br />
modification does not cover the use of any<br />
auxiliary medicalequipment to be used in<br />
conjunct<br />
11.02.2<strong>01</strong>1<br />
Prior to installation of this modification it 09.03.2<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 />
Modification applicable to F2000 & F2000 EX Prior to installation of this modification it 11.05.2<strong>01</strong>1<br />
aircraft with:- 1400W available on A4 bus must be determined thatthe<br />
(version 1) or 1280W (version 2), and- Master interrelationship between this modification<br />
switch in cockpit to switch off components and any other previouslyinstalled<br />
electricallysupplied in Galley area, and- Master modification and/ or repair will introduce<br />
switch in cockpit to switch off<br />
no adverse effectupon the airworthiness<br />
of the product<br />
F900EX and 900C aircraft equipped with WiFi<br />
equipments installationcompliant with<br />
prerequisite note DT-003-10.MF900B aircraft<br />
equipped with WiFi equipments installation<br />
compliantwith prerequisite note DT-0<strong>01</strong>-11.<br />
Prior to installation of this modification it 22.12.2<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 />
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