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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>4152 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>273 FALCON 2000 DFSD066 dtd. 19. October 05: Airview 1. This STC is limited to Falcon 2000 S/N<br />

08.11.2005<br />

Communication and Security System 0<strong>01</strong>2. This STC is approved only for the<br />

configuration as defined in Mod Sheet<br />

DFSD066<br />

10<strong>01</strong>4156 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>280 MYSTERE FALCON 200 AFM supplement associated to Dassault Subject AFM supplement is associated to<br />

21.06.2005<br />

Aviation Mod M1632 "Installation d'un hublot Dassault Aviation Mod M1632: "Installation<br />

inférieur avec volet de protection".<br />

d'un hublot inférieur avec volet de<br />

protection",applicable to F20 GF SN 397 only<br />

10<strong>01</strong>4170 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>303 FALCON 10 Antenna installation 1. This STC is approved only for the<br />

configuration as defined in Mod Sheet DFS<br />

1263.2. Compatibility with other aircraft/engine<br />

configurations shall be determined by the<br />

installer.<br />

10<strong>01</strong>4172 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>305 MYSTERE FALCON 50 Introduction of Pressure Seals for wire runs This STC is approved only for the configuration<br />

as defined in Mod Sheet DFS<br />

5610.Compatibility with other aircraft/engine<br />

configurations shall be determined by the<br />

installer.<br />

10<strong>01</strong>4217 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>378 MYSTERE FALCON 900 Call out evolution with EGPWS Honeywell Applicable to all MF900 aircraft with<br />

Mark V 212-212.This STC supersedes the STC modification DFS 9259<br />

F-C163-SF-2107 <strong>EASA</strong> approved on March 9,<br />

20<strong>04</strong> with the reference 20<strong>04</strong>-2073.<br />

10<strong>01</strong>4243 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>452 MYSTERE FALCON 20 Deviation to M GE 2 - Pressure seals FR17-18 1. This STC is applicable to Falcon 20S/N 103<br />

only2. This STC is to be applied simultaneously<br />

with Dassault Aviation Mod M GE23.<br />

Compatibility with other aircraft/engine<br />

configurations shall be determines by the<br />

installer<br />

10<strong>01</strong>4255 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>481 FAN JET<br />

DFS 2545 dtd. 12. October 05: Camera and This STC approves the installation only, system<br />

MYSTERE FALCON 20<br />

Video Recorder installation<br />

activation is not considered.<br />

10<strong>01</strong>4263 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>493 Installation of two V/UHF AN/ARC210 1. This STC is applicable to Falcon 20 SN 076<br />

only2. System activation is not considered3.<br />

This STC is approved only for the configuration<br />

as defined in Mod Sheet DFS 25434.<br />

Compatibility with other aircraft/engine<br />

configurations shall be determined<br />

10<strong>01</strong>4267 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>496 MYSTERE FALCON 20 Antenna relocations, skin repairs 1. This STC is only approved for the<br />

configuration as defined in Mod Sheet DFS<br />

2558 Issue Original<br />

14.09.2005<br />

10<strong>01</strong>4270 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>500 FALCON 10 GPS Antenna installation 1. Applicable to Falcon 20 S/N 103 only. 16.08.2005<br />

10<strong>01</strong>4274 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>510 FALCON 20 Time Base Installation. 1. This STC is applicable to Falcon 20 SN 076<br />

only 2. System activation is not considered 3.<br />

This STC is approved only for the configuration<br />

as defined in Mod Sheet DFS 2548 4.<br />

Compatibility with other aircraft/engine<br />

configurations shall be determined b<br />

18.08.2005<br />

10<strong>01</strong>4276 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>512 FALCON 10 Frame 0 Pressure Seal through-fitting<br />

modification (enlarge pressure seals)<br />

This STC is approved only for the configuration<br />

as defined in Mod Sheet DFS 1272 Issue<br />

Original. Compatibility with other aircraft/engine<br />

configurations shall be determined by the<br />

installer.<br />

10<strong>01</strong>4284 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>521 MYSTERE FALCON 20 Power Utility System activation is not considered 28.09.2005<br />

10<strong>01</strong>4294 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>536 MYSTERE FALCON 20 DFS 2562 dtd 21.Dec 05: Master Mission 1. This STC is approved only for the<br />

25.<strong>01</strong>.2006<br />

Function<br />

configuration as defined in Mod Sheet DFS<br />

25622. Compatibility with other aircraft/engine<br />

configurations shall be determinded by the<br />

installer<br />

10<strong>01</strong>4332 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>586 FALCON 10 Update ATC Transponder for elementary This STC is approved only for the configuration<br />

10.10.2005<br />

surveillance DFS 1253 issue A<br />

as defined in Mod Sheet DFS 1253.<br />

10<strong>01</strong>4334 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>589 FALCON 10 DFS1226 Revision D dated 9 June 2005:<br />

Installation of Collins TCAS 4000with one or<br />

two TDR-94D<br />

10<strong>01</strong>4383 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>667 MYSTERE FALCON 2000<br />

MYSTERE FALCON 2000EX<br />

DFS D078 dtd. 5.4.2006: EGPWS Software<br />

222-222<br />

This STC is approved only for the configuration<br />

as defined in Mod Sheet DFS 1226.<br />

1. Activation of Runway Awareness Advisory<br />

System (RAAS) is not approved through this<br />

STC2. This STC is approved only for the<br />

configuration as defined in Mod Sheet DFS<br />

D0782. Compatibility with other aircraft/engine<br />

configurations shall be determined by th<br />

<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 175/<strong>462</strong><br />

10.08.2005<br />

22.09.2005<br />

<strong>04</strong>.07.2005<br />

22.09.2005<br />

08.11.2005<br />

09.08.2005<br />

24.08.2005<br />

10.10.2005<br />

07.07.2006

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