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 />
10037659 DASSAULT FALCON JET<br />
FAA STC ST10890SC-D F2000EX Aft RH Divan installationValidation of FAA STC As per FAA STC N°ST10890SC-D Prior to installation of this modification it 14.12.2<strong>01</strong>1<br />
CORPORATION<br />
N°ST10890SC-D<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 />
10037660 DASSAULT FALCON JET<br />
CORPORATION<br />
FAA STC ST10891SC-D F2000EX Avionics and interiors installationValidation of<br />
FAA STC N°ST10891SC-D<br />
10<strong>01</strong>3990 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>022 MYSTERE FALCON 20-5 Installation of Collins TCAS-4000 and of 2 ATC<br />
TDR 94D capable of elementary surveillance.<br />
10<strong>01</strong>4<strong>01</strong>8 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>065 MYSTERE FALCON 50 Installation of a Honeywell Mark V EGPWS<br />
soft 217-217 with terrain display in the Collins<br />
EFIS 86-C14<br />
10<strong>01</strong>4030 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>096 MYSTERE FALCON 50 Installation of a Honeywell Mark VII EGPWS<br />
soft 217-217 with terrain display in the MFD<br />
10<strong>01</strong>4052 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>134 FALCON 10 DFS 1261 dtd 13.Oct 2005: Installation of a<br />
TAWS Honeywell Mark VIII EGPWS soft <strong>01</strong>1<br />
10<strong>01</strong>4071 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>161 FALCON 10 DFS 1255 dtd. 29.3.06: Installation of two FMS<br />
UNS-1L Soft 802.X / B-RNAV & P-RNAV<br />
10<strong>01</strong>4072 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>163 REV. 1 FALCON 10 DFS 1252 dtd. 9.6.05: EFIS Universal EFI<br />
550/600<br />
10<strong>01</strong>4099 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>200 FALCON 10 Installation of Collins ATC with flight ID and<br />
Gables Control Panel<br />
10<strong>01</strong>4117 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>224 FALCON 10 DFS 1251 dtd. 2.6.05: Installation of a Multi<br />
functional display MFD 640<br />
As per FAA STC N°ST10891SC-DRestricted<br />
to F2000EX S/N 216<br />
1. Applicable to Mystère Falcon 50 equipped<br />
with Collins EFIS 86-C14 only2. This STC is<br />
approved only for the product configuration as<br />
defined in the approved design data referred to<br />
in the paragraph "Description". Compatibility<br />
with other aircraft/engine<br />
This STC is only valid for Falcon 50 equipped<br />
with a Universal FMS UNS-1B with GPS-1000,<br />
or UNS-1C/1C+/1D/1E/1F/1K/1K+/1L and with<br />
Collins EFIS-86C(x)/weather radar WXR-350<br />
1. This STC is approved only for the<br />
configuration as defined in Mod Sheet DFS<br />
1261.2. Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer<br />
1. This STC is approved only for the<br />
configuration as defined in Mod Sheet DFS<br />
1255. Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraphs "Description"<br />
and “Associated Technical Documentation”.<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined<br />
STC applicable only to Falcon 10 aircraft<br />
equipped with:- 2 Collins ATC TDR-94D p/n<br />
622-9210-0<strong>01</strong>/002/003 or 0<strong>04</strong>.- and ATC<br />
control box Gables G7 130-XX.<br />
1. This STC is approved only for the<br />
configuration as defined in Mod Sheet DFS<br />
1251. Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer<br />
10<strong>01</strong>4118 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>225 MYSTERE FALCON 900 EGPWS Software Evolution (222-222) Applicable to MF900 equipped with EGPWS<br />
Mark V soft 212-212 installed with DFS 9259<br />
STC<br />
10<strong>01</strong>4119 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>226 MYSTERE FALCON 900 Incorporation of RAAS function on EGPWS<br />
soft 222-222<br />
Applicable to MF900 equipped with EGPWS<br />
Mark V soft 222-222 installed with DFS 9472<br />
STC<br />
10<strong>01</strong>4137 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>248 FALCON 10 DFS 1250 dtd. 22.3.06: Weather Radar Primus 1. This STC is approved only for the<br />
660<br />
configuration as defined in Mod Sheet DFS<br />
1250. Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer<br />
10<strong>01</strong>4141 DASSAULT FALCON SERVICE <strong>EASA</strong>.A.S.<strong>01</strong>254 MYSTERE FALCON 20-5 Installation of one FMS Universal UNS-1L<br />
SOFT 802.X in accordance with the Change<br />
Approval Sheet -Original- or later <strong>EASA</strong><br />
approved revisions.<br />
Operation of the Flight Management System in<br />
the Approach Mode is not allowed<br />
Prior to installation of this modification it 14.12.2<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 />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 174/<strong>462</strong><br />
28.<strong>04</strong>.2005<br />
03.02.2005<br />
15.02.2005<br />
02.05.2006<br />
02.05.2006<br />
11.<strong>01</strong>.2007<br />
11.<strong>04</strong>.2005<br />
02.05.2006<br />
12.12.2005<br />
06.10.2006<br />
02.05.2006<br />
19.05.2005
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