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 />
10038677 L D AVIATION PRAGUE, s.r.o. F172M<br />
Avionics upgrade - installation of:GMA 340 None. Prior to installation of this modification it 07.03.2<strong>01</strong>2<br />
F172N<br />
(audio), SL 40 (VHF COMM), SL 30 (VHF<br />
must be determined thatthe<br />
F172P<br />
NAV/COMM),MD 200-306 (CDI indicator),<br />
interrelationship between this modification<br />
GTX 328 (Mode S XPNDR), CI 102<br />
and any other previouslyinstalled<br />
(MKRantenna), Kannad 406 AF Compact<br />
modification and/ or repair will introduce<br />
(ELT), AV 200 (ELT antenna), CI 105(XPNDR<br />
no adverse effectupon the airworthiness<br />
antenna).<br />
of the product.<br />
10<strong>01</strong>6133 L-3 COMMUNICATIONS INTEGRATED <strong>EASA</strong>.IM.A.S.02329 FAA STC ST9765SC-D BOEING 767 Installation of a First-Class Interior/The project<br />
installs an all first-class interior in a Swiss<br />
registered Boeing 767 aircraft. This interior<br />
consists of installing 54seats, a bar and dining<br />
area, and upgrades to entertainment system<br />
1. Instruction for Continued Airworthiness<br />
(ICA) dated May 1, 2007.2. This approval is<br />
limited to only the installation made in the<br />
Boeing Model B767-306, Serial Number 30393<br />
aircraft.<br />
10<strong>01</strong>6313 L-3 COMMUNICATIONS INTEGRATED <strong>EASA</strong>.IM.A.S.02617 FAA STC ST091<strong>01</strong>AC-D BOEING 737-700 IGW<br />
electronics.<br />
Modification of aircraft environmental control Raytheon Systems Company "Type Design<br />
system.<br />
Data List" Report no. 98<strong>01</strong>03<strong>04</strong>-000.<br />
10<strong>01</strong>6314 L-3 COMMUNICATIONS INTEGRATED <strong>EASA</strong>.IM.A.S.02618 FAA STC ST09102AC-D BOEING 737-700 IGW Installation of passenger gaseous oxygen Raytheon Systems Company "Type Design<br />
equipment.<br />
Data List" Report no. 98<strong>01</strong>02<strong>04</strong>-000.<br />
10<strong>01</strong>6854 L-3 WESCAM INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>230 REV. 1 TCCA STC SH<strong>04</strong>-29 EUROCOPTER FRANCE AS 350 MX-15 camera installation (structural provisions<br />
B<br />
only).Note: The revision extends the<br />
EUROCOPTER FRANCE AS 350 applicability of STC <strong>EASA</strong>.IM.R.S.<strong>01</strong>230 to<br />
B1<br />
EUROCOPTER FRANCE AS 350<br />
B2<br />
EUROCOPTER FRANCE AS 350<br />
B3<br />
EUROCOPTER FRANCE AS 350<br />
BA<br />
EUROCOPTER FRANCE AS 350<br />
D<br />
EUROCOPTER FRANCE AS<br />
355N<br />
AS355N.<br />
10<strong>01</strong>7071 L-3 WESCAM INC. <strong>EASA</strong>.IM.R.S.<strong>01</strong>507 REV. 1 TCCA STC SH<strong>04</strong>-29 SEE <strong>EASA</strong> APPROVED MODEL MX-Series Camera Installation (Structural This STC is for structural provisions only. Placard containing the following<br />
LIST<br />
Provisions Only)Note: This revision to the STC Functional and electricalaspects will require limitations to be installed in clearview of<br />
adds a second Downlink antenna<br />
separate airworthiness approval.VNE limited to the pilot:AS350: VNE Limited to 126<br />
(OMNIAntenna) and a MX-10 Camera 126ktsVFR OnlyCategory A operations KIAS, VFR Operations OnlyAS355:<br />
applicability.<br />
prohibited<br />
Category A operations prohibited. VNE<br />
Limited to 126 KIAS, VFROperations<br />
OnlyPrior to installation of this modi<br />
10027823 L-3 WESCAM INC. P-<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>517<br />
REV. 1 TCCA STC SH97-31 1. AS350 B, B1, B2, B3, BA, D<br />
2. AS355 E, F, F1, F2, N, NP<br />
MX-Series Camera Installation (Structural<br />
Provisions Only)<br />
This STC is for structural provisions only.<br />
Functional and electricalaspects will require<br />
separate airworthiness approval.VNE limited to<br />
126ktsVFR OnlyCategory A operations<br />
prohibited<br />
10<strong>01</strong>5833 LAKE & AIR INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>924 FAA STC SA39CH SEE ATTACHED <strong>EASA</strong><br />
Installation of an Amphibian Landing Gear<br />
APPROVED TYP<br />
Position Advisory System<br />
10<strong>01</strong>5759 LAKE CENTRAL AIR SERVICES <strong>EASA</strong>.IM.A.S.<strong>01</strong>795 TCCA STC SA-05-71 LAKE LA 4/200 Horizontal Stabilizer Attachment Fitting P/N LC- - Parts must be manufactured in accordance<br />
2200-21 TCCA STC SA-05-71 issued on 8th with Lake Central Air Services Drawing LC-<br />
July 2005<br />
2200-21, Rev. 0, dated July 06, 2005, and<br />
LakeCentral Air Services Manufacturing<br />
Procedures MP-LC-2200-21, Rev. B, dated<br />
July 06, 2005, or later approved revisions.- Inst<br />
10<strong>01</strong>54<strong>01</strong> LANDMARK AVIATION <strong>EASA</strong>.IM.A.S.<strong>01</strong>111 FAA STC ST451CH-D CESSNA 650 Installation of an AlliedSignal Avionics MK-VII,<br />
Enhanced Ground Proximity Warning System<br />
1. This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
10<strong>01</strong>5402 LANDMARK AVIATION <strong>EASA</strong>.IM.A.S.<strong>01</strong>112 FAA STC ST451CH-D CESSNA 650<br />
installer.<br />
Installation of a Bendix/King CAS 67A TCAS II 1. This STC is approved only for the product<br />
System with Dual Bendix/King MST-67A Mode configuration as defined in the approved design<br />
S Transponders<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
Placard containing the following<br />
limitations to be installed in clearview of<br />
the pilot:AS350: VNE Limited to 126<br />
KIAS, VFR Operations Only AS355:<br />
Category A operations prohibited. VNE<br />
Limited to 126 KIAS, VFROperations<br />
Only Prior to installation of this mo<br />
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15.05.2007<br />
11.02.2008<br />
11.02.2008<br />
21.<strong>01</strong>.2008<br />
14.<strong>01</strong>.2<strong>01</strong>1<br />
<strong>04</strong>.<strong>01</strong>.2<strong>01</strong>1<br />
21.06.2006<br />
18.<strong>04</strong>.2006<br />
24.03.2005<br />
24.03.2005