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 />
10035668 SKY IMD Inc. REV. 1 SEE APPROVED MODEL LIST Installation of Sensor Pod and wiring for This STC is for installation of the sensor pod The installation of this modification by 08.07.2<strong>01</strong>1<br />
passenger operated monitoringsystem and wiring from thesensor pod into fuselage. third persons is subject towritten<br />
This STC does not include power to the permission of the approval holder and<br />
sensorpod or the sensor control unit.Limitations disposal of the approvedappropriate<br />
as defined in the applicable Aircraft Flight documentation. Prior to installation of this<br />
ManualSupplements.<br />
modification it must be determined<br />
thatthe interrelationship<br />
10<strong>01</strong>5785 SKY INTERNATIONAL Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>841 REV 1 SA1<strong>04</strong>63SC AVIAT HUSKY A-1B Installation of a Lycoming model IO-360-A1D6 The engine must be de-rated to 196 HP (see<br />
23.08.2006<br />
engine (derated to 196 HP) and MT Propeller Installation Instructions for details).The Airplane<br />
model MTV-15-B/205-58 propeller in<br />
Flight Manual Supplement No 55009-18,<br />
accordance with Installation Instructions No Revision IR or later <strong>EASA</strong> approved revision,<br />
11<strong>01</strong>, Revision C dated 8 May 2006, or later must be used with this modification.The<br />
approved revision<br />
approved Noise Level is 81.6 dB(A).<br />
10035483 SKYE AVIONICS Ltd. TCCA STC SH11-14 BELL 407 Installation of "Check Engine Instruments"<br />
Audio Alert System.<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 />
27.06.2<strong>01</strong>1<br />
10<strong>04</strong>2298 SKYTECH, INC. <strong>EASA</strong>.IM.A.S.006<strong>04</strong> FAA STC ST<strong>01</strong>851NY PA46-310P 1- Skytech Inc. Airplane Flight Manual<br />
Supplement, HTW-494-782-100<br />
FAAApproved December 31, 2003, is<br />
required for this modification.2- This STC<br />
is approved only for the product<br />
configuration as defined inthe approved<br />
design data referred to in the paragrap<br />
02.03.2005<br />
10<strong>01</strong>6790 SKYTRAC SYSTEMS Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>137 REV. 2 TCCA STC SH05-42 BELL 407<br />
SkyTrac ISAT-100 Airborne Position/Data 1. Equipment configuration: ISAT-100 (no<br />
13.02.2006<br />
EUROCOPTER DEUTSCHLAND Communicator System Installation.TCCA STC mod.)/mod A, or later TCCA approved major<br />
BO-105<br />
SH05-42 Issue no 1 dated 12 September 2005 mod.2. This STC references specified<br />
interfacing equipment that is approved via this<br />
data. The ISAT-100 equipempment is capable<br />
of being interfaced to additional aircr<br />
10<strong>01</strong>6798 SKYTRAC SYSTEMS Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>151 REV. 2 TCCA STC SH03-30 ISSUE 4 BELL 212<br />
BELL 412<br />
BELL 412 CF<br />
BELL 412 EP<br />
EUROCOPTER FRANCE SA<br />
365C<br />
EUROCOPTER FRANCE SA<br />
365C1<br />
EUROCOPTER FRANCE SA<br />
365N<br />
SIKORSKY S-61N<br />
SIKORSKY S-76A<br />
SIKORSKY S-76C<br />
10<strong>01</strong>6927 SKYTRAC SYSTEMS Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>313 TCAA STC SH03-30 ISSUE 5 EUROCOPTER FRANCE AS<br />
365C<br />
EUROCOPTER FRANCE AS<br />
365C1<br />
EUROCOPTER FRANCE AS<br />
365N<br />
EUROCOPTER FRANCE EC<br />
155B<br />
Installation of SkyTrac ISAT-100 Airborne 1. This STC references specific interfacing<br />
Position/Data Communicator SystemRevison 1 equipment that is approved via this data.<br />
to add: BK-117 A-1, A-3, A-4, B-1 and B-2 The ISAT-100 equipment is capable of being<br />
modelsRevision 2 to add: Eurocopter SA 365 interfaced to additional aircraft systems for<br />
C, C1, N, EC 155B<br />
wich approval is beyond the scope of this STC.<br />
Such interfaces may<br />
Installation of SkyTrac ISAT-100 Airborne This STC references specific interfacing<br />
Position/ Data Communication System Note: equipment that is approved via this data. The<br />
This application is to amend an existing <strong>EASA</strong> ISAT 100 equipment is capable of being<br />
STC (Ref P-<strong>EASA</strong>.IM.R.S.0<strong>01</strong>151 Rev. 1) to interfaced to additional aircraft systems for<br />
add the SA 365 C,C1,N, EC 155B helicopter which approval is beyond the scope of this<br />
models<br />
STC. Such interfaces may need further ap<br />
10030917 SKYTRAC SYSTEMS Ltd. TCCA STC SA09-93 SkyTrac Flight Following / SATCOM Installation<br />
in acc. with TCCA STCSA09-93:ISAT-100<br />
transceiver installed in aft zone of aircraft, Dual<br />
elementGPS/Iridium antenna installed on upper<br />
fuselage, optional DVI-250 andCDP-250<br />
control panels installed at centre<br />
21.03.2007<br />
21.03.2007<br />
None None 12.07.2<strong>01</strong>0<br />
10030918 SKYTRAC SYSTEMS Ltd. TCCA STC SA09-80 CESSNA 208, 208B SkyTrac Flight Following / SATCOM Installation None<br />
in acc. with TCCA STCSA09-80, Issue 1:ISAT-<br />
100 transceiver installed in aft zone of aircraft,<br />
Dual elementGPS/Iridium antenna installed on<br />
upper fuselage, optional DVI-250 andCDP-250<br />
control panels installed a<br />
None 12.07.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 408/<strong>462</strong>
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