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 />
10036823 INNOTECH AVIATION TCCA STC NO. SA10-8 BD-700-1A10 I-KU System Installation with VIASAT VMT None Prior to installation of this modification it 10.10.2<strong>01</strong>1<br />
1500 KU Band System<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 />
10037477 INNOTECH AVIATION BD-700-1A10 Installation, Complete Custom Aircraft Interior -<br />
ASN 9416<br />
10<strong>04</strong>0515 INNOTECH AVIATION TCCA STC NO. Q-LSA07-<strong>04</strong>0/D BD-700-1A10 Installation of Iridium Phone System and<br />
interior modification - ASN9028<br />
10<strong>04</strong>0920 INNOTECH AVIATION REV. 1 TCCA STC C-LSA12-105 BD-700-A110 Installation, Complete Custom Aircraft Interior -<br />
ASN 9433<br />
10033170 INNOVATIVE SOLUTIONS AND<br />
SUPPORT, I<br />
10036223 INNOVATIVE SOLUTIONS AND<br />
SUPPORT, I<br />
P-<br />
<strong>EASA</strong>.IM.A.S.03020<br />
P-<br />
<strong>EASA</strong>.IM.A.S.03107<br />
FAA STC ST02372CH B757-200/-300 Installation of Integrated Flat Panel Display<br />
10<strong>01</strong>6867 INTEGRATED FLIGHT SYSTEMS, INC <strong>EASA</strong>.IM.R.S.<strong>01</strong>243 FAA STC SH3509SW EUROCOPTER FRANCE AS 350<br />
B<br />
EUROCOPTER FRANCE AS 350<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 />
C<br />
EUROCOPTER FRANCE AS 350<br />
D<br />
EUROCOPTER FRANCE AS 350<br />
D1<br />
EUROCOPTER FRANCE EC 130<br />
10029611 INTEGRATED FLIGHT SYSTEMS, INC P-<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>407<br />
System (IFPDS) and L-3Avionics Systems GH-<br />
3100 Electronic Standby Instrument System<br />
(ESIS)<br />
Restricted to ASN 9416.Refer to the<br />
Airworthiness Limitations contained in the<br />
requiredAirplane Flight Manual<br />
Supplements.The Wireless LAN System is<br />
intended to provide internet connectivity<br />
andemail services to the airplane’s cabin using<br />
portable electron<br />
Prior to installation of this modification it 29.11.2<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 />
Restricted to ASN 9028.Previous installation of Prior to installation of this modification it 06.07.2<strong>01</strong>2<br />
<strong>EASA</strong> STC No. 10039790 and <strong>EASA</strong> STC No. must be determined thatthe<br />
10039791are pre-requisites.<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 />
Restricted to ASN 9433.The Wireless LAN<br />
System is intended to provide internet<br />
connectivity andemail services to the airplane's<br />
cabin using portable electronic devices(PEDs).<br />
Any other intended function of this equipment<br />
will require are-examination of the<br />
FAA STC ST02165NY B767-200/-300/-300F Installation of Flat Panel Display System Installation Configuration #6 approved only.The<br />
Smiths Aerospace Limited Integrated Standby<br />
Instrument System (ISIS)is not approved for<br />
installation under this STC.No earlier revisions<br />
of the listed documents are approved under<br />
thisSTC.<br />
Installation of a Belt Driven Freon Air<br />
Conditioning System (FAA STC SH3509SW).<br />
REV. 1 STC SR09178RC<br />
B4<br />
600N Integrated Flight Systems Vapor Cycle Air<br />
Conditioning System<br />
Prior to installation of this modification it 09.08.2<strong>01</strong>2<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 />
Approved Installation Configuration #9 only 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 />
21.12.2<strong>01</strong>0<br />
1. VFR Operations only2. This STC is<br />
approved only for the product configuration as<br />
defined in the approved design data referred to<br />
in the paragraphs "Description" and<br />
“Associated Technical Documentation”.<br />
Compatibility with other aircraft/engine con<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 />
23.08.2<strong>01</strong>1<br />
26.<strong>04</strong>.2007<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 />
29.06.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 280/<strong>462</strong>
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