04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10039722 EMBRAER GPX Ltda. (PC 722) ANAC STC NO. 2009S10-20 EMB-135BJ The Certification Basis for the original product<br />
remains applicable tothis certificate/<br />
approval.The requirements for environmental<br />
protection and the associatedcertificated noise<br />
and/or emissions levels of the original product<br />
areunchanged and remain appl<br />
none none 18.05.2<strong>01</strong>2<br />
10031622 EMBRAER S.A. EMB-500 <strong>01</strong>.09.2009<br />
10032105 EMS AVIATION, Inc. REV. 1 FAA STC SR03333AT S-76A, S-76B, S-76C Installation of the Sky Connect Satellite Phone None Prior to installation of this modification it 21.09.2<strong>01</strong>1<br />
and Tracking 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 />
10038432 EMS AVIATION, Inc. FAA STC SR09583RC EC135 P1/P2/P2+/T1/T2/T2+ Installation of the Sky Connect Forte Iridium<br />
Satellite Phone and /orautomated reporting<br />
system (FAA STC SR09583RC)<br />
10<strong>04</strong>1<strong>01</strong>7 EMS AVIATION, Inc. FAA STC NO SR02569NY AS 350 B,AS 350 B1,AS 350 B2<br />
AS 350 B3,AS 350 BA,AS 350 D<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 />
16.02.2<strong>01</strong>2<br />
Installation of Sky Connect Tracking System This STC is not applicable to AS350B3 model If the holder agrees to permit another<br />
iaw Master Drawing ListMDL07094This STC is helicopters withmodification OP4305 (Arriel 2D person to use this certificate tomodify a<br />
the validation of FAA STC SR02569NY (last engine installation) incorporated.<br />
product, the holder must give to the other<br />
reissued April 15,2009)<br />
person writtenevidence of that<br />
permission.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship<br />
10<strong>01</strong>6107 EMS TECHNOLOGIES CANADA LTD <strong>EASA</strong>.IM.A.S.02297 TCCA STC SA05-12, ISSUE 3, DAT Installation of EMS HSD-64/-128/-X/-400/-400i/- This STC is approved only for the product<br />
HD-710 High Speed Data Transceiver 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 />
10<strong>01</strong>5314 EMTEQ <strong>EASA</strong>.IM.A.S.0<strong>01</strong>84 FAA STC ST00221AT B727-100, B727-200 Installation of a Digital Flight Data Recorder<br />
Upgrade from 6 to 11 channels in accordance<br />
with Avitas Engineering Report No 92AMJT.<br />
003 R-1, Revision B, dated May 4, 1993 or<br />
later<br />
1. This approval should not be extended to<br />
other aircraft of this modelon which other<br />
previously approved modifications are<br />
incorporated, unless it is determined by the<br />
installer that the interrelationship between this<br />
10<strong>01</strong>5315 EMTEQ <strong>EASA</strong>.IM.A.S.0<strong>01</strong>85 FAA STC ST02006AT 727-100, 727-200<br />
change and any other previously ap<br />
Installation of an Allied Signal 18 Channel Flight 1. This approval should not be extended to<br />
Data Recorder (Upgrade) for Aircraft not other aircraft of this model on which other<br />
containing a Flight Data Acquisition Unit in previously approved modifications are<br />
accordance with Avitas Engineering Report No incorporated, unless it is determined by the<br />
99AMJT.<strong>04</strong>0R-1, No Revision, dated march installer that the interrelationship between this<br />
15, 1999, Appendix A, master Drawi<br />
change and any other previously a<br />
10<strong>01</strong>5645 EMTEQ <strong>EASA</strong>.IM.A.S.<strong>01</strong>609 REV 1 FAA STC ST02<strong>01</strong>9AT B767-300 Installation of Passenger Cabin Interior<br />
Arrangement<br />
10<strong>01</strong>5316 EMTEQ ENGINEERING <strong>EASA</strong>.IM.A.S.0<strong>01</strong>88 FAA STC ST02869AT BOEING 767-300 Installation of a passenger cabin interior<br />
arrangement in accordance with Master<br />
Drawing List ANST-<strong>04</strong>8-MDL, Revision C<br />
dated 27/05/20<strong>04</strong> or later <strong>EASA</strong> approved<br />
revision<br />
10<strong>01</strong>54<strong>04</strong> EMTEQ ENGINEERING <strong>EASA</strong>.IM.A.S.<strong>01</strong>115 FAA STC ST02780AT BOEING 757-200 Installation of Honeywell Mark V Enhanced<br />
Ground Proximity Warning System (EGPWS)<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification<br />
will introduce no adverse effect upon the<br />
airworthiness of the prod<br />
1. Subject to compliance with the provisions<br />
of Part 21 Subpart E, this STC and associated<br />
data shall remain valid until surrendered,<br />
withdrawn or otherwise terminated2. If<br />
transfer of this Certificate is requested under<br />
Part 21A.116 the STC will be<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 />
installer.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 206/<strong>462</strong><br />
15.08.2<strong>01</strong>2<br />
27.06.2007<br />
07.10.20<strong>04</strong><br />
07.10.20<strong>04</strong><br />
02.02.2009<br />
<strong>01</strong>.10.20<strong>04</strong><br />
<strong>04</strong>.05.2005
Change language