04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10<strong>01</strong>5937 DEVORE AVIATION CORPORATION OF <strong>EASA</strong>.IM.A.S.02078 REV 1 FAA STC SA7473SW BOEING 757 Installation of tail floodlights in accordance with<br />
DeVore Drawing No. 757000<strong>01</strong>, Rev B, dated<br />
September 14, 1988, or later FAA approved<br />
revision.<br />
02.<strong>04</strong>.2007<br />
10<strong>01</strong>5947 DEVORE AVIATION CORPORATION OF <strong>EASA</strong>.IM.A.S.02089 SA998EA BOMBARDIER DHC-6 SERIES Installation of Engine Fuel Drain Recirculation<br />
18.10.2006<br />
100<br />
BOMBARDIER DHC-6 SERIES<br />
200<br />
BOMBARDIER DHC-6 SERIES<br />
300<br />
System<br />
10<strong>01</strong>6743 DEVORE AVIATION CORPORATION OF <strong>EASA</strong>.IM.R.S.<strong>01</strong>069 FAA STC SH4694SW S-76A/B/C Installation of Under Fuselage forward facing This STC is approved only for the product<br />
31.05.2006<br />
recognitionn lights and rotor disc lights 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 />
10<strong>01</strong>6744 DEVORE AVIATION CORPORATION OF <strong>EASA</strong>.IM.R.S.<strong>01</strong>070 FAA STC SH5867SW AS 365N/N1/N2, EC 155B/B1 Installation of Tail Floodlights and Associated 1. This STC is approved only for the product<br />
21.06.2005<br />
Technical Documentation Devore Drawing List configuration as defined in the approved design<br />
365000<strong>01</strong> Revision J dated March 16 data referred to in the paragraph "Description".<br />
1999DCN F-1 dated February 8 1989 & DCN L-Compatibility<br />
with other aircraft/engine<br />
1 dated October 22 20<strong>01</strong> or later approved configurations shall be determined by the<br />
revision<br />
installer.<br />
10<strong>01</strong>6745 DEVORE AVIATION CORPORATION OF <strong>EASA</strong>.IM.R.S.<strong>01</strong>071 FAA STC SH5866SW AS 365N/N1/N2, EC 155B/B1 Installation of Forward Facing Recognition 1. This STC is approved only for the product<br />
21.06.2005<br />
Lights<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 />
10<strong>01</strong>6746 DEVORE AVIATION CORPORATION OF <strong>EASA</strong>.IM.R.S.<strong>01</strong>072 FAA STC SH7579SW AS 365N1/N2/N3, EC 155B/B1 Installation of a rotor disc light and associated 1. This STC is approved only for the product<br />
22.06.2005<br />
DeVore Aviation Corporation Top Drawing- configuration as defined in the approved design<br />
Rotor Disc Light Inspection;<br />
data referred to in the paragraph "Description".<br />
AerospatialeDauphin Drawing 36500003 Compatibility with other aircraft/engine<br />
revision E dated August 21 20<strong>01</strong> or later configurations shall be determined by the<br />
approved revision DeVore Aviation<br />
Corporation RFM Supplem<br />
installer.<br />
10<strong>01</strong>7026 DEVORE AVIATION CORPORATION OF <strong>EASA</strong>.IM.R.S.<strong>01</strong>445 FAA STC SH3754SW Installation of DeVore forward facing<br />
recognitions lights<br />
<strong>01</strong>.07.2008<br />
10028007 DEVORE AVIATION CORPORATION OF FAA STC SR09557RC R44II Installation of Tail/Rotor, Forward Facing None Prior to installation of this modification it 24.11.2009<br />
Recognition and FuselageFloodlights in<br />
must be determined thatthe<br />
accordance with DeVore Aviation Corporation<br />
interrelationship between this modification<br />
DrawingNumber 440000<strong>01</strong>. This installation is<br />
and any other previouslyinstalled<br />
based on FAA STC SR09557RC.<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong>6995 DIAMOND J, INC <strong>EASA</strong>.IM.R.S.<strong>01</strong>4<strong>04</strong> FAA STC NO. SR00031LB DATED MA BELL 206B<br />
BELL 206L<br />
BELL 206L-1<br />
BELL 206L-3<br />
BELL 206L-4<br />
Installation of Analog/Digital Turbine Outlet<br />
Temperature (TOT) Indicator with Exceedance<br />
logging Capability. This STC has been<br />
classified as "Basic" by FAA and has been<br />
approved under the PTVP.<br />
10<strong>01</strong>5149 DIEHL SERVICE MODULES GmbH <strong>EASA</strong>.A.S.03509 REV 1 BOEING 777-200 Installation of Galleys and Closets on BAW<br />
B777-236, Kit P/N 190331-51<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any otherpreviously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The installa<br />
10<strong>01</strong>4433 DINAN AVIATION SIBA AVIONIQUE <strong>EASA</strong>.A.S.02481 PIPER PA-31T Modification SIBA MD<strong>01</strong>_2006Replacement of This STC is limited to: S/N 31T-7920094 F-<br />
one ATC mode C by Mode S and replacement GPBF<br />
of an old DME with adding an ATC antenna on<br />
the top of frame<br />
31.08.2006<br />
10030311 DINAN AVIATION SIBA AVIONIQUE PA28 R 2<strong>01</strong> T M05-2009 Rev. 0 modernisation du système<br />
de communication.<br />
None. None. 10.06.2<strong>01</strong>0<br />
10039614 DONICA INTERNATIONAL LIMITED REV. 1 MD-90-30 AE-DMR300 Digital Media Reproducer in lieu<br />
of existing Rockwell Collinsor Panasonic<br />
analogue Hi 8 video tape reproducer.<br />
05.03.2008<br />
24.11.2008<br />
None Amendment to the STC is required in<br />
order to extend applicability tothose types<br />
listed in the attached AML list. The<br />
amendment to the STCshall provide the<br />
installation instructions and ICA to<br />
supplement thecommon data package<br />
that is defined within Modific<br />
16.05.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 187/<strong>462</strong>
Change language