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 />
10<strong>01</strong>6261 JET AVIATON ST. LOUIS, Inc. <strong>EASA</strong>.IM.A.S.02540 FAA STC ST4837WI-T BOMBARDIER CL-600-2B16 Installation of an Audio International Articulated Prior to installation of this modification the<br />
03.10.2008<br />
Mounting Arm and Data Connectivity for an installer must determine that the<br />
Electronic Flight Bag<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
10<strong>01</strong>6411 JET AVIATON ST. LOUIS, Inc. <strong>EASA</strong>.IM.A.S.02743 FAA STC ST00754WI BOMBARDIER CL-600-1A11 (CL-<br />
600<br />
BOMBARDIER CL-600-2A12 (CL-<br />
6<strong>01</strong><br />
BOMBARDIER CL-600-2B16<br />
Installation of Emergency Lighting System. This STC must be installed with Cabin interior<br />
arrangement per <strong>EASA</strong> STC No.<br />
<strong>EASA</strong>.IM.A.S.02745 and an oxygen system<br />
per <strong>EASA</strong> STC <strong>EASA</strong>.IM.A.S.02744 or other<br />
approved interior arrangement and oxugen<br />
10<strong>01</strong>6412 JET AVIATON ST. LOUIS, Inc. <strong>EASA</strong>.IM.A.S.02744 FAA STC ST00755WI BOMBARDIER CL-600-2B16 Installation of Passenger Oxygen System.<br />
system.<br />
This STC must be installed with Cabin interior<br />
arrangement per <strong>EASA</strong> STC No.<br />
<strong>EASA</strong>.IM.A.S.02745 and an emergency<br />
lighting per <strong>EASA</strong> STC. No. IM.A.S.02743 or<br />
other approved interior arrangement and<br />
emergency lighting system.<br />
10<strong>01</strong>6413 JET AVIATON ST. LOUIS, Inc. <strong>EASA</strong>.IM.A.S.02745 FAA STC ST00756WI BOMBARDIER CL-600-2B16 (6<strong>01</strong>- Cabin Interior Arrangement. This STC must be installed concurrent with an<br />
3A<br />
emergency lighting system per <strong>EASA</strong> STC No.<br />
BOMBARDIER CL-600-2B16 (6<strong>01</strong>-<br />
<strong>EASA</strong>.IM.A.S.02743 and an oxygen system<br />
3R<br />
per<strong>EASA</strong>.IM.A.S.02744 or other approved<br />
BOMBARDIER CL-600-2B16 (6<strong>04</strong>)<br />
emergency lighting and oxygen system.<br />
10<strong>01</strong>6414 JET AVIATON ST. LOUIS, Inc. <strong>EASA</strong>.IM.A.S.02746 FAA STC ST00812WI BOMBARDIER CL-600-2B16 (6<strong>01</strong>- Installation of the Allied Signal MK-V Enhanced Gama Support Services Modification No.<br />
03.06.2008<br />
3A<br />
Ground Proximity Warning System (EGPWS). GSSL-MIN-CL6<strong>04</strong>-226 (Including Gama<br />
BOMBARDIER CL-600-2B16 (6<strong>01</strong>-<br />
Support Services Flight Manual Change Sheet<br />
3R<br />
No. GSS-FMS-CL6<strong>04</strong>-226 <strong>EASA</strong> approval<br />
BOMBARDIER CL-600-2B16 (6<strong>04</strong>)<br />
number <strong>EASA</strong>.A.A.<strong>01</strong>831), or equivalent<br />
<strong>EASA</strong> approved modification, is a prerequisite<br />
for the <strong>EASA</strong> appro<br />
10<strong>04</strong>0724 JET AVIATON ST. LOUIS, Inc. FAA STC NO. ST02744CH-D BD-700-1A10 Installation of a Rockwell Collins Wireless Local None. Prior to installation of this modification it 24.07.2<strong>01</strong>2<br />
Area Network (WLAN).<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 />
10<strong>04</strong>2519 JET AVIATON ST. LOUIS, Inc. FAA STC SA02789CE MYSTERE FALCON MF 50 <strong>EASA</strong> validation of FAA originally approved<br />
STC SA02789CE "Installationof a Bendix/King<br />
CAS-81 TCAS System".<br />
Aeroplanes modified in accordance with this<br />
STC must be maintained inaccordance with<br />
Approved Instructions for Continued<br />
Airworthiness, JetAviation Report No. 13-<br />
027E054, Section O - Airworthiness<br />
Limitations,Revision NC dated June 03rd 2<strong>01</strong>1<br />
or later revi<br />
10<strong>01</strong>4336 JET AVIONICS AVIATION & MARINE <strong>EASA</strong>.A.S.<strong>01</strong>591 CESSNA 650 CITATION III BDI 0<strong>04</strong>-05 Updating to TCAS II & ELT system Applicable only if the STC No ST502CH of 16<br />
and installation SSFDR<br />
may 1996 was previously installed<br />
10<strong>01</strong>4349 JET AVIONICS AVIATION & MARINE <strong>EASA</strong>.A.S.<strong>01</strong>614 BEECH 58, BARON Imrpoving of avionics systems for updating FM FM Supplement Sandel SN-3400, dated<br />
immunity 8.33 kHz channelling, B-RNAV, Mode 09/07/2007.FM Supplement Sandel ST-3400,<br />
S Transponder, TAWS, Weather Radar, Traffic dated 09/07/2007.FM Supplement Garmin<br />
Advisory System, ELT and entertainment GTX 330, dated 09/07/2007.FM Supplement<br />
system.<br />
Garmin GNS 430, dated 09/07/2007.FM<br />
Supplement Garmin MX-20, dated<br />
09/07/2007.FM Supplement L3 Sky-49<br />
20.03.2008<br />
20.03.2008<br />
20.03.2008<br />
Prior to installation of this modification it 06.12.2<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 />
10<strong>01</strong>4674 JET AVIONICS AVIATION & MARINE <strong>EASA</strong>.A.S.02834 BOMBARDIER CL-215-6B11 Installation of Radar Altimeter AA-300 System N/A <strong>01</strong>.03.2007<br />
10<strong>01</strong>5<strong>04</strong>4 JET AVIONICS AVIATION & MARINE <strong>EASA</strong>.A.S.03360 CESSNA 500, CITATION BDI 0<strong>04</strong>-07 Installation of Mode S Transponder<br />
- Elementary Surveillance.<br />
10<strong>01</strong>5237 JET AVIONICS AVIATION & MARINE <strong>EASA</strong>.A.S.03664 CESSNA CITATION 5<strong>01</strong> Installation of Mode S Transponder. 1. 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 will<br />
introduce no adverse effect upon the<br />
airworthiness of the product.2.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 297/<strong>462</strong><br />
11.10.2005<br />
08.08.2007<br />
05.03.2008<br />
23.12.2008
Change language