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 />
10<strong>01</strong>5920 LEARJET INC. <strong>EASA</strong>.IM.A.S.02053 FAA STC SA8109NM-D BOMBARDIER CL-600-2B16 Installation of Honeywell Enhanced Ground<br />
Proximity Warning System with Runway<br />
Awareness & Advisory System (RAAS)<br />
05.07.2007<br />
10<strong>01</strong>5948 LEARJET INC. <strong>EASA</strong>.IM.A.S.02090 REV. 1 FAA STC SA8129NM-D BOMBARDIER CL-600-2B16 (6<strong>04</strong>) Installation of Ultra Electronics Active Noise &<br />
Vibration Control system<br />
-- 14.09.2007<br />
10<strong>01</strong>6066 LEARJET INC. <strong>EASA</strong>.IM.A.S.02245 FAA STC ST<strong>01</strong>731LA-D LEARJET 45 Installation of Honeywell Integrated<br />
1. Incorporation of ECR 7598 and Honeywell<br />
14.03.2007<br />
Communication Unit / Enhanced Surveillance Service Bulletins 7517400-23-6008, 7510700-<br />
Upgrade (-1 Configuration).<br />
23-6<strong>04</strong>4 and 7510700-23-6<strong>04</strong>6 is a prior or<br />
concurrent requirement to this installation.2.<br />
This STC is approved only for the product<br />
configuration as defined in the approve<br />
10<strong>01</strong>6070 LEARJET INC. <strong>EASA</strong>.IM.A.S.02251 FAA STC SA8178NM-D BOMBARDIER BD-700-1A10 Installation of an Artex ELT/NAV Interface<br />
SystemValidation of the FAA STC SA8178NM-<br />
D<br />
10<strong>01</strong>6106 LEARJET INC. <strong>EASA</strong>.IM.A.S.02296 FAA ST00222BO BOMBARDIER CL-600-2B16 Installation of enhanced surveillance<br />
modification to Dual Collins TDR-94/94D<br />
transponder system.<br />
10<strong>01</strong>6108 LEARJET INC. <strong>EASA</strong>.IM.A.S.02298 REV. 1 FAA STC ST<strong>01</strong>732LA-D BOMBARDIER BD-700-1A10 Installation of a Rockwell Collins Integrated<br />
Flight Information System (IFIS-5000).<br />
10<strong>01</strong>6140 LEARJET INC. <strong>EASA</strong>.IM.A.S.02336 REV. 3 FAA STC SA8164NM-D BD-700-1A10 Installation of a Complete Custom Aircraft<br />
Interior - ASN 9<strong>01</strong>6, 9020,9054, 9098, 9106<br />
10<strong>01</strong>6148 LEARJET INC. <strong>EASA</strong>.IM.A.S.02349 FAA STC SA8133NM-D BOMBARDIER CL-600-2B16 (CL-<br />
6<strong>04</strong><br />
Replacement of a Collins TCAS II bottom<br />
OMNI-Directional Antenna (Sensor Systems)<br />
10<strong>01</strong>6160 LEARJET Inc. <strong>EASA</strong>.IM.A.S.02382 FAA STC ST<strong>01</strong>082WI-D LEARJET 60 Universal UNS-1E/C+ Flight Management<br />
SystemFAA STC ST<strong>01</strong>082WI-D<br />
10<strong>01</strong>6163 LEARJET INC. <strong>EASA</strong>.IM.A.S.02390 FAA STC SA8100NM-D BOMBARDIER CL-600-2B16 Installation of an Axle Jack Storage Box<br />
Installation<br />
10<strong>01</strong>6164 LEARJET INC. <strong>EASA</strong>.IM.A.S.02391 FAA STC SA8097NM-D BOMBARDIER CL-600-2B16 Installation of an Engine Cover Storage - Aft<br />
Equipment<br />
10<strong>01</strong>6165 LEARJET INC. <strong>EASA</strong>.IM.A.S.02392 FAA STC SA6003NM-D BOMBARDIER CL-600-2A12 (CL- Interior Installation/Modification in accordance<br />
6<strong>01</strong><br />
with DAS approved Learjet Master document<br />
BOMBARDIER CL-600-2B16 list No. CA-1000TUC, Rev "N" dated January<br />
12, 1995 or later approved revision<br />
10<strong>01</strong>6226 LEARJET INC. <strong>EASA</strong>.IM.A.S.02478 FAA STC SA81<strong>01</strong>NM-D BOMBARDIER CL-600-2B16 (CL-<br />
6<strong>04</strong><br />
FAA STC SA81<strong>01</strong>NM-D, NAV Lights<br />
RelocationThis STC supersedes LBA TA<strong>01</strong>36.<br />
Installation of emhanced surveillance<br />
modificationper this STC requires that a<br />
previously <strong>EASA</strong> approved dual installation of<br />
Collins p/n 622-9352-007 (TDR-94) or 622-<br />
9210-007 (TDR-94D) or later version has been<br />
installed in the aircraft.<br />
Restricted to ASN 9<strong>01</strong>6, 9020, 9054, 9098,<br />
9106.The following STC's are a concurrent<br />
requirement with this STC:-<strong>EASA</strong> STC<br />
10<strong>01</strong>6535 (FAA STC ST00941LA) - Floor<br />
Proximity EmergencyEscape Path Marking<br />
System is applicable to all aircraft serial<br />
numbersapproved<br />
This STC is approved only for the product<br />
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 />
1. This approval only applies to the -0<strong>04</strong>, -<br />
005, -006, and -<strong>01</strong>0 configurations of the<br />
Universal UNS-1C+ Flight Management<br />
System2. See also FAA STC ST<strong>01</strong>082WI-<br />
D3. Prior to installation of this modification<br />
the installer must determine that the inte<br />
The proper interrelationship between this<br />
installation and any previously approved<br />
configuration has to be assured.<br />
10<strong>01</strong>6356 LEARJET INC. <strong>EASA</strong>.IM.A.S.02678 FAA SA8191NM-D BOMBARDIER CL-600-2B16 (6<strong>04</strong>) Installation of a Safe Flight Enhanced The -3 configuration requires the installation of<br />
Autopower System.<br />
FAA STC SA8191NM-D -2 configuration.<br />
10<strong>01</strong>6387 LEARJET INC. <strong>EASA</strong>.IM.A.S.02715 FAA STC ST<strong>01</strong>737LA-D BOMBARDIER BD-700-1A10 Installation of Honeywell / EMS HD-710 High- The installation of an <strong>EASA</strong> approved Router/<br />
BOMBARDIER BD-700-1A11 Speed Data Satcom System.<br />
LAN System is a prerequisite/ concurrent<br />
requirement to the installation of the -1<br />
Configuration.<br />
10<strong>01</strong>64<strong>01</strong> LEARJET INC. <strong>EASA</strong>.IM.A.S.02730 FAA ST0<strong>01</strong>63BO BOMBARDIER BD-700-1A10 Installation of a main entry door rain deflector<br />
BOMBARDIER BD-700-1A11 channel.<br />
10<strong>01</strong>6445 LEARJET INC. <strong>EASA</strong>.IM.A.S.02791 FAA STC ST02023 LA-D BOMBARDIER CL-600-2B16 Installation of a Mid-Cabin Interior Modification. A prior or concurrent requirement for the<br />
installation of the -1 Configuration is the<br />
incorporation of <strong>EASA</strong> STC No.<br />
<strong>EASA</strong>.IM.A.S.02392 for the<br />
interior/Modification Installation.<br />
21.02.2007<br />
31.05.2007<br />
<strong>04</strong>.12.2007<br />
Prior to installation of this modification it 10.08.2<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 />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 308/<strong>462</strong><br />
07.05.2007<br />
08.08.2007<br />
31.05.2007<br />
31.05.2007<br />
03.08.2007<br />
31.05.2007<br />
21.08.2007<br />
07.<strong>04</strong>.2008<br />
08.05.2008<br />
07.05.2008
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