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>04</strong>0869 JET AVIATION FLUGZEUGWARTUNG<br />
CESSNA 560XL Installation of a Moving Map System. None. Prior to installation of this modification it 31.07.2<strong>01</strong>2<br />
GmbH<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>2792 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
525<br />
525A<br />
WX-950 Stormscope installation. 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 />
18.12.2<strong>01</strong>2<br />
10<strong>01</strong>4249 JET AVIATION GMBH <strong>EASA</strong>.A.S.<strong>01</strong>471 LEARJET 55<br />
LEARJET 55C<br />
Installation of Flight Data Recorder F1000 <strong>01</strong>.08.2005<br />
10<strong>01</strong>4291 JET AVIATION GMBH <strong>EASA</strong>.A.S.<strong>01</strong>533 IAI ASTRA SPX Installation of Universal Unilink UL-6<strong>01</strong> Certification Basis:FAR Part 25, TGL Leaflet<br />
No. 15 and 16<br />
19.<strong>04</strong>.2006<br />
10<strong>01</strong>4353 JET AVIATION GMBH <strong>EASA</strong>.A.S.<strong>01</strong>618 CESSNA 560 (CITATION V) Installation of Honeywell EGPWS Mark VIII 02.11.2005<br />
10<strong>01</strong>4393 JET AVIATION GMBH <strong>EASA</strong>.A.S.<strong>01</strong>683 BEECH 1900<br />
Installation of Universal UNS-1K+ Instructions for Continued Airworthiness, Doc.<br />
31.08.2006<br />
BEECH 1900C, AIRLINER<br />
BEECH 1900D<br />
No. 2005-35-10 Rev. B<br />
10<strong>01</strong>4394 JET AVIATION GMBH <strong>EASA</strong>.A.S.<strong>01</strong>684 BEECH 1900<br />
BEECH 1900D<br />
Installation of Universal TAWS and MFD 640 28.08.2006<br />
10<strong>01</strong>44<strong>01</strong> JET AVIATION GMBH <strong>EASA</strong>.A.S.<strong>01</strong>696 LEARJET 31 Installation of Bluesky C-1000 SATCOM -- 03.08.2006<br />
10039198 JET AVIATION ST. LOUIS, INC. FAA STC ST<strong>01</strong>065WI-D BD-700-1A10/11 Installation of a Supplemental Crew Oxygen None The supplemental crew oxygen masks 17.<strong>04</strong>.2<strong>01</strong>2<br />
System<br />
are not intended to be used in<br />
anemergency situation as a direct<br />
replacement for the type-certificatedcrew<br />
oxygen mask with integral smoke<br />
goggles.Prior to installation of this<br />
modification it must be determined<br />
thatthe i<br />
10039199 JET AVIATION ST. LOUIS, INC. FAA STC ST02658CH-D BD-700-1A10 Installation of a Passenger Address System 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 />
17.<strong>04</strong>.2<strong>01</strong>2<br />
10<strong>04</strong>0607 JET AVIATION ST. LOUIS, INC. FAA STC ST<strong>01</strong>376WI-D BD-700-1A10 Installation of a Cabin Interior Arrangement,<br />
Passenger Oxygen Systemand Emergency<br />
Lighting<br />
Restricted to ASN 9267 (Configuration 13) 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 />
13.07.2<strong>01</strong>2<br />
10<strong>04</strong>1674 JET AVIATION ST. LOUIS, INC. FAA STC ST02868CH-D CL-600-2B16 (CL-6<strong>04</strong> VARIANT) Installation of Drain Mast 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 />
05.10.2<strong>01</strong>2<br />
10<strong>01</strong>5882 JET AVIATON ST. LOUIS, Inc. <strong>EASA</strong>.IM.A.S.02000 FAA STC ST<strong>01</strong>319WI-D BOMBARDIER CL-600-2B16 (CL-<br />
6<strong>04</strong><br />
Addition of Runway Awareness & Advisory<br />
System-RAAS to Honeywell MK-V & MK-VII<br />
Enhanced Ground Proximity Warning System-<br />
EGPWS<br />
10<strong>01</strong>5883 JET AVIATON ST. LOUIS, Inc. <strong>EASA</strong>.IM.A.S.020<strong>01</strong> FAA STC ST<strong>01</strong>318WI-D BOMBARDIER CL-600-2B16 Software upgrade to 218-218 of the Honeywell<br />
MK-V Enhanced Ground Proximity Warning<br />
System to support Runway Awareness &<br />
Advisory System (RAAS).<br />
10<strong>01</strong>6260 JET AVIATON ST. LOUIS, Inc. <strong>EASA</strong>.IM.A.S.02539 FAA STC ST02543CH-D BOMBARDIER CL-600-2B16 Installation of a Cabin Interior Arrangement,<br />
Passenger Oxygen System, and Emergency<br />
Lighting.<br />
1. Prerequisite: MK V or MK VII EGPWS<br />
must be installed at Software Level - 218-218<br />
or greater.2. Prior to installation of this<br />
modification the installer must determine that<br />
the interrelationship between this modification<br />
and any other previously in<br />
Prerequisite: MK V EGPWS must be installed<br />
per Bombardier Service Bulletin 6<strong>04</strong>-34-020<br />
or 6<strong>04</strong>-34-025.<br />
06.09.2007<br />
06.09.2007<br />
Restricted to ASN 57<strong>01</strong>. 03.06.2008<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 296/<strong>462</strong>
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