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>5151 JET AVIATION FLUGZEUGWARTUNG <strong>EASA</strong>.A.S.03512 PILATUS PC-12<br />
Replacement of existing KX 165 COM / NAV, Limited to single GNS 480 installation per<br />
17.10.2008<br />
GmbH<br />
PILATUS PC-12/45<br />
KLN 90B GPS, and GTX 330D Mode S cockpit only.Prior to installation of this<br />
PILATUS PC-12/47<br />
Transponder installation by GNS480 COM / modification the installer must determine that<br />
NAV / GPS and GTX 33D Mode S<br />
the interrelationship between this<br />
Transponder installation.<br />
modification and any other previously installed<br />
modification will introduce no a<br />
10<strong>01</strong>5152 JET AVIATION FLUGZEUGWARTUNG <strong>EASA</strong>.A.S.03513 PILATUS PC-12<br />
Installation of AIRCELL SATCOM ST3100 1. Prior to installation of this modification the<br />
14.10.2008<br />
GmbH<br />
PILATUS PC-12/45<br />
installer must determine that the<br />
PILATUS PC-12/47<br />
interrelationship between this modificationand<br />
any other previously installed modification<br />
will introduce no adverse effect upon the<br />
airworthiness of the produc<br />
10<strong>01</strong>5161 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>5171 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>5190 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>5221 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>5222 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>5223 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>5224 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>5225 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>5231 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
<strong>EASA</strong>.A.S.03530 CESSNA 525<br />
CESSNA 525A<br />
<strong>EASA</strong>.A.S.03545 PILATUS PC-12<br />
PILATUS PC-12/45<br />
PILATUS PC-12/47<br />
<strong>EASA</strong>.A.S.03574 CESSNA 525<br />
CESSNA 525A<br />
Upgrade of existing Dual Honeywell MST 67A For variant 525 this change is limited to serial<br />
Mode-S XPDR Installation to EHS Capabilities numbers 525 0360 and subsequent<br />
Installation of Honeywell EGPWS MK VI by<br />
installing a Honeywell EGPWS MK-VI.<br />
Installation of GARMIN GPS 400 (w) or 500<br />
(w)<br />
1. For approved Software Versions refer to<br />
Airplane Flight Manual, Section II -<br />
Limitations2. Prior to installation of this<br />
modification the installer must determine that<br />
the interrelationship between this modification<br />
and any other previously instal<br />
<strong>EASA</strong>.A.S.03638 REV. 1 650 (CITATION III) Primus 880 WX & MFRD installationRemoved None Prior to installation of this modification it 23.02.2<strong>01</strong>2<br />
existing Weather Radar Equipment:- i.a.w<br />
must be determined thatthe<br />
Installation Instructions, Doc. No. OPM-<br />
interrelationship between this modification<br />
003New Installed Weather Radar Equipment:-<br />
and any other previouslyinstalled<br />
Primus 880 Weather Radar System-<br />
modification and/ or repair will introduce<br />
Honeywell Multi Function Display, P/N 80-52<strong>04</strong>-<br />
no adverse effectupon the airworthiness<br />
XX-Xi.a.w In<br />
of the product.<br />
<strong>EASA</strong>.A.S.03639 REV. 2 650 (CITATION III) MK VII EGPWS Installation.Removed existing<br />
Equipment:i.a.w. Installation Instructions, Doc.<br />
No. OPM-0<strong>04</strong>New installed EGPWS<br />
Equipment:- Honeywell MK-VII EGPWSi.a.w.<br />
Installation Instructions, Doc. No. OPM-<br />
0<strong>04</strong>Revision 1: By revising the interface<br />
between the<br />
<strong>EASA</strong>.A.S.03640 REV. 1 650 (CITATION III) RAAS activation on the Honeywell MK-VII<br />
EGPWSi.a.w. Installation Instructions, Doc. No.<br />
OPM-005 Revision 1 has been issued to reflect<br />
the transfer of STC.<br />
<strong>EASA</strong>.A.S.03641 REV. 1 650 (CITATION III) P-RNAV Compliance on the installed GNS-<br />
XLS FMS, i.a.w. InstallationInstructions, Doc.<br />
No. OPM-006 Revision 1 has been issued to<br />
reflect the transfer of STC.<br />
<strong>EASA</strong>.A.S.03642 REV. 1 650 (CITATION III) FA2100 CVR installationRemoved Equipment:-<br />
i.a.w. Installation Instructions, Doc. No. OPM-<br />
007New Installed Equipment:- FA2100 Cockpit<br />
Voice Recorder Systemi.a.w. Installation<br />
Instructions, Doc. No. OPM-007 Revision 1 has<br />
been issued to reflect the transfer<br />
<strong>EASA</strong>.A.S.03653 CESSNA CITATION C525 Installation of AIRCELL Iridium Dual Patch<br />
Satcom Antenna.<br />
07.07.2008<br />
13.10.2008<br />
28.<strong>04</strong>.2009<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 />
23.02.2<strong>01</strong>2<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 />
23.02.2<strong>01</strong>2<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 />
23.02.2<strong>01</strong>2<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 />
23.02.2<strong>01</strong>2<br />
1. Antenna Installation only.2. Prior to<br />
installation of this modification the installer must<br />
determine that the interrelationship between<br />
this modification and any other previously<br />
installed modification will introduce no adverse<br />
effect upon the air<br />
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12.05.2009
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