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>4377 RUAG AEROSPACE SERVICES GmbH <strong>EASA</strong>.A.S.<strong>01</strong>652 CESSNA 560 Installation of a Honeywell Solid-State Flight<br />
Data Recorder (SSFDR) with Teledyne<br />
Controls Mini Flight Data Acquisition Unit<br />
(MFDAU)<br />
20.<strong>01</strong>.2006<br />
10<strong>01</strong>4407 RUAG AEROSPACE SERVICES GmbH <strong>EASA</strong>.A.S.<strong>01</strong>702 CESSNA 550 CITATION II Honeywell EGPWS Mk VIII Certification Basis of the Change: FAR 25 as<br />
defined in TCDS A22CE;Rev. 58, additionally<br />
JAA Leaflet No. 12 (TAWS)<br />
24.<strong>04</strong>.2006<br />
10<strong>01</strong>4409 RUAG AEROSPACE SERVICES GmbH <strong>EASA</strong>.A.S.<strong>01</strong>705 REV. 1 CESSNA 650 Upgrade of two existing Mode S transponders, Aircraft Serial Numbers 650-70<strong>01</strong> through 650- Prior to installation of this modification it 29.10.2<strong>01</strong>0<br />
Rockwell CollinsTDR-94D byRockwell Collins 7119<br />
must be determined thatthe<br />
SB 5<strong>01</strong>.Replacement of Mode S Controller<br />
interrelationship between this modification<br />
CTL-92 by CTL-92E along withinstallation of<br />
and any other previouslyinstalled<br />
new wiring for Enhances SurveillanceRevision<br />
modification and/ or repair will introduce<br />
1 to include <strong>EASA</strong> AD 2009-<strong>01</strong>73, Rockwel<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong>4429 RUAG AEROSPACE SERVICES GmbH <strong>EASA</strong>.A.S.02475 CESSNA 550 CITATION II ACAS II 5CAS67A) with Dual Mode S XPDR<br />
MST-67A-EHS<br />
Certification Basis of the Change: FAR 25 as<br />
defined in TCDS A22CE; Rev. 58, additionally<br />
JAA Leaflet No. 8, Rev. 2 (ACAS II), JAA<br />
Leaflet No. 13, Rev. 1 (Mode-S ELS) and JAA<br />
NPA 20-12a (Mode-S EHS)<br />
10<strong>01</strong>4571 RUAG AEROSPACE SERVICES GmbH <strong>EASA</strong>.A.S.02675 Installation of Honeywell Solid-State Flight Data --<br />
Recorder (SSFDR) with Teledyne Controls Mini<br />
Flight Data Acquisition Unit (MFDAU)<br />
26.06.2006<br />
10<strong>01</strong>4599 RUAG AEROSPACE SERVICES GmbH <strong>EASA</strong>.A.S.02720 BOMBARDIER CL-600-1A11 (CL- Enhanced Ground Proximity Waning System-<br />
600<br />
EGPWS-MK VII or MKV enhancement with<br />
BOMBARDIER CL-600-2A12 (CL- RAAS<br />
6<strong>01</strong><br />
BOMBARDIER CL-600-2B16 (6<strong>01</strong>-<br />
3A<br />
BOMBARDIER CL-600-2B16 (6<strong>01</strong>-<br />
3R<br />
BOMBARDIER CL-600-2B16 (6<strong>04</strong>)<br />
10<strong>01</strong>4610 RUAG AEROSPACE SERVICES GmbH <strong>EASA</strong>.A.S.02737 CESSNA 525 Installation of KLN-90BModel: 525 S/N 00<strong>01</strong><br />
up to 0359<br />
10<strong>01</strong><strong>462</strong>3 RUAG AEROSPACE SERVICES GmbH <strong>EASA</strong>.A.S.02757 BOMBARDIER CL-600-1A11 (CL- Honeywell Primus II RCZ-833 () Integrated<br />
600<br />
BOMBARDIER CL-600-2A12 (CL-<br />
6<strong>01</strong><br />
BOMBARDIER CL-600-2B16 (CL-<br />
6<strong>01</strong><br />
Radio System – EHS.<br />
10<strong>01</strong><strong>462</strong>4 RUAG AEROSPACE SERVICES GmbH <strong>EASA</strong>.A.S.02758 BOMBARDIER CL-600-1A11 (CL- Upgrade Dual Honeywell FMS NZ-2000 /<br />
600<br />
BOMBARDIER CL-600-2A12 (CL-<br />
6<strong>01</strong><br />
BOMBARDIER CL-600-2B16 (CL-<br />
6<strong>01</strong><br />
PRNAV.<br />
S/N 525-00<strong>01</strong> up to 525-0359This STC is<br />
approved only for the product configuration as<br />
defined in the approved design data referred to<br />
in the paragraph "Description". Compatibility<br />
with other aircraft/engine configurations shall<br />
be determined by the install<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 />
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 />
10<strong>01</strong><strong>462</strong>5 RUAG AEROSPACE SERVICES GmbH <strong>EASA</strong>.A.S.02759 BOMBARDIER CL-600-1A11 (CL- Iridium Satcom ST3100. This STC is approved only for the product<br />
600<br />
configuration as defined in the approved design<br />
BOMBARDIER CL-600-2A12 (CL-<br />
data referred to in the paragraphs "Description"<br />
6<strong>01</strong><br />
and “Associated Technical Documentation”.<br />
BOMBARDIER CL-600-2B16 (6<strong>01</strong>-<br />
Compatibility with other aircraft/engine<br />
3A<br />
configurations shall be determined<br />
10<strong>01</strong>4645 RUAG AEROSPACE SERVICES GmbH <strong>EASA</strong>.A.S.02799 BOMBARDIER CL-600-2B16 (CL-<br />
6<strong>01</strong><br />
40Ah Battery with Charger. 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 />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 378/<strong>462</strong><br />
19.<strong>04</strong>.2006<br />
07.02.2007<br />
10.07.2006<br />
12.<strong>01</strong>.2007<br />
12.<strong>01</strong>.2007<br />
12.<strong>01</strong>.2007<br />
12.<strong>01</strong>.2007
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