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>0249 JET AVIATION AG, ZURICH AIRPORT<br />
REV. 1 B200, B200C, B200GT, B200CGT ADS-B-OUT ComplianceOut: Dual Collins TDR-none<br />
Collins Pro Line 21 system & dual FMS- 11.09.2<strong>01</strong>2<br />
BRA<br />
B300, B300C<br />
94D Transponder Mode S P/N 822-9210-<br />
3000 & dual GPS-4000<br />
008In: Dual Collins TDR-94D Transponder<br />
(EGNOScapable) are prerequisiteThe<br />
Mode S P/N 622-9210-409 & 1<br />
approval holder shall fulfil the obligations<br />
dualannunciator/switch ADS-B 1/ADS-B 2<br />
of Part 21, Paragraph21.A109.Prior to<br />
inhibit<br />
installation of this modification it must be<br />
determined thatthe interrelationsh<br />
10<strong>04</strong>0290 JET AVIATION AG, ZURICH AIRPORT<br />
BRA<br />
10<strong>04</strong>2873 JET AVIATION AG, ZURICH AIRPORT<br />
BRA<br />
10<strong>01</strong>3961 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>3983 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>4009 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>4<strong>01</strong>0 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>4<strong>04</strong>1 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>4108 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>4109 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>4110 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>4144 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>4145 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>4153 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>4271 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>4272 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>4288 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10<strong>01</strong>4289 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
B200, B200C, B200GT, B200CGT Mini Quick Access Recorder<br />
None The approval holder shall fulfil the 22.06.2<strong>01</strong>2<br />
B300, B300C<br />
(QAR)InstallationIn: Single or Dual Avionica<br />
obligations of Part 21,<br />
P/N 8<strong>04</strong>-1205 miniQAR Mk III<br />
Paragraph21.A109. Prior to installation of<br />
this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repai<br />
B200, B200C, B200GT, B200CGT BARO-VNAV Temp. Comp. Activation & RF S/N: same as <strong>EASA</strong> TCDS with Rockwell Prior to the installation of this modification 21.12.2<strong>01</strong>2<br />
B300, B300C<br />
Legs Authorization Activation of Temperature Collins Proline 21 Avionics<br />
it must be determinedthat the<br />
Compensation on already approved APV<br />
interrelationship between this modification<br />
BARO-VNAVsystem and RF Legs<br />
and any otherpreviously installed<br />
Authorization (This functionality can be used in<br />
modification and/or repair will introduce<br />
the initial andintermediate approach segments,<br />
noadverse effect upon the airworthiness<br />
the final ph<br />
of the product.<br />
<strong>EASA</strong>.A.S.00645 LEARJET 55 Installation of Honeywell ACAS II CAS 67A and 1. FAA TCDS A10CE plus JAA TGL No 8 and<br />
17.05.2005<br />
Mode S XPDR MST 67A<br />
JAA TGL No 13 apply2. This STC is approved<br />
only for the product configuration as defined in<br />
the approved design data referred to in the<br />
paragraph "Description". Compatibility with<br />
other aircraft/engine configurations<br />
<strong>EASA</strong>.A.S.<strong>01</strong><strong>01</strong>5 CESSNA 5<strong>01</strong>-551 Installation of a Honeywell KTA 870 and<br />
ART2000<br />
15.06.2005<br />
<strong>EASA</strong>.A.S.<strong>01</strong>052 CESSNA 525- 525A Installation of a Dual MST 67A Mode S This STC is approved only for the product<br />
13.06.2005<br />
Transponder System.<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
<strong>EASA</strong>.A.S.<strong>01</strong>053 525<br />
Installation of Dual Garmin GTX 330D Mode<br />
17.11.2005<br />
CESSNA 525A<br />
SAFM Supplement 20<strong>04</strong>-16-8 Revision A or<br />
later <strong>EASA</strong> approved RevisionMM Supplement<br />
2005-16-10 Revision A or later <strong>EASA</strong><br />
approved Revision<br />
<strong>EASA</strong>.A.S.<strong>01</strong>116 PA-42 SERIES Installation of Artex ELT 406. 23.06.2005<br />
<strong>EASA</strong>.A.S.<strong>01</strong>213 CESSNA 650 Installation of SATCOM Universal TT-3000 16.11.2005<br />
<strong>EASA</strong>.A.S.<strong>01</strong>214 CESSNA 650 Installation of Airshow Entertainer System Part 25 of the Federal Aviation Regulations<br />
effective February 1, 1965 as amended by<br />
Amendments 25-1 through 25-39; TGM JAA<br />
leafletNo. 17Weight and Balance Analysis,<br />
Report 2005-17-9, Rev. A<br />
13.03.2006<br />
<strong>EASA</strong>.A.S.<strong>01</strong>215 CESSNA 550-560-S550 Installation of ACAS II CAS 67A and Dual<br />
Mode - S Transponder RCZ-833<br />
23.09.2005<br />
<strong>EASA</strong>.A.S.<strong>01</strong>262 LEARJET 55 Installation of Secondary UNS 1F 23.06.2005<br />
<strong>EASA</strong>.A.S.<strong>01</strong>263 LEARJET 55 Installation of ELT 406 29.06.2005<br />
<strong>EASA</strong>.A.S.<strong>01</strong>274 GULFSTREAM ASTRA/SPX Upgrade of Universal UNS-1C to 1C+ 21.09.2005<br />
<strong>EASA</strong>.A.S.<strong>01</strong>5<strong>01</strong> REV. 1 525, 525A Installation of Honeywell KMH 880 or KMH-980 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 />
27.06.2<strong>01</strong>1<br />
<strong>EASA</strong>.A.S.<strong>01</strong>502 CESSNA 5<strong>01</strong><br />
CESSNA 551<br />
Installation of Honeywell RDS 84 WX System. 16.08.2005<br />
<strong>EASA</strong>.A.S.<strong>01</strong>529 BEECH 1900 Installation of Universal Flight Manager System<br />
UNS-1L<br />
25.<strong>01</strong>.2006<br />
<strong>EASA</strong>.A.S.<strong>01</strong>531 BEECH 200<br />
Installation of Universal Flight Management<br />
24.10.2006<br />
BEECH 200C<br />
System UNS-1L<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 292/<strong>462</strong>
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