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 />
10032246 HAWKER BEECHCRAFT<br />
FAA STC ST10598SC-D 4000 Installation of Flight Camera System None Prior to installation of this modification it 19.10.2<strong>01</strong>0<br />
CORPORATION<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 />
10035154 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10036742 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>04</strong>2768 HAWKER BEECHCRAFT<br />
CORPORATION<br />
10<strong>01</strong>5370 HAWKER BEECHCRAFT<br />
CORPORATION (HBC)<br />
10<strong>01</strong>5373 HAWKER BEECHCRAFT<br />
CORPORATION (HBC)<br />
10<strong>01</strong>5909 HAWKER BEECHCRAFT<br />
CORPORATION (HBC)<br />
10<strong>01</strong>5982 HAWKER BEECHCRAFT<br />
CORPORATION (HBC)<br />
10<strong>01</strong>6127 HAWKER BEECHCRAFT<br />
CORPORATION (HBC)<br />
10<strong>01</strong>6230 HAWKER BEECHCRAFT<br />
CORPORATION (HBC)<br />
10<strong>01</strong>6231 HAWKER BEECHCRAFT<br />
CORPORATION (HBC)<br />
10<strong>01</strong>6367 HAWKER BEECHCRAFT<br />
CORPORATION (HBC)<br />
10<strong>01</strong>6577 HAWKER BEECHCRAFT<br />
CORPORATION (HBC)<br />
REV. 1 FAA STC SA00526DE 390 (PREMIER I)<br />
390 (PREMIER IA)<br />
FAA STC SA02331LA B300 & B300C Installation and maintenance of Switches and<br />
wiring for anElectro-Optical/Infra-Red Lift and<br />
Turret System.<br />
Installation of an AirCell telephone system. Serial Number RB-73 OnlyHawker Beechcraft<br />
Ltd. Minor Modification SC0392A must be<br />
embodied.<br />
FAA STC SA00782WI-D <strong>EASA</strong> APPROVED MODEL LIST Modification of Collins VHF-22A/VHF-22B VHF<br />
COMM Receiver Transmitterwith CTL-22<br />
Control Pro Line II System Installation to a<br />
CollinsVHF-22C/VHF-22D VHF COMM<br />
Receiver Transmitter with CTL-22C Control<br />
8.33kHz Pro Line II System Installation.<br />
Prior to installation of this modification it 15.11.2<strong>01</strong>2<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 />
none This STC is part of an existing belly<br />
mounted Radar installation and mayonly<br />
be installed on aircraft previously installed<br />
with STC SA02253LA(<strong>EASA</strong> approval ref<br />
10027658)Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelations<br />
05.10.2<strong>01</strong>1<br />
A VHF-22C unit can be installed to replace<br />
either an existing VHF-22A orVHF-22B unit. A<br />
VHF-22D unit can only be installed to replace<br />
anexisting VHF-22B unit.<br />
<strong>EASA</strong>.IM.A.S.<strong>01</strong>009 FAA STC SA8356SW HAWKER 1000 Installation of Air Distribution System 1. This STC is approved only for the product<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>.IM.A.S.<strong>01</strong>026 SA8348SW HAWKER 1000 Installation of Honeywell SRZ-8000 Digital<br />
Integrated Flight Control System with low<br />
speed awareness cue in accordance with<br />
Arkansas Aerospace Inc. Drawing List 1000-<br />
008<br />
<strong>EASA</strong>.IM.A.S.02036 ST09250AC HAWKER 1000<br />
HAWKER 800<br />
HAWKER 800 XP<br />
HAWKER 850 XP<br />
<strong>EASA</strong>.IM.A.S.02134 REV. 3 FAA STC ST0<strong>04</strong>59NY HAWKER 750<br />
HAWKER 800<br />
HAWKER 800 XP<br />
HAWKER 850 XP<br />
HAWKER 900 XP<br />
Installation of a Logo Light on the lower surface<br />
of the Horizontal Stabiliser<br />
Installation of an Allied Signal (Garrett) GTCP<br />
36-150W gas turbine Auxiliary Power Unit<br />
(APU).<br />
<strong>EASA</strong>.IM.A.S.02321 FAA STC SA<strong>01</strong>417WI RAYTHEON A36 Replace pilot's altimeter with IS&S encoding<br />
altimeter.<br />
<strong>EASA</strong>.IM.A.S.02492 FAA STC SA0859WI BEECH 1900D Installation of EROS MAGIC (Mask and<br />
Goggles Integrated Concept) Quick Donning<br />
Masks.<br />
<strong>EASA</strong>.IM.A.S.02494 FAA STC SA0876WI BEECH 1900D Installation of an Allied Signal CAS 67A Traffic<br />
Alert and Collision Avoidance System (TCAS<br />
II)<br />
<strong>EASA</strong>.IM.A.S.02689 FAA STC SA<strong>01</strong>798SE BEECH 200<br />
BEECH 200C<br />
BEECH 200CT<br />
BEECH 300<br />
BEECH 300C<br />
Reduced Vertical Separation Minimum<br />
Qualification Document Group Aircraft<br />
Classification Hawker Beechcraft Models<br />
B200/B200C/B200GT/B200CGT/ B300/B300C<br />
(Super King Air)<br />
<strong>EASA</strong>.IM.A.S.02975 FAA STC ST02113LA BEECH 400A Rockwell Collins dual Attitude Heading<br />
Reference system (AHRS).<br />
This STC does not give:PRNAV<br />
approvalRVSM approvalCAT II approval<br />
Compliance with the following requirements, in<br />
addition to the requirements shown on the<br />
Type Certificate Data Sheet 3A20, has<br />
beenshown: 23.303, 23.305, 23.307, 23.321,<br />
23.341, 23.365, 23.6<strong>01</strong>, 23.609, 23.627<br />
effective February 1, 196523.611 as amended<br />
thr<br />
Cutter aviation Master Data List Document No.<br />
02A-2406-2<strong>01</strong>, Revision “B” dated December<br />
5, 2007 or later approved revisions.<br />
Prior to installation of this modification it 18.12.2<strong>01</strong>2<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> 264/<strong>462</strong><br />
11.02.2005<br />
<strong>01</strong>.02.2007<br />
21.09.2006<br />
16.06.2008<br />
26.02.2007<br />
17.07.2007<br />
17.07.2007<br />
18.<strong>04</strong>.2008<br />
12.09.2008
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