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 />
10030074 HAWKER BEECHCRAFT<br />
FAA STC SA<strong>01</strong>566WI-D KING AIR B200 SERIES Installation of modified Rockwell Collins Flight Prior approved installation of a Rockwell Prior to installation of this modification it 19.05.2<strong>01</strong>0<br />
CORPORATION (HBC)<br />
Guidance Computers(FGC-3000 units) as a Collins Inc FGC-3000 FlightGuidance must be determined thatthe<br />
solution to eliminate nuisance pitch trim Computer Module (CPN 822-1108-031) is a interrelationship between this modification<br />
wheelmovement.<br />
prerequisite to thisSTC.<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>01</strong>4008 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.<strong>01</strong>051 REV. 1 HAWKER HS 125-700B Increase Maximum Zero Fuel Weight 22.02.2005<br />
10<strong>01</strong>4102 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.<strong>01</strong>206 BEECH 400A (HAWKER 400 XP) Certification for Steep Approaches 26.07.2005<br />
10<strong>01</strong>4103 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.<strong>01</strong>207 BAE 125 SERIES 800B Raytheon Aircraft Services Modification<br />
SC<strong>01</strong>35R. Runway Awareness & Advisory<br />
System (RAAS) to the MK VII EGPWS<br />
Computer<br />
10<strong>01</strong>41<strong>04</strong> HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.<strong>01</strong>208 HAWKER HS 125-700B Installation of a Collins AHS-3000A Attitude<br />
Heading Reference System.<br />
10<strong>01</strong>4105 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.<strong>01</strong>209 HAWKER HS 125-700B Installation of Traffic Alert & Collision<br />
Avoidance System (TCAS-4000), Mode S<br />
Elementary Surveillance (Flight ID) and<br />
Emergency Locator Transmitter (Artex C406-2)<br />
10<strong>01</strong>4157 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.<strong>01</strong>283 BAE 125 SERIES 800B Special Interior Refurbishement 28.<strong>04</strong>.2005<br />
10<strong>01</strong>4350 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.<strong>01</strong>615 BAE 125 -800 SERIES Steep Approch Capability 25.10.2005<br />
10<strong>01</strong>4466 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.02527 BAE 125 SERIES 800B To indroduce completion of the upgrade to the Applicable to Aircraft Serial 258208 only<br />
existing Terrain Awareness Warning System<br />
(TAWS) installation to include terrain display.<br />
02.05.2006<br />
10<strong>01</strong>4803 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.03006 REV. 1 HAWKER 850 XP Introduction of Steep Approach Capability. 03.07.2007<br />
10<strong>01</strong>5118 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.03467 HAWKER 800 XP To upgrade Dual Honeywell NZ-2000 FMS<br />
Computers from 5.2 to 6.0 software and<br />
provide P-RNAV approval.<br />
None. 06.10.2008<br />
10<strong>01</strong>5119 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.03468 HAWKER 1000 To introduce Dual Honeywell NZ-2000 FMS 1. As per AFM Supplement for Hawker<br />
25.09.2008<br />
Computers in lieu of NZ-920 FMS Computers 1000B (HS1.18) Supplement 3 issue 1;2.<br />
and add a second GPS GNSSU. The existing Prior to installation of this modification the<br />
Data Loader is replaced with Model DL-950. installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification wi<br />
10<strong>01</strong>5126 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.03476 REV. 1 HAWKER 750 Installation of Steep Approach Capability 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 />
05.05.2<strong>01</strong>1<br />
10<strong>01</strong>5127 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.03477 REV. 1 HAWKER 900 XP Installation of Steep Approach Capability 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 />
05.05.2<strong>01</strong>1<br />
10<strong>01</strong>5133 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.03486 HAWKER HS 125-700A To upgrade Dual UNS-1K FMS to Dual UASC<br />
UNS-1Lw in preparation for P-RNAV<br />
compliance.<br />
1. Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
10<strong>01</strong>5322 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.IM.A.S.00275 FAA STC ST00983CH BEECH 400A Installation of a Honeywell Enhanced Ground<br />
airworthiness of the product. The i<br />
1. AFM Supplement Elliott Aviation<br />
Proximity Warning System (EGPWS) Mark VIII Document No. FS2<strong>01</strong>8-571 rev.0 or later<br />
in accordance with Elliot Aviation Master Data <strong>EASA</strong> approved revisions.2. Instructions for<br />
List 2<strong>01</strong>8-571DL, Revision 4, dated 6 Continued Airworthiness Document No.<br />
November 2003 or later <strong>EASA</strong> approved CA2<strong>01</strong>8-571.3. This STC is approved only<br />
revisions.This STC is issued as result of the va for the product configuration as defined in the<br />
app<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 265/<strong>462</strong><br />
21.06.2005<br />
13.06.2005<br />
23.03.2005<br />
10.11.2008<br />
20.10.20<strong>04</strong>
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