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 />
10037809 AIR ALLIANCE GmbH 337, A, B, C, D, E, F, G, H Replacement of installed Slaved Gyro system None Prior to installation of this modification it 22.12.2<strong>01</strong>1<br />
M337B, P337H<br />
by ASPEN EFD 1000 PROPrimary Flight<br />
must be determined thatthe<br />
T337B, C, D, E, F, G, H, H-SP Display<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 />
10038951 AIR ALLIANCE GmbH 208, 208B Installation of Honeywell KFD840 Primary<br />
Flight Display.<br />
10<strong>04</strong>2509 AIR ALLIANCE GmbH PA-44-180<br />
PA-44-180T<br />
Replacement of installed Gyro system by<br />
ASPEN EFD 1000 Pro PrimaryFlight Display.<br />
10<strong>01</strong>4268 AIR ALPHA A/S <strong>EASA</strong>.A.S.<strong>01</strong>497 REV 1 BAE HS 748 2A & 2B Installation of a Honeywell EGPWS MK6<br />
system.<br />
10028446 AIR ALPHA A/S P-<strong>EASA</strong>.A.S.03971 BEECH 200, BEECH B200 Installation of Blue Sky Network (BSN)<br />
BEECH B200C, BEECH<br />
D1000(A) Iridium SatelliteCommunication and<br />
B200CGT<br />
BEECH B200GT<br />
Tracking<br />
1003<strong>04</strong>56 AIR ALPHA A/S B200, B200GT Air Alpha STC Definition Document EO-B200-<br />
25-145. Flight InspectionSystem Interface<br />
Installation King Air 200 Series.<br />
1003<strong>04</strong>70 AIR ALPHA A/S P-<strong>EASA</strong>.A.S.03969 200, B200 AND B200GT Provision for Flight Inspection use of MLS<br />
navigation input<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 />
26.03.2<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 />
05.12.2<strong>01</strong>2<br />
1. Existing GPS antenna shall be used with<br />
15.08.2005<br />
coach splitter.<br />
None 1. Prior to installation of this modification 12.<strong>01</strong>.2<strong>01</strong>0<br />
the installer mustdetermine that the<br />
interrelationship between this modification<br />
and anyother previously installed<br />
modification will introduce no adverse<br />
effectupon the airworthiness of the<br />
product.2. The insta<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 />
16.06.2<strong>01</strong>0<br />
MINIMUM FLIGHT CREW: FIS MLS<br />
Navigation may only be used with two (2)flight<br />
crew members seated in the cockpitMLS/FIS<br />
NOT FOR PRIMARY NAVIGATION. FLIGHT<br />
INSPECTION GUIDANCE ONLY<br />
STC Holder approval required prior to<br />
application by any other partyPrior to<br />
installation of this modification it must be<br />
determined thatthe interrelationship<br />
between this modification and any other<br />
previouslyinstalled modification and/ or<br />
1003<strong>04</strong>71 AIR ALPHA A/S P-<strong>EASA</strong>.A.S.03942 B200 AND B200GT MD-124F Direction Finder Antenna Installation None<br />
repair will intr<br />
STC Holder approval required prior to<br />
application by any other partyPrior to<br />
installation of this modification it must be<br />
determined thatthe interrelationship<br />
between this modification and any other<br />
previouslyinstalled modification and/ or<br />
repair will intr<br />
17.06.2<strong>01</strong>0<br />
10<strong>01</strong>4578 AIR ALPHA MAINTENANCE A/S <strong>EASA</strong>.A.S.02683 BEECH B200 Installation of Trane & Trane Aero-I satcom<br />
equipment in accordance with danish STC<br />
03/9Note: This STC superseads SLV STC No.<br />
3/99<br />
13.07.2006<br />
10<strong>01</strong>4579 AIR ALPHA MAINTENANCE A/S <strong>EASA</strong>.A.S.02684 BEECH B200 Installation of Trane & Trane Aero-M satcom<br />
equipment in accordance with danish STC<br />
<strong>04</strong>/99Note: This STC superseads SLV STC<br />
No. <strong>04</strong>/99<br />
13.07.2006<br />
10<strong>01</strong>4580 AIR ALPHA MAINTENANCE A/S <strong>EASA</strong>.A.S.02685 BEECH B200 Installation of Trane & Trane Aero-C satcom<br />
equipment in accordance with danish STC<br />
05/99.Note: This STC superseads SLV STC<br />
No. 05/99<br />
13.07.2006<br />
10<strong>01</strong>4581 AIR ALPHA MAINTENANCE A/S <strong>EASA</strong>.A.S.02686 BEECH B200 Installation of Trane & Trane Aero-I, Aero-M<br />
and Aero-C satcom equipment in accordance<br />
with danish STC 29/99.Note: This STC<br />
superseads SLV STC No. 29/99.<br />
13.07.2006<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 47/<strong>462</strong><br />
17.06.2<strong>01</strong>0
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