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>5332 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.IM.A.S.00350 FAA STC SA0<strong>04</strong>21WI BEECH 1900C, AIRLINER Defines an all cargo interior using web nets. 1. The Airplane Flight Manual Supplement<br />
03.12.20<strong>04</strong><br />
The all cargo interior is defined by the top No RAS 114-590021 is required equipment<br />
drawing of Raytheon Aircraft Services No114- when this STC is installed.2. Compatibility of<br />
<strong>01</strong>00, no change, dated April 17, 1996, with an this design change with previously approved<br />
"FAA Approved" stamp of April 17, 1996 or modifications must be determined by the<br />
later FAA-approved revision.<br />
installer.3. This STC is issued as<br />
10032984 HAWKER BEECHCRAFT Ltd. B200, B300 Installation of Thrane & Thrane Aviator 200/300<br />
Inmarsat Satcom withWi-Fi capability on<br />
Beechcraft King Air B200/B300<br />
10037296 HAWKER BEECHCRAFT Ltd. HAWKER 750, 800XP<br />
HAWKER 850XP, 900XP<br />
10038135 HAWKER BEECHCRAFT Ltd. HAWKER 750, 800XP, 850XP<br />
HAWKER 900XP<br />
10038252 HAWKER BEECHCRAFT Ltd. <strong>EASA</strong>.A.S.03559 HAWKER 750<br />
HAWKER 800 XP<br />
HAWKER 850 XP<br />
HAWKER 900 XP<br />
To introduce interior and electrical provisions<br />
for Medevac stretcherrole change<br />
capability.This Change instructs the interior and<br />
electrical changes to theaircraft. Stretcher and<br />
medical equipment installation will be<br />
certifiedby the appropriate vendor.<br />
To introduce Dual L3 Electronic Flight Bags<br />
(EFB) units in the cockpitwith power supplies.<br />
To introduce a new forward cabin door with<br />
associated placards.<br />
10038800 HAWKER BEECHCRAFT Ltd. KING AIR B300CER To introduce increased maximum landing<br />
weight to 16,500lbs for the KingAir B300CER.<br />
This modification is only applicable to aircraft<br />
equipped with theCollins Proline 21 avionics<br />
package. Refer to aircraft defined in<br />
HawkerBeechcraft major change SC0353A.<br />
Prior to installation of this modification it 13.12.2<strong>01</strong>0<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. 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 />
17.11.2<strong>01</strong>1<br />
All EFB functionality and software approval will<br />
be the responsibilityof the aircraft operator.<br />
Unless approved otherwise by all<br />
RequiredManuals (Hard Copy) must still be<br />
carried in the aircraft.<br />
Prior to installation of this modification it 23.<strong>01</strong>.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. 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 />
<strong>01</strong>.02.2<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 />
14.03.2<strong>01</strong>2<br />
10<strong>04</strong>0927 HAWKER BEECHCRAFT Ltd. C90GTI To introduce L3 Electronic Standby Instrument None<br />
System (ESIS) in lieu ofexisting Meggitt Mk II<br />
Secondary Flight Display (SFD) System.The<br />
existing Meggitt Mk II SFD (part number 39221-<br />
<strong>01</strong>-<strong>01</strong>) is removed andreplaced with L3 GH-<br />
3900.2 ESIS (Part number 9200-3450<br />
None 03.08.2<strong>01</strong>2<br />
10<strong>04</strong>1476 HAWKER BEECHCRAFT Ltd. REV. 1 B200<br />
B200GT<br />
10<strong>01</strong>6247 HAWKER BEECHCRAFT SERVICES <strong>EASA</strong>.IM.A.S.02524 FAA STC ST02619AT BEECH 400<br />
BEECH 400A<br />
Introduce Rockwell Collins TCAS 4000, Traffic<br />
Collision Avoidance System(TCAS) II System.<br />
Installation of a Battery Low Voltage Warning /<br />
Shutoff System on Raytheon Aircraft 400 and<br />
400A.<br />
10<strong>01</strong>6248 HAWKER BEECHCRAFT SERVICES <strong>EASA</strong>.IM.A.S.02525 FAA STC SA03292AT BEECH 390 Modification to install an Auxiliary Gound<br />
Heating System.<br />
STC does not provide compliance with<br />
Commission Regulation (EC)1332/2<strong>01</strong>1 as<br />
regards to ACAS II equipment.<br />
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 />
airworthiness of the product.The installa<br />
Prior to installation of this modification it 05.10.2<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> 266/<strong>462</strong><br />
28.08.2007<br />
18.10.2007
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