04/01/2013 Page 1/462 - EASA

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EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015332 HAWKER BEECHCRAFT Ltd. EASA.IM.A.S.00350 FAA STC SA00421WI BEECH 1900C, AIRLINER Defines an all cargo interior using web nets. 1. The Airplane Flight Manual Supplement 03.12.2004 The all cargo interior is defined by the top No RAS 114-590021 is required equipment drawing of Raytheon Aircraft Services No114- when this STC is installed.2. Compatibility of 0100, no change, dated April 17, 1996, with an this design change with previously approved "FAA Approved" stamp of April 17, 1996 or modifications must be determined by the later FAA-approved revision. installer.3. This STC is issued as 10032984 HAWKER BEECHCRAFT Ltd. B200, B300 Installation of Thrane & Thrane Aviator 200/300 Inmarsat Satcom withWi-Fi capability on Beechcraft King Air B200/B300 10037296 HAWKER BEECHCRAFT Ltd. HAWKER 750, 800XP HAWKER 850XP, 900XP 10038135 HAWKER BEECHCRAFT Ltd. HAWKER 750, 800XP, 850XP HAWKER 900XP 10038252 HAWKER BEECHCRAFT Ltd. EASA.A.S.03559 HAWKER 750 HAWKER 800 XP HAWKER 850 XP HAWKER 900 XP To introduce interior and electrical provisions for Medevac stretcherrole change capability.This Change instructs the interior and electrical changes to theaircraft. Stretcher and medical equipment installation will be certifiedby the appropriate vendor. To introduce Dual L3 Electronic Flight Bags (EFB) units in the cockpitwith power supplies. To introduce a new forward cabin door with associated placards. 10038800 HAWKER BEECHCRAFT Ltd. KING AIR B300CER To introduce increased maximum landing weight to 16,500lbs for the KingAir B300CER. This modification is only applicable to aircraft equipped with theCollins Proline 21 avionics package. Refer to aircraft defined in HawkerBeechcraft major change SC0353A. Prior to installation of this modification it 13.12.2010 must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. None. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 17.11.2011 All EFB functionality and software approval will be the responsibilityof the aircraft operator. Unless approved otherwise by all RequiredManuals (Hard Copy) must still be carried in the aircraft. Prior to installation of this modification it 23.01.2012 must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. None. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 01.02.2012 None. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 14.03.2012 10040927 HAWKER BEECHCRAFT Ltd. C90GTI To introduce L3 Electronic Standby Instrument None System (ESIS) in lieu ofexisting Meggitt Mk II Secondary Flight Display (SFD) System.The existing Meggitt Mk II SFD (part number 39221- 01-01) is removed andreplaced with L3 GH- 3900.2 ESIS (Part number 9200-3450 None 03.08.2012 10041476 HAWKER BEECHCRAFT Ltd. REV. 1 B200 B200GT 10016247 HAWKER BEECHCRAFT SERVICES EASA.IM.A.S.02524 FAA STC ST02619AT BEECH 400 BEECH 400A Introduce Rockwell Collins TCAS 4000, Traffic Collision Avoidance System(TCAS) II System. Installation of a Battery Low Voltage Warning / Shutoff System on Raytheon Aircraft 400 and 400A. 10016248 HAWKER BEECHCRAFT SERVICES EASA.IM.A.S.02525 FAA STC SA03292AT BEECH 390 Modification to install an Auxiliary Gound Heating System. STC does not provide compliance with Commission Regulation (EC)1332/2011 as regards to ACAS II equipment. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.The installa Prior to installation of this modification it 05.10.2012 must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 04/01/2013 Page 266/462 28.08.2007 18.10.2007
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016250 HAWKER BEECHCRAFT SERVICES EASA.IM.A.S.02527 FAA STC NUMBER ST01441WI HAWKER 800 Hawker Beechcraft Corporation Installation of 10.10.2007 HAWKER 800 XP upper and lower LED beacons, wingtip LED navigation lights and wingtip strobe lights. 10016269 HAWKER BEECHCRAFT SERVICES EASA.IM.A.S.02552 FAA STC ST03405AT BEECH 400 BEECH 400A Replacement of a Standby Altimeter installation in the Raytheon (Beech) models 400, 400A aircraft.This STC is a duplicate of STC ST03379AT, EASA.IM.A.S.02353 10016281 HAWKER BEECHCRAFT SERVICES EASA.IM.A.S.02574 REV. 1 FAA STC ST01369AT BEECH 300 Installation of a 70% Ground Idle Stop Dropout System.Installs cams and switches on the existing aircraft’s power lever system to allow the propeller system to transition from Ground Idle to Flight Idle when both Power levers are advances above 70 %. This 10016352 HAWKER BEECHCRAFT SERVICES EASA.IM.A.S.02672 FAA STC SA01414WI HAWKER BEECHCRAFT G58 Modification to install a Honeywell KR 87 None 27.05.2009 (BARON) Automatic Direction Finder (ADF) System and the Honeywell KA-44B Antenna interfaced with the previously installed Garmin 1000 Avionics System. 10016353 HAWKER BEECHCRAFT SERVICES EASA.IM.A.S.02673 FAA STC SA01455WI HAWKER BEECHCRAFT G36 Modification to install a Honeywell KR 87 None 27.05.2009 (BONANZA Automatic Direction Finder (ADF) System and the Honeywell KA-44B Antenna interfaced with the previously installed Garmin 1000 Avionics System. 10016550 HAWKER BEECHCRAFT SERVICES EASA.IM.A.S.02930 FAA STC ST01191WI BEECH 1900D Installation of Cargo Conversion Modifications. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. 03.09.2008 10016551 HAWKER BEECHCRAFT SERVICES EASA.IM.A.S.02931 REV. 1 FAA STC ST00589LA HAWKER 1000 Installation of AlliedSignal Enhanced Gound The installation should not be incorporated in 04.07.2008 Proximity Warning System (EGPWS). any aircraft unless it is determined that the relationship between this installationand any previously approved configuration will not introduce any adverse effect upon the Airworthiness of the Aircraft. The a 10026878 HAWKER BEECHCRAFT SERVICES P- FAA STC SA01525WI BEECH 200, 200C, 200CT, 200T Installation of AirLock Secure Entry Door Lock None 1) Prior to installation of this modification 13.08.2009 EASA.IM.A.S.03243 BEECH 300, 300LW, B200, System in place oforiginal equipment locks for the installer mustdetermine that the B200C, the main cabin door, nose avionics doors,and interrelationship between this modification BEECH B200CT, B200T, B300, aft equipment door. and anyother previously installed BEECH B300C, modification will introduce no adverse HAWKER BEECHCRAFT effectupon the airworthiness of the B200GT, B200 product. 2) The inst 10036781 HAWKER BEECHCRAFT SERVICES FAA STC SA00857WI BEECH 1900D Installation of Universal Avionics System Corp UNS-1K Flight ManagementSystem. 10036782 HAWKER BEECHCRAFT SERVICES FAA STC SA00878WI BEECH 1900D Installation of a forward double or triple club executive style interiorconfiguration. 10016046 HAWKER BEECHCRAFT SERVICES, Inc. EASA.IM.A.S.02217 REV. 2 FAA STC SA10478SC BEECH B200, B200C BEECH B200GT, B200CGT BEECH B300, B300C Installation of Digital Flight Data Recorder System 04.09.2007 19.10.2007 None. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 06.10.2011 None. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 06.10.2011 None Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 16.06.2009 04/01/2013 Page 267/462
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04/01/2013 Page 1/462 - EASA

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