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 10015871 HAWKER BEECHCRAFT EASA.IM.A.S.01986 REV. 2 FAA STC SA8063SW BAE 125 SERIES 800A Installation of Cabin Headliner/Window Panel 20.05.2008 CORPORATION HAWKER 800 HAWKER 800 XP HAWKER 850 XP HAWKER 900 XP Brackets. 10015872 HAWKER BEECHCRAFT EASA.IM.A.S.01987 REV. 2 FAA STC SA8062SW BAE 125 SERIES 800A Installation of a Therapeutic Oxygen System. 20.05.2008 CORPORATION HAWKER 800 HAWKER 800 XP HAWKER 850 XP HAWKER 900 XP 10015873 HAWKER BEECHCRAFT EASA.IM.A.S.01988 REV. 2 FAA STC SA7972SW-D HAWKER 800 XP Installation of Airborne Flight Information 20.05.2008 CORPORATION HAWKER 850 XP HAWKER 900 XP System (AFIS). 10015874 HAWKER BEECHCRAFT EASA.IM.A.S.01989 REV. 2 FAA STC SA7944SW BAE 125 SERIES 800A Installation of a Cabin Oxygen System. 20.05.2008 CORPORATION HAWKER 800 HAWKER 800 XP HAWKER 850 XP HAWKER 900 XP 10015875 HAWKER BEECHCRAFT EASA.IM.A.S.01990 REV. 1 FAA STC SA3810SW-D BAE 125 SERIES 800A Installation of Precise Pulselite Control Unit 1. 103 Installation is for Models Hawker 19.11.2007 CORPORATION HAWKER 800 800XP, Hawker 850XP and Hawker 900XP.2. HAWKER 800 XP All installations except -103 is for Models BAe. HAWKER 850 XP 125 Series 800A, Hawker 800; Hawker 800XP 10015876 HAWKER BEECHCRAFT CORPORATION 10015877 HAWKER BEECHCRAFT CORPORATION 10015878 HAWKER BEECHCRAFT CORPORATION 10015879 HAWKER BEECHCRAFT CORPORATION 10015880 HAWKER BEECHCRAFT CORPORATION 10015881 HAWKER BEECHCRAFT CORPORATION 10016024 HAWKER BEECHCRAFT CORPORATION 10016179 HAWKER BEECHCRAFT CORPORATION 10016501 HAWKER BEECHCRAFT CORPORATION EASA.IM.A.S.01992 REV. 2 FAA STC SA2710SW BAE 125 SERIES 800A HAWKER 800 HAWKER 800 XP HAWKER 850 XP HAWKER 900 XP HAWKER HS 125 EASA.IM.A.S.01993 REV. 2 FAA STC ST01342WI-D HAWKER 800 XP HAWKER 850 XP HAWKER 900 XP EASA.IM.A.S.01994 REV. 2 FAA STC ST09772SC-D BAE 125 SERIES 800A HAWKER 800 HAWKER 800 XP HAWKER 850 XP HAWKER 900 XP EASA.IM.A.S.01995 ST0998SC HAWKER 800 XP HAWKER 850 XP EASA.IM.A.S.01996 REV. 2 FAA STC ST09986SC-D HAWKER 800 XP HAWKER 850 XP HAWKER 900 XP Installation of Observer’s Jump Seat. 20.05.2008 Installation of Collins Integral Flight Information System (IFIS 5000) and Proline 21 Radios. EASA.IM.A.S.01997 REV. 3 FAA STC ST10001SC-D 750, 800XP, 850XP, 900XP Installation of a Honeywell Solid State Flight Data Recorder withInterface to Collins Proline 21. EASA.IM.A.S.02192 REV. 2 FAA STC ST10432SC-D HAWKER 800 XP HAWKER 850 XP HAWKER 900 XP EASA.IM.A.S.02408 REV. 2 FAA STC ST09955SC-D BAE 125 SERIES 800A HAWKER 800 HAWKER 800 XP HAWKER 850 XP HAWKER 900 XP EASA.IM.A.S.02863 REV. 3 FAA STC SA10747SC C90, C90A, C90GT, C90GTI, E90 Increase Operating Gross Weight Approval(as defined in the attached table) 1. Prior installation and approval of Kit 149- 3419-0001 is a prerequisite;2. Prior installation and approval of Kit 149-3420-0001 20.05.2008 is a prerequisite; Installation of a Smoke Detector System. 20.05.2008 Installation of the Magnastar C-2000 Airborne Telephone System -- 19.09.2006 Installation of an Airshow System. 20.05.2008 For Hawker 800XP model, installation is limited Prior to installation of this modification it 19.09.2011 to aircraft equippedwith Collins Proline 21 must be determined thatthe Avionics interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. Installation of Mark V Enhance Ground 1. The Flight Manual Supplement is not Proximity Warning System (EGPWS) with and needed for the -101 installation because the without Runway Awareness Advisory System. aircraft's basic AFM is still applicable.2. When fitted to Hawker 800XP and 850XP this STC is limited to the following aircraft 258541, 258556, 258567 through 258609, Installation of a Divan Cargo Net Assembly. 1. In accordance with Master Drawing List 800-197, Revision D, or later approved revision.2. Maintenance Manual Addenda 25- 50-05, This modification is only applicable to aircraft equipped with theCollins Proline 21 avionics package.Refer to aircraft defined in HawkerBeechcraft major change SC0353A. 21.05.2008 20.05.2008 Prior to installation of this modification it 23.03.2011 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 262/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016598 HAWKER BEECHCRAFT EASA.IM.A.S.03011 REV. 4 FAA STC ST 10596SC-D 800,750, 800XP, 850XP, 900XP Installation of an Aircell Axxess Voice/Data This modification is only applicable to aircraft Prior to installation of this modification it 30.10.2012 CORPORATION Communications System. equipped with theCollins Proline 21 or must be determined thatthe Honeywell SPZ-8000 avionics packages.RDL interrelationship between this modification 230-2001-103 and-107 Installation requires the and any other previouslyinstalled aircraft be equippedwith Collins Proline 21 modification and/ or repair will introduce radios with the IFIS STC ST01342WI-D no adverse effectupon the airworthiness of the product. 10016625 HAWKER BEECHCRAFT CORPORATION 10027658 HAWKER BEECHCRAFT CORPORATION 10029215 HAWKER BEECHCRAFT CORPORATION 10029220 HAWKER BEECHCRAFT CORPORATION 10029784 HAWKER BEECHCRAFT CORPORATION 10029917 HAWKER BEECHCRAFT CORPORATION 10030002 HAWKER BEECHCRAFT CORPORATION 10030003 HAWKER BEECHCRAFT CORPORATION 10031606 HAWKER BEECHCRAFT CORPORATION EASA.IM.A.S.03058 REV. 1 FAA STC SA03622AT BEECH B300, BEECH B300C Installation of an Air Conditioning Evaporator Blower Motor RF NoiseFilter into a Hawker Beechcraft Model B300 / B300C aircraft . P- EASA.IM.A.S.03021 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 23.03.2011 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. REV. 1 FAA STC SA02253LA B300/B300C Installation of Belly Radome. 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. 05.10.2011 FAA STC SA01502WI-D B300 SERIES STC SA01502WI-D issued to allow modification of the FGC-3000 units as asolution to eliminate nuisance pitch trim wheel movement. None. None. 12.03.2010 FAA STC ST03749AT-D GIV-X Installation of cabin interior and Airplane This approval is limited to only the installation None. 12.03.2010 Completion for Serial 4175. made in GulfstreamGIV-X, Serial No 4175.The following STC’s are a required part of this STC: ST02228CH-D, ,,ST02979AT-D, ST02980AT-D, ST02987AT-D, ST03047AT-D, ST03290AT-D, ST03410AT-D, ST03532AT-D, ST0354 FAA STC REF SA02277LA B300 KING AIR Installation of High Definition Audio Video Only applicable to King Air Model B300 aircraft Prior to installation of this modification it 20.04.2010 (HDAV-3002) LRU Unit as aninterface with the equipped with theRockwell Collins Venue must be determined thatthe Rockwell Collins Venue Cabin Management Cabin Management System. interrelationship between this modification System. and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. FAA STC ST10599SC-D 800XP, 850XP, 900XP Installation of an Espresso Maker This modification requires the installation of FAA STC ST10385SC-D,Installation of a Rockwell Collins CMS-1 Cabin Management System. FAA STC SA10969SC KING AIR C90GTI Installation of an upgraded Flight Management System (Version 4.0). This upgrade will offer a standard Flight Management Computer and willinclude an option for Search and Rescue Mission Profiles. Prior to installation of this modification the 03.05.2010 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. The installati None. None. 10.05.2010 FAA STC SA10970SC KING AIR B200 AND B300 Installation of an upgraded Flight Management None. System (Version 4.0) . This upgrade will offer a standard Flight Management Computer and willinclude an option for Search and Rescue Mission Profiles. None. 10.05.2010 REV. 2 FAA STC ST10922SC-D MODEL 4000 Installation of Cabin Interior Furnishings and Systems. Only configuration 3, 6, 8 and 9 installations EASA accepts the use of FAA (Means of 16.10.2012 are EASA approved. Airworthiness Limitations Compliance) Issue Papers S-1(Stage 4, inspections are contained in Chapter 4 of Closed 04/05/2010), S-1 (signed June theCompletions Manual. Airworthiness 21, 2011) and S-2 (signedJune 21, 2011) Limitations:for configurations 6 and 8 per 240- as being applicable to this project. Future 590011-0003C approved August 2010;for changes tothis STC that impact on the agreed means of comp 04/01/2013 Page 263/462
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04/01/2013 Page 1/462 - EASA

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