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 10040578 PROTOPLANE SPECIAL MISSION 208B Installation of Video Transmission Unit in Installer must check availability of EASA- The installation of this modification by 11.07.2012 AIRCRAFT accordance with Master DataList PP-008-MDL- approval for one or morereferenced STC when third persons is subject towritten 04, Issue 4, dated 11. July 2012 or later airplane is modified per that / those STC(s). permission of the approval holder and approvedrevision. disposal of the approvedappropriate ,,documentation.Prior to installation of this modification it must be determined thatthe interrelationship 10040714 PROTOPLANE SPECIAL MISSION B200C Removing of the metal parts of a cargo pod Limited to serial numbers BL 49 and BB 1473It This STC is applicable to aircraft B200C 23.07.2012 AIRCRAFT and provisions for theinstallation of signal is forbidden to use the modified pod to carry modified with an externalbaggage/cargo transmission antennas inside the pod. baggage or cargo.This modification does not carrier "Super 60 pod" as per FAA STC include power to the antennas installed onthe SA24551CE, EASAgrandfathered pod. The operation of the antennas is not through LBA STC 321/2/92.Prior to include in this approvaland must installation of this modification it must be determined thatthe interrelati 10015666 RAISBECK ENGINEERING EASA.IM.A.S.01642 REV 3 ST01468SE LEARJET 35 LEARJET 35A LEARJET 36 LEARJET 36A 10016131 RAISBECK ENGINEERING EASA.IM.A.S.02325 STC ST01724SE DATED JANUARY 5T 10016246 RAISBECK ENGINEERING EASA.IM.A.S.02521 REV. 2 FAA STC SA3593NM KING AIR 65-A90, B90, C90 KING AIR 65-C90A, C90GT, C90GT KING AIR 65-C90GTI, E90 10016579 RAISBECK ENGINEERING EASA.IM.A.S.02983 FAA STC SA2939NM BEECH 65-90 BEECH 65-A90 BEECH B90 BEECH C90 BEECH C90A 10016580 RAISBECK ENGINEERING EASA.IM.A.S.02984 FAA STC ST3857NM BEECH 200 BEECH 200C BEECH 200CT BEECH 200T BEECH A200 BEECH A200C BEECH A200CT BEECH B200 BEECH B200C BEECH B200CT BEECH B200T 10016581 RAISBECK ENGINEERING EASA.IM.A.S.02985 FAA STC SA3831NM BEECH 200 BEECH 200C BEECH 200CT BEECH A200 BEECH A200C BEECH A200CT BEECH B200 BEECH B200C BEECH B200CT BEECH B200T 10016582 RAISBECK ENGINEERING EASA.IM.A.S.02987 REV. 2 FAA STC SA4010NM 1. 65-90, 65-A90, B90, E90 2. C90A, C90GT, C90GTI 10016583 RAISBECK ENGINEERING EASA.IM.A.S.02988 FAA STC SA3366NM BEECH 200 BEECH 200C BEECH 200CT BEECH A200 BEECH A200C BEECH A200CT BEECH B200 BEECH B200C BEECH B200CT BEECH B200T Installation of drag reduction system (including outboard trailing edge extension, leading edge vortilons & contoured flap). 21.08.2006 LEARJET 31 Installation of a drag reduction system (contoured flap). 22.11.2007 Installation of propeller system. 1. See attached Propellers and Propeller Prior to installation of this modification it 06.09.2010 Limitations 2. Hartzell HC-D4N-3C hubs with must be determined thatthe Hartzell D9290K blades in pairs.Diameter 93.0 interrelationship between this modification in. (maximum); minimum allowable for repair: and any other previouslyinstalled 92.0 in. Nofurther reduction in diameter modification and/ or repair will introduce permitted. Pitch Settings: Low Pitch: 2 no adverse effectupon the airworthiness of the product. Installation of nacelle overwing storage lockers and lower flap fairing. Installation of nacelle overwing storage lockers and lower flap fairing. 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 install 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 install Installation of improved leading edge consisting Prior to installation of this modification the of inboard leading edges, deice boots, leading installer must determine that the edge ducts, leading edge to nacellefairing, and interrelationship between this modification and associated hardware. any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install Installation of dual aft body strakes on the 90 series King Air aircraftper Raisbeck Engineering Inc. STC SA4010 NM. 05.08.2008 05.08.2008 05.08.2008 none Prior to installation of this modification the 26.04.2011 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 Installation of Ram Air Recovery System. 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 install 04/01/2013 Page 364/462 05.08.2008
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016599 RAISBECK ENGINEERING EASA.IM.A.S.03012 REV. 1 FAA STC ST3591NM 200, 200C, 200T, 200CT, A200, Installation of lower aft fuselage strakes. None Prior to installation of this modification the 01.07.2011 A200C, A200CT, B200, B200C, installer must determinethat the B200GT, B200CGT interrelationship between this modification B200T, B200T, B200CT, and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. The installati 10016620 RAISBECK ENGINEERING EASA.IM.A.S.03051 FAA STC ST00752SE BEECH 200 This change applies only to the above listed Requires the prior incorporation of Raisbeck 15.12.2008 SEE ATTACHED EASA model aircraft in accordance with Raisbeck STC’s ref:-SA4175NM (when equipped with APPROVED TYP Engineering Master Drawing List 99-1500, High Floatation Revision D, dated May 13, 2008 or later gear)SA3366NMSA3831NMSA3519NMIt is approved revisions. the installers responsibility to ensure all these referenced STC’s are EASA approved. 10030124 RAISBECK ENGINEERING EASA.IM.A.S.02986 REV. 3 FAA STC SA4175NM 200, 200C, 200T, 200CT, A200 A200C, A200CT, B200, B200C B200T, B200CT, B200GT, B200CGT B300, B300C Installation of fully enclosed main landing gear door system forhigh-flotation gear equipped aircraft. 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. 10.08.2011 10031275 RAISBECK ENGINEERING EASA.IM.A.S.00765 REV. 1 FAA STC SA2698NM-S BEECH 200, A200, B200 Installation of Hartzell/Raisbeck Quiet Turbofan Data is suitable for reproduction and installation Prior to installation of this modification it 09.08.2010 Propeller. Thisinstallation consists of Hartzell 4- on all Beech SuperKing Model 200 series must be determined thatthe bladed propellers and aluminum hubswith aircraft. Approval of this change in type interrelationship between this modification spinners, and a propeller de-icing system designapplies to the above model aircraft only and any other previouslyinstalled This approval should not be extended to other modification and/ or repair will introduce aircraft on which otherpreviou no adverse effectupon the airworthiness of the product. 10031307 RAISBECK ENGINEERING FAA STC ST01182LA A320-232 A320 bin extension systemInstallation of a bin extension system in accordance with FAASupplemental Type Certificate ST01182LA issued 10 July 2001. 10027805 RAM AIRCRAFT, LIMITED PARTNERSHIP 10031425 RAM AIRCRAFT, LIMITED PARTNERSHIP 10031513 RAM AIRCRAFT, LIMITED PARTNERSHIP 10032348 RAM AIRCRAFT, LIMITED PARTNERSHIP - Refer to paragraph "Limitations & Conditions" listed in the FAA STCST01182LA;The Maintenance Instructions for Continued Airworthiness are containedin the RCAG Component Maintenance Manual 200A-2560. These maintenanceinstructions must be included in the o Prior to installation of this modification it 09.08.2010 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. FAA STC SE10746SC-D IO-520-B -, -BB, -C, -CB Conversion of Teledyne Continental Motors The RAM model IO-550-B-RA engine is This approval should not be extended to 17.11.2009 (TCM) models IO-520-B, -BB toRAM model IO- identical to and has the sameratings, other engines of these models onwhich 550-B-RA engine, or conversion of TCM limitations, and installation interfaces as TCM other previously approved modifications models IO-520-C, -CBto RAM model IO-550-C- model IO-550-Bengine. The RAM model IO- are incorporated unless itis determined by RA engine in accordance with RAM Master 550-C-RA is identical to and has the the installer that the interrelationship DrawingList 2691, Revision I.R. dated sameratings, limitations, and installation between thischange and any other November 7, 20 interfaces as T previously approved m REV. 2 FAA STC SA8125SW-D CESSNA 414A Installation of vortex generators in acc. with None See under "Description" Prior to 12.11.2010 FAA STC SA8125SW-D, lastissue, dated May installation of this modification it must be 12, 2008:Option 1: Modification in acc. with determined thatthe interrelationship RAM Master Drawing No. 1507,Revision C, between this modification and any other dated 11/03/1992.Option 2: Modification in acc. previouslyinstalled modification and/ or with RAM Master Drawing No. 1507,Re repair will introduce no adverse effectupon the airworthines REV. 1 FAA STC SA09105SC-D CESSNA 414A Modification in acc. with FAA STC SA09105SC-This approval is limited to Hartzell PHC-C3YF- Prior to installation of this modification it 12.11.2010 D: Aircraft modified inaccordance with RAM 2UF/FC7663D(B)-2Q or PHC-C3YF- must be determined thatthe Master Drawing No. 1765, Revision B, 2UF/FC7693DF(B) propellers. interrelationship between this modification dated20/09/1995 and Installation of modified and any other previouslyinstalled TCM engine model TSIO-520-NB:Option 1: modification and/ or repair will introduce Cessna 414A modified by FAA STC no adverse effectupon the airworthiness SE09104SC-D or S of the product. REV. 1 FAA STC SA09971SC-D 1. CESSNA 340, 340A 2. CESSNA 414, 414A, 402C Installation of Hartzell propeller PHC-C3YF- 2UF/FC7693DF(B) inaccordance with FAA STC SA09971SC-D 1. Hartzell Modell PHC-C3YF-2UF/FC7693DF Prior to installation of this modification it or PHC-C3YF-2UF/FC7693DFBpropellers are must be determined thatthe 02.11.2010 limited to aircraft that are previously FAA interrelationship between this modification approved toinstall 78-inch (198 cm) diameter and any other previouslyinstalled propellers and have TCM model TSIO- modification and/ or repair will introduce 520series engines with maximum rated power no adverse effectupon the airworthiness from 285 of the product 04/01/2013 Page 365/462
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04/01/2013 Page 1/462 - EASA

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