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 10017285 DRF STIFTUNG LUFTRETTUNG EASA.R.S.01533 EUROCOPTER DEUTSCHLAND Title: Installation of a L-3 SSCVR Cockpit 1. Prior to installation of this modification the 04.05.2009 BK117 B Voice RecorderDescription: Optional installer must determine that the Installation of a Cockpit Voice Recorder. The interrelationship between this modification and installation is in accordance with DRF change any other previously installed modification will no. 135, MDL MD-117-31-32-00001. introduce no adverse effect upon the airworthiness of the product.2. 10029942 DRF STIFTUNG LUFTRETTUNG MBB-BK 117 B-2, MBB-BK 117 C- Installation of Garmin GNS 530 FMS Not Applicable The approval holder shall fulfil the 04.05.2010 1 COM/NAV System and TCAS-1 Sky 899TCAS obligations of Part 21, Paragraph21A.118A. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repa 10031819 DRF STIFTUNG LUFTRETTUNG MBB-BK117B-2, MBB-BK117 C-1 Installation of second directional gyro None Prior to installation of this modification it 16.09.2010 systemInstallation of a second directional gyro must be determined thatthe system for IFR operation basedon DRF Major interrelationship between this modification Change Project 240 and defined in MD-117-34- and any other previouslyinstalled 20-00001. modification and/ or repair will introduce no adverse effectupon the airworthiness of the product 10033429 DRF STIFTUNG LUFTRETTUNG P-EASA.R.S.01563 BK117 C-1 Title: Installation of Modular Airborne Data Recording/AcquisitionSystem (MADRAS)Description: Optional Installation of a Cockpit Voice and Flight DataRecorder System. The installation is in accordance with DRF change no.111, MOL MD-117-31- 32-00003 Re 10041970 DRF STIFTUNG LUFTRETTUNG MB BK 117 C-2 Installation of a TETRA Digital Radio System into a NVIS certifiedCockpit. 10016181 DRIESSEN AIRCRAFT INTERIOR SYSTEMS 10016292 DRIESSEN AIRCRAFT INTERIOR SYSTEMS 10016552 DRIESSEN AIRCRAFT INTERIOR SYSTEMS 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. The in 23.06.2009 Required premodification: EASA approval EASA 10034057 (ECD major changeE-1807). This rotorcraft employs Night Vision Imaging System lighting, commonlynamed NVIS lighting, that has been certified to ensure the aircraft iscompatible with night vision goggl EASA.IM.A.S.02410 FAA STC ST00826LA AIRBUS A340-300 Installation of Lower Deck Mobile Crewrest. 1. The limitations and conditions as referenced in FAA STC ST00826LA apply.2. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification The change has undergone NVIS 29.10.2012 compatibility engineering evaluation. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will intr EASA.IM.A.S.02588 REV. 1 FAA STC ST00843LA BOEING 757-200 SERIES Galley installation. None. Prior to installation of this modification the 18.02.2010 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 EASA.IM.A.S.02932 BOEING 747-200B BOEING 747-200C Installation of a TBO Container. The installation should not be incorporated in 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 10037862 DUGAN KINETICS, L.L.C. FAA STC ST02127SE DC-9-81/-82/-83/-87, MD-88 Thrust Reverser/Installation of ejector thrust reverser on Pratt &Whitney Turbofan JT8D- 217, -217A, 217C or -219 Engines as per FAA STCST02127SE dated 08 Apr. 2011. Refer to FAA STC ST02127SE. Refer to FAA STC ST02127SE. 03.01.2012 10015358 DUNCAN AVIATION, INC. EASA.IM.A.S.00657 FAA STC ST00515WI LEARJET 35 Installation of an Allied Signal CAS 67A Traffic 1. This STC is approved only for the product 04.04.2005 LEARJET 35A Alert & Collision Avoidance (TCAS II). (STC configuration as defined in the approved design LEARJET 36 ST00515WI) data referred to in the paragraph "Description". LEARJET 36A Compatibility with other aircraft/engine configurations shall be determined by the installer. 10015417 DUNCAN AVIATION, INC. EASA.IM.A.S.01139 FAA STC ST00546WI LEARJET 60 Installation of a Universal Avionics Inc. UNS-1B 1. For certification basis refer to FAA TCDS 11.04.2005 FMS (Dual). A10CE.2. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall b 04/01/2013 Page 188/462 22.08.2007 04.07.2008
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015488 DUNCAN AVIATION, INC. EASA.IM.A.S.01249 FAA STC ST00452WI CESSNA 650 CITATION III Installation of the AlliedSignal CAS 67A TCAS This STC is approved only for the product 13.03.2006 CESSNA 650 CITATION IV II System configuration as defined in the approved design CESSNA 650 CITATION VII data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 10015505 DUNCAN AVIATION, INC. EASA.IM.A.S.01268 ST00315WI LEARJET 60 Installation of Collins TCAS-94 i.a.w. Dok List 10045000 07.02.2007 10015640 DUNCAN AVIATION, INC. EASA.IM.A.S.01603 FAA STC ST0069WI BOMBARDIER CL-600-1A11 (CL- Installation of Honeywell TCZ-910 TCAS II & This STC is approved only for the product 25.10.2005 600 XS-852 Mode S Transponder System configuration as defined in the approved design BOMBARDIER CL-600-2A12 (CL- data referred to in the paragraph "Description". 601 Compatibility with other aircraft/engine BOMBARDIER CL-600-2B16 configurations shall be determined by the installer. 10015742 DUNCAN AVIATION, INC. EASA.IM.A.S.01766 FAA STC SA00894WI CESSNA 525 Installation of Honeywell CAS 67A TCAS II The call outs and their priority are to be 26.01.2006 System on Cessna 525. FAA Approval of STC confirmed as part of each installation. Nr. SA00894WI: 08 September 2000. 10015826 DUNCAN AVIATION, INC. EASA.IM.A.S.01904 ST00932WI LEARJET 31 LEARJET 35 LEARJET 35A LEARJET 36 LEARJET 36A Installation of Universal Avionics TAWS None 11.05.2006 10015844 DUNCAN AVIATION, INC. EASA.IM.A.S.01941 FAA STC SA2405CE-D GULFSTREAM 1125 WESATRD Installation of Garret Model GTCP36-150(W) This STC is approved only for the product 25.10.2006 ASTRA Auxiliary Power Unit used as nonessential configuration as defined in the approved design GULFSTREAM ASTRA/SPX Bleed Air source for on board electrical and data referred to in the paragraph "Description". enviromental systems. Compatibility with other aircraft/engine configurations shall be determined by the installer. 10015917 DUNCAN AVIATION, INC. EASA.IM.A.S.02049 FAA STC ST00865CH-D BAE 125 -800 SERIES Installation of Honeywell MK VII Enhanced 1. Only Software standard -226-226 or later 10.09.2007 HAWKER 800 Ground Proximity Warning System (EGPWS) is approved for installation.2. Prior to HAWKER 800 XP to software version -226-226 and Optional installation of this modification the installer must RAAS determine that the interrelationship between this modification and any other previously installed modification w 10015938 DUNCAN AVIATION, INC. EASA.IM.A.S.02079 ST01157WI-D LEARJET 35A Installation of L-3 Communications F1000, 30.10.2006 LEARJET 36A SSFDRFAA STC ST01157WI-D 10015972 DUNCAN AVIATION, INC. EASA.IM.A.S.02123 FAA STC ST01159WI-D LEARJET 31 Installation of Honeywell Mk-VIII EGPWS.FAA None. 17.01.2007 LEARJET 35A LEARJET 36A STC ST01159WI-D 10015987 DUNCAN AVIATION, INC. EASA.IM.A.S.02141 ST02092CH-D HAWKER 800 XP Installation of a forward cabin entry door and Applicable to Aircraft Serial Number 258645 20.09.2006 aft cabin reconfiguration only 10016104 DUNCAN AVIATION, INC. EASA.IM.A.S.02294 FAA STC NO. ST2359CH-D BAE 125 SERIES 800A Modification of the existing Collins TDR-94D 1. This STC is only approved where ARINC 20.08.2007 Transponders and Collins RTU-870 Radio 429 databus or similar standard is used as an Tuning Units to Enhanced Surveillance capable input to the transponders, it does not approve equipment and aircraft interface requirements. the use of Gilham or Grey code as the input to the Mode S transponders. As the applicant has not demonstrated that this 10016105 DUNCAN AVIATION, INC. EASA.IM.A.S.02295 FAA STC NO. ST02370CH-D BAE 125 SERIES 800A HAWKER 800 HAWKER 800XP 10016110 DUNCAN AVIATION, INC. EASA.IM.A.S.02300 US STC NO. ST02371CH-D HAWKER 800 XP HAWKER 800, 800A 10016149 DUNCAN AVIATION, INC. EASA.IM.A.S.02351 FAA STC NO. ST02091 CH-D BAE 125 SERIES 800A HAWKER 800 HAWKER 800 XP 10016235 DUNCAN AVIATION, INC. EASA.IM.A.S.02499 FAA STC ST00858WI LEARJET 35 LEARJET 35A LEARJET 36 LEARJET 36A Upgrade of the existing dual Universal Avionics Systems Corporation UNS-1D Flight Management System to UNS-1D+ Flight Management System. EASA approved Airplane Flight Manual Supplement, 061108004, Revision 0, dated November 10, 2006, EASA approved Jabuary 10, 2007 or later EASA approved revision is required.Compatibility of this design change with previously approved modifications must be d Installation of Aircell Iridium ST-3100 single Compatibility of this design change with channel SATCOM system. previously approved modifications must be determined by the installer.If the holder agrees to permit another person to use this certificate to alter the product , the holder shall give the other personwritten eviden Replacement of Existing #3, #4 and #5 1. If the holder agrees to permit another person auxiliary batteries with Securaplane XL245 lead to use this certificate to alter the product, the acid batteries holder shall give the other person written evidence of that permission. Installation of Collins TCAS-94 TCAS II This installation is not to be used in airspace System. where Elementary Surveillance (ELS) or enhanced surveillance (EHS) is required. 04/01/2013 Page 189/462 31.05.2007 31.05.2007 30.04.2007 19.12.2007
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04/01/2013 Page 1/462 - EASA

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