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 10028706 ECMS AVIATION SYSTEMS GMBH BELL 212, 412 Load Attachment Device BRD01 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. 04.02.2010 10017166 ECT INDUSTRIES EASA.R.S.01274 AS 350 B3 Installation of ECT Industries DMS ARINC data recorder p/n REC-AR0-TT-OO 04.04.2007 10017228 ECT INDUSTRIES EASA.R.S.01399 REV. 4 AS355F1, AS355F2 Installation of BRITE SAVER 2 Data Monitoring None The installation of this modification by 15.05.2012 AS355N, AS355NP SystemRevision 1 - covered a documentary third persons is subject towritten change to STCRevision 2 - covered torque and permission of the approval holder and memory management minor changeRevision 3 holding and disposal ofthe approved - covered installation of ultrasonic air/ground appropriate documentation.Prior to switch,second possible location of installation of this modification it must be determined thatthe interre 10017230 ECT INDUSTRIES EASA.R.S.01401 REV. 4 AS350B, AS350B1, AS350B2 Installation of BRITE SAVER 2 Usage None This STC is approved only for the product 20.08.2012 AS350BA, AS350BB, AS350D Monitoring System Revision 1 - includes torque configuration as defined inthe approved and memory management minor change design data referred to in the Revision 2 - includes addition of the possibility paragraphs"Title/Description" and to install theultrasonic air/ground switch and "Associated Technical second source for the SUBD connectorsand Documentation".Compatibility with other aircraft/engine configurations shall bedetermin 10017248 ECT INDUSTRIES EASA.R.S.01446 REV. 2 AS350 B3, EC 130 B4 Installation of BRITE SAVER 2 Data Monitoring None Prior to installation of this modification it 19.10.2009 System (DMS)This STC is a Revision to an must be determined thatthe already EASA approved STC ref. interrelationship between this modification 10017248,rev 1 dated 31/08/2009 to include and any other previouslyinstalled Software Evolution and upgrade of CPUand modification and/ or repair will introduce analogical card of the data Monitoring System no adverse effectupon the airworthiness BRITE SA of the product. 10017272 ECT INDUSTRIES EASA.R.S.01494 ROBINSON R22 ROBINSON R22 ALPHA ROBINSON R22 BETA ROBINSON R44 ROBINSON R44 II DMS R22 & R44 - Brite Saver PE Usage Monitoring System for Robinson R22 and R44 Series Helicopters 10027406 ECT INDUSTRIES P-EASA.R.S.01417 REV. 3 EC 120B Installation of ECT Industries DMS P/N REC- ARAO-TT-00 Rev. 1 adds a software change in the Data Monitoring System "Brite Saver2 and an RFM SupplementRev. 2 adds a Usage Monitoring System for EC120 - "Brite Saver 2 amdt 4" • 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.• Th 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. 10027594 ECT INDUSTRIES P-EASA.R.S.01487 REV. 6 EC120B Installation of Night Image Vision System kit, Refer to applicable RFM for list of equipment allowing night VFR flightwith Night Vision mandatory for Night VisionImage System GogglesRev. 2 changes temperature limitation certificationEC120B equipped with STC in Rotorcraft Flight ManualRev. 3 incorporates 10027594 Revision 4 minor changes to NVIS Shunt and LACURev. 4 displays administrative changes 10028220 ECT INDUSTRIES REV. 1 206H, P206, P206A, P206B, P206C, P206D, P206E, T206H, TP206A, TP206B, TP206C, PT206D TP206E, TU206A, TU206B, TU206C TU206D, TU206E, TU206F, TU206G U206A, U206B, U206C, U206D U206E, U206F, U206G 10029479 ECT INDUSTRIES P-EASA.R.S.01541 AS355E, AS355F, AS355F1 AS355F2, AS355N, AS355NP STC DTS and DTS V2 Cessna 206 - Installation Tracking System STC DTS AS 355 - Installation of a Tracking system. 13.01.2009 19.09.2011 Prior to installation of this modification it 19.09.2011 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. The fi Limitation to Cessna 206 VFR only 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. 05.03.2010 None. Prior to installation of this modification the 26.03.2010 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. 04/01/2013 Page 198/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10029936 ECT INDUSTRIES REV. 1 AS350B, AS350B1, AS350B2 Installation of DTSV2 Data Transmission Modification not approved for aircraft equipped The approval holder shall fulfil the 30.07.2012 AS350BA, AS350BB, AS350B3 System.Revision 1 introduces corrections of with weather radar orAFCS (Automatic Flight obligations of Part 21, the tracking system installation. Control System).Modification not approved for Paragraph21.A118A. Prior to installation AS350B3 model helicopters withmodification of this modification it must be determined OP-4305 (Arriel 2D engine installation) thatthe interrelationship between this incorporated. modification and any other previouslyinstalled modification and/ or repa 10030143 ECT INDUSTRIES AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP Installation of DTSV2 Tracking System None None 27.05.2010 10030338 ECT INDUSTRIES P-EASA.R.S.01510 AS350B, AS350B1, AS350B2, Installation of a tracking system (DTS - Data Modification not approved for aircraft equipped Prior to installation of this modification it 11.06.2010 AS350BA, AS350BB, AS350B3 Transmission System) with weather radar orAFCS (Automatic Flight must be determined thatthe Control System) interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 10033164 ECT INDUSTRIES P-EASA.R.S.01505 REV. 3 EC135 P1(CPDS) EC135 P2(CPDS), EC135 P2+ EC135 T1(CPDS) EC135 T2(CPDS), EC135 T2+ EC135 NVIS Lighting SystemInstallation of a Night Vision Imaging Lighting system, to enableoperation with Night Vision Goggles.- Avionic type 1- P/N: 60D-1000-000, into helicopters with CPDS andconventional flight/navigation instruments-Avionic type 2- P/N: None The first installation of this kit must be supervised by the STC holder.This rotorcraft employs Night Vision Imaging System lighting, commonlynamed NVIS lighting, that has been certified to ensure the aircraft iscompatible with night vision goggles (NVG). 10037841 ECT INDUSTRIES EC135 P1, EC135 P2, EC135 P2+ Installation of Brite Saver Usage Monitoring Only for EC135/EC635 variants with CPDS- EC135 T1, EC135 T2, EC135 T2+ SystemInstallation of a Brite Saver Usage Cockpit EC635 P2+ Monitoring System. This modificationis defined EC635 T1(CPDS), EC635 T2+ in CONFAD-0115-92-EN. 10042012 ECT INDUSTRIES AS 350 B,AS 350 B1,AS 350 B2 AS 350 B3,AS 350 BA,AS 350 BB Installation of Data Tracking System DTS- Alpha.Modification as defined in STC Data List, doc. SDL-DTSALPHA-AS350 Rev.04 10032345 EICHELSDOERFER GmbH RF5 STC "Installation engine Rotax 912 and propeller HO-V352F-S1/S170FQ inthe powered sailplane Fournier RF 5" 10040934 EIRTECH AVIATION SERVICES LIMITED REV. 1 737-600,-700,-800,-900,-900ER Cabin Altitude and Take-off Configuration warnings and indications -Activation. 27.01.2012 Prior to installation of this modification it 03.01.2012 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 Modification not approved for rotorcraft Prior to installation of this modification it 31.10.2012 equipped with AFCS (AutomaticFlight Control must be determined thatthe System) or Weather Radar.Modification not interrelationship between this modification approved for AS350B3 model helicopters and any other previouslyinstalled withmodification OP-4305 (Arriel 2D engine modification and/ or repair will introduce installation) incorporated. no adverse effectupon the airworthiness of the product. Limited to Fournier RF 5, S/N 5012 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. 28.10.2010 This change is not applicable to an aircraft with High Altitude LandingCapability. 10016491 EJM AEROSPACE SERVICES EASA.IM.A.S.02853 FAA STC ST02534AT BOEING 747-400 Installation of a Matsushita Avionics Systems This STC is approved only for the product Corporation System 3000 In-Flight configuration as defined in the approved design Entertainement System on a Singapore Airlines data. Compatibilty with other aircraft/engine Boeing 747-400 in accordance with Master configurations shall be determined by the Drawing List MDL 10321, Rev. H. dated 29/04/2003, or later FAA approved revision. installer. 10028392 EJM AEROSPACE SERVICES FAA STC ST02531AT B747-400 Installation of a Matsushita Avionics Systems Corporation System 3000In-Flight Entertainment system on a Singapore Airlines Boeing 747-400type aircraft in accordance with Master Drawing List MDL10270, Rev. G,dated 06 June 2003 or later FAA approved revisio Prior to installation of this modification it 26.10.2012 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. 18.08.2008 Not Applicable Airplane Flight Manual Supplement, Doc. 04.01.2010 Nr. 14526003 dated June 4, 2002or later approved revision is required as part of this STC 04/01/2013 Page 199/462
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04/01/2013 Page 1/462 - EASA

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