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 10032060 RUAG AEROSPACE SERVICES GmbH CL-600-1A11 Installation of Satcom Iridium System none Prior to installation of this modification it 06.10.2010 CL600-2B16, CL-600-2A12 Simphone DUO 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. 10032061 RUAG AEROSPACE SERVICES GmbH CL-600-1A11 CL600-2B16, CL-600-2A12 Electronic Flight Bag NavAero tBagC2 (EFB) - Class II 10033641 RUAG AEROSPACE SERVICES GmbH P-EASA.A.S.03896 EMB-135BJ Modification 289A: Thrane & Thrane Aero SB Lite Satcom Installation 10034074 RUAG AEROSPACE SERVICES GmbH 525 525A 10036250 RUAG AEROSPACE SERVICES GmbH BD 100-1A10 (CHALLENGER 300) 10036633 RUAG AEROSPACE SERVICES GmbH REV. 1 BD-700-1A10 BD-700-1A11 Installation of High Speed SATCOM system with on-board WLAN Interface. Installation of EGPWS MK-V with Runway Awareness and Advisory System(RAAS). 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. 06.10.2010 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. 01.02.2011 STC limited to S/N 525-0516The WLAN clients Prior to installation of this modification it 04.03.2011 (Handsets, Laptops, etc) are not covered by must be determined thatthe this STC.The usage of these components is interrelationship between this modification requiring operational approval. and any other previouslyinstalledmodification and/ or repair will introduce no adverse effect upon theairworthiness 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. 25.08.2011 Dual Electronic Flight Bag (EFB) Installation 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. 27.09.2011 10039078 RUAG AEROSPACE SERVICES GmbH BELL 205A-1 Title: Load Attachment Device BRD01 on Bell None 205A-1Description: The BRD01 is a cabin mounted device for attaching loads onBell helicopters. It is used with opened sliding doors and can bemounted left- and righthand simultaneously. None 04.04.2012 10042290 RUAG AEROSPACE SERVICES GmbH REV. 1 CL-600-1A11, CL-600-2A12 CL-600-2B16 10042291 RUAG AEROSPACE SERVICES GmbH CL-600-1A11, CL-600-2A12 CL-600-2B16 Flight Management System NZ-2000 - Upgrade to SW 6.1 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. 21.11.2012 ACSS TCAS II / 2000 Change 7.1 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. 21.11.2012 04/01/2013 Page 382/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015012 RUAG SCHWEIZ AG EASA.A.S.03314 BOMBARDIER DHC-6 SERIES Avionics system upgrade- In: Weather Radar 1. Reg.:T-741 S/N: 4662. Prior to 20.04.2009 300 System incl. ART-2000, AA-2012V, CM-2000; installation of this modification the installer must Garmin GMX-200 Multi Function Display determine that the interrelationship between system; Avidyne TAS-620 system incl. Heading this modification and any other previously Adapter AHRS-500; Garmin GTX-330 Mode S installed modification will introduce no adverse Transponder system; Collins DME IND-42 system effect upon the airworth 10017236 RUAG SCHWEIZ AG EASA.R.S.01415 EUROCOPTER FRANCE SA Enhanced navigation systemRemoved T-771 S/N: 6146Valid for this S/N. 04.08.2008 365N Equipment:- Pilot & Copilot HSI 651- Trimble 2101 GPS with MD41 Annunciator Control Unit and MD40 CDI- KTR 908 VHF COM System with KSF 598 Control Unit- KEA 346 Encoding Altimeter- Badin Crouzet Encoding Altimeter- KAS 297 10026920 RUAG SCHWEIZ AG EASA.R.S.01550 01.07.2009 10027200 RUAG SCHWEIZ AG P-EASA.R.S.01582 MD900 TV Broadcasting Equipment Installation The Installation TV Broadcasting Equipment is 1) Prior to installation of this modification 14.09.2009 (camera adaptation on existingmount and limited to: S/N 900-00131 the installer mustdetermine that the certification of the operators rack) interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product. 2) The inst 10030985 RUAG SCHWEIZ AG P 180 AVANTI II In-Flight Entert. System Installation by installing a ROSEN"RosenViewVX" moving Map and DVD System, an IR-Eye, One FLIGHT DISPLAYSYSTEM 10.2 inch LCD and two 7 inch LCD's and a FLIGHT DISPLAY SYSTEMwireless audio transmitter for audio distribution to SENNH 10031322 RUAG SCHWEIZ AG EASA.R.S.01547 500 N IRIS Camera Installation.Installed: L3 Avionics System Type A100 IRIS Camera System. 10034921 RUAG SCHWEIZ AG PC-6 ALL SERIES Avionics upgrade with Aspen EFD1000 Removed: - Various Equipment (if installed) i.a.w. DIC 1898256-101 Installed:- Aspen EFD1000 Electronic Flight Instrument System- Dual Garmin GNS430W COM/NAV/GPS- Garmin GMA 340 Audio Panel 10037011 RUAG SCHWEIZ AG EC 130 B4 Avionics RetrofitOut: Garmin GTX·330 Mode S Transponder & GMA·340 Audio/Marker system;Honeywell KX·165A VHF·COM/NAV systemIn: Aspen EFD 1000H EFIS system; Garmin GNS 430W VHF COM/NAV & GPSsystem; Garmin GSR 56 Iridium system; PS Engineering PMA 8000BAudio/ 10014929 RUECKER AEROSPACE GMBH EASA.A.S.03182 AIRBUS A340-300 A340-300 new First Class Seats Test Aircraft /Installation of four newly developed First Class Seats in an Airbus A340-300 aircraft for testing. 10014961 RUECKER AEROSPACE GMBH EASA.A.S.03232 DORNIER 328-100 Installation of s 230VAC Euro standard power socketat both cockpit sidewalls. 10027449 RUECKER AEROSPACE GMBH DORNIER 228-101 Installation of UHF Research Mission Equipment None The approval holder shall fulfil the obligations of Part 21, Paragraph21.A109. Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repai 20.07.2010 Serial number: LN088. Prior to installation of this modification the 02.06.2009 installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the product. S/N: All- One independent Communication or Navigation System needs to beinstalled in addition to the two GNS430W.- RNAV (GPS) Approaches to LNAV, LNAV/VNAV or LPV minima are notapproved. The approval holder shall fulfil the obligations of Part 21, Paragraph21.A109.Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or 13.05.2011 S/N 7214 repair 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. 22.11.2011 25.03.2008 22.08.2007 Limited to serial number 7083 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. 01.10.2009 04/01/2013 Page 383/462
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04/01/2013 Page 1/462 - EASA

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