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 10039496 AVIONICS INTEGRATION & 35A/36A Replacement of UNS-1M by UNS-1Fw MMMS None Prior to installation of this modification it 08.05.2012 ENGINEERING (UASC) 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. 10041282 AVIONICS INTEGRATION & ENGINEERING CL-600-2B16 CPDLC System Capability CPDLC system not compliant with Commission Regulation (EC) 29/2009 10014074 AVIONICS MOBILE DESIGN SERVICES EASA.A.S.01166 BAE JETSTREAM 31 Installation of Airborne Collision Avoidance BAE JETSTREAM 32 System (ACASII) 10014139 AVIONICS MOBILE DESIGN SERVICES EASA.A.S.01252 CESSNA 550 Installation of an Airborne Collision Avoidance CESSNA 650 System (ACAS II) 10014184 AVIONICS MOBILE DESIGN SERVICES EASA.A.S.01322 CN 235M-100 Installation of a Ground Proximity Warning Aircraft Registration A40-CU and A40- 10014198 AVIONICS MOBILE DESIGN SERVICES EASA.A.S.01341 BAE 125-800 system (GPWS) & Terrain Awareness Warning CVSerial numbers C062 and C063 System (TAWS) Installation of an Airborne Collision Avoidance System (ACAS II) 10014215 AVIONICS MOBILE DESIGN SERVICES EASA.A.S.01376 CESSNA 550 SERIES Avionics Mobile Services Modification CESSNA 560 SERIES AM/1478. Installation of an Airborne Collision Avoidance System (ACAS II) 10014303 AVIONICS MOBILE DESIGN SERVICES EASA.A.S.01547 PIPER PA-31T2 Certification of FAA Approved field modificains for the issue of an EASA C of A.Avionics Mobile Services AFM supplement Part 21-008 014 GNS-530,Avionics Mobile Services AFM supplement Part 21-008 015 KMH- 880Avionics Mobile Services AFM supplement Part 21- Applicable to s/n 5042 onlyPrior 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 airworthi 10014431 AVIONICS MOBILE DESIGN SERVICES EASA.A.S.02479 1124A WESTWIND II Installation of Airborne Collision Avoidance System (ACAS II) 13.03.2006 10014480 AVIONICS MOBILE DESIGN SERVICES EASA.A.S.02543 REV 2 HAWKER HS 125-700 SERIES Installation of an Airborne Collision Avoidance This STC is approved only for the product 09.10.2006 REV 2 System (ACASII)Amendment of the above to configuration as defined in the approved design include installation variations for alternate data referred to in the paragraph "Description". aircraft with regard to the Downlink Aircraft Compatibility with other aircraft/engine Parameters (DAP's) for Mode-S Enhanced configurations shall be determined by the Surveillance (EHS) installer. 10014481 AVIONICS MOBILE DESIGN SERVICES EASA.A.S.02544 HS 125-700 SERIES Installation of a Digital Air Data Display System -- 06.04.2006 10015654 AVIONICS MOBILE DESIGN SERVICES EASA.IM.A.S.0163 REVISION 1 10015663 AVIONICS MOBILE DESIGN SERVICES EASA.IM.A.S.0164 REVISION 1 10036511 AVIONICS MOBILE DESIGN SERVICES (AM REV 1 HS 125-700 SERIES Installation of a Rockwell Collins TCAS-4000 Traffic Alert and Collision Avoidance System (TCAS-II) REV 1 - HS 125-700 SERIES Installation of a Ground Proximity Warning System (GPWS) and Terrain Awareness Warning System (TAWS) 10015345 AVIONICS SUPPORT GROUP, INC. EASA.IM.A.S.00446 FAA STC ST02900AT BOEING 747-200 BOEING 747-300 HAWKER 800XP Installation of a Flight Data Recorder (FDR) System. T2CAS provisions on Boeing 747-200 & -300 Series Aircraft. 04.09.2012 17.03.2005 08.04.2005 29.11.2005 06.10.2005 26.07.2005 18.11.2005 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 be determined by the installer. 09.06.2006 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 be determined by the installer. 09.06.2006 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. 16.09.2011 1. Subject to compliance with the provisions of Part 21 Subpart E, this STC and associated shall remain valid until surrendered, withdrawn or otherwise terminated.2. If transfer of this STC is requested under Part 21A.116, the STC will be reissued.3. This 04/01/2013 Page 100/462 21.12.2004
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015447 AVIONICS SUPPORT GROUP, INC. EASA.IM.A.S.01188 FAA STC ST02976AT BOEING 737-300 SERIES Installation of ACCS Elementary and Enhanced 1. According to FAA STC No ST02976AT2. 25.10.2005 BOEING 737-400 SERIES Surveillance capable Mode S Transponders This STC is approved only for the product BOEING 737-500 SERIES and Flight ID capable Transponder Control configuration as defined in the approved design Panel data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by 10015660 AVIONICS SUPPORT GROUP, INC. EASA.IM.A.S.01637 FAA STC ST02763AT BOEING 757-200 BOEING 757-300 Installation of an In-Flight Cabin Video Surveillance System 10016116 AVIONICS SUPPORT GROUP, INC. EASA.IM.A.S.02307 FAA STC ST03071AT BOEING 727-200 Installation of Avionics System for Reduced Vertical Separation Minimum (RVSM) Provisions into a Boeing 727-200 aircraft. 10026764 AVIONICS SUPPORT GROUP, INC. P- EASA.IM.A.S.03249 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 be determined by the installer. FAA STC ST03700AT 747-400, 747-400F Installation of an International communications After Installation of this STC the operator is Group ICS-220A IridiumSATCOM System in a required to incorporatein the Airworthiness B747-400/-400F series aircraft in accordance Limitations Section of the Instructions withAvionics Support Group, Inc. Master Data forContinued Airworthiness applicable to the List 28546-MDL, Revision A,dated March 16, existing Maintenance Program adetailed 2009, or later FAA approved revisi inspection item at a threshold of 8400 Fl 16.03.2006 04.06.2007 1) Prior to installation of this modification 10.08.2009 the installer mustdetermine that the interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product. 2) The inst 10013962 AVIONIK STRAUBING ENTWICKLUNGS EASA.A.S.00646 GmbH REV. 1 Installation of single/dual Garmin GTX330D. 17.06.2008 10014031 AVIONIK STRAUBING ENTWICKLUNGS EASA.A.S.01097 PIPER PA-31 Installations of Avidyne FM850, 2x Garmin This STC is approved only for the product 26.10.2005 GmbH GTX330D Mode S Transponder and Garmin configuration as defined in the approved design GMA340 Marker/Audio data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 10014032 AVIONIK STRAUBING ENTWICKLUNGS EASA.A.S.01098 BEECH 300LW Installation of Mode S Transponder TDR94D 22.06.2005 GmbH with new Top Antenna. 10014089 AVIONIK STRAUBING ENTWICKLUNGS EASA.A.S.01185 CESSNA 501 Installation of Artex ELT C406-1. 28.04.2005 GmbH CESSNA 551 10014174 AVIONIK STRAUBING ENTWICKLUNGS EASA.A.S.01309 BEECH 65-90 Installation of Skywatch L3 SKY899, Radar 07.10.2005 GmbH BEECH 65-A90 BEECH 90 BEECH B90 BEECH C90 BEECH C90 A BEECH E90 RDR 2000 and EGPWS KGP 560 10014213 AVIONIK STRAUBING ENTWICKLUNGS EASA.A.S.01372 CESSNA 501 Installation of Dual Garmin GNS 430A 01.09.2005 GmbH CESSNA 551 10014273 AVIONIK STRAUBING ENTWICKLUNGS EASA.A.S.01507 GmbH BEECH 90 Installation of Avidyne FM850 18.08.2005 10014311 AVIONIK STRAUBING ENTWICKLUNGS EASA.A.S.01556 CESSNA 525 Installation of SKY497 and TAWS 8000The 21.06.2006 GmbH SKY497 is wired to the new Antenna, existing AM-250 Copilot Altimeter, i-linc MFD and Audio CTL. The TAWS 8000 is wired to theexisting MFD, KLN90B and ADC 200 10014340 AVIONIK STRAUBING ENTWICKLUNGS GmbH EASA.A.S.01598 CESSNA 550 Installation of CAS67A (incl. MST67A), Mark VIII, Kannad 406AF and Garmin GPS400 10014448 AVIONIK STRAUBING ENTWICKLUNGS EASA.A.S.02501 PIPER PA-46-310P Installation of GNS530, with GDC31 Roll GmbH Steering Converter 10014546 AVIONIK STRAUBING ENTWICKLUNGS EASA.A.S.02634 PIPER PA-31P Installation of COM/NAV/GS/GPS Garmin GmbH GNS530/GNS430 (dual installation) 10014566 AVIONIK STRAUBING ENTWICKLUNGS EASA.A.S.02667 PIPER PA34-200 Installation of dual Garmin GNS430 and Dittel GmbH PIPER PA34-200T PIPER PA34-220T FSG 2T in a Piper PA34. Certification Basis of the Change: CS 25, additionally AMC 20-4 (Basic R-Nav), AMC 20- 5 (GPS), JAA Leaflet No. 8, Rev. 2 (ACAS II),JAA Leaflet No. 12 (TAWS), JAA Leaflet No. 13 Rev. 1 (Mode-S ELS), JAA Leaflet No. 18 (Mode-S EHS) 1. Maximum operating altitude 18.000 ft2. GPS is not approved for TERM and APPR NAV3. This STC is approved only for the product configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with oth 04/01/2013 Page 101/462 11.04.2006 05.04.2006 11.09.2006 22.05.2006
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