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 10016169 ELISEN TECHNOLOGIES EASA.IM.A.S.02396 TCCA STC SA07-21 BOMBARDIER CL-600-2B19 Towbar Stowage, Project No. 29R2-708. 03.07.2007 10016170 ELISEN TECHNOLOGIES EASA.IM.A.S.02397 TCCA STC SA07-22 BOMBARDIER CL-600-2B19 Equipment Bay Forward Catwalk, Project No. 29R2-709. 03.07.2007 10016171 ELISEN TECHNOLOGIES EASA.IM.A.S.02398 TCCA STC SA07-23 BOMBARDIER CL-600-2B19 Equipment Bay Stowage Box, Project No. Prior to installation of this modification the 04.07.2007 29R2-710. 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 10016310 ELISEN TECHNOLOGIES EASA.IM.A.S.02612 TRANSPORT CANADA STC NO. SA07- BOMBARDIER CL-600-2B19 Lockable Fuels Caps. 21.11.2007 10015349 ELLIOTT AVIATION EASA.IM.A.S.00503 REV. 1 FAA STC SA01352CH BEECH 200 Installation of Dual TDR-94D Transponders 1. Limited to Aircraft equipped with Raytheon 06.03.2006 BEECH 200C with Flight ID in B200/B200C/B300/B300C Aircraft Company "Collins Pro Line 21 Avionics BEECH 200CT Aircraft with Pro Line 21 Avionics, in Suite" major change2. Limited to BEECH 200T accordancewith Configuration 3 of Elliott Configuration 3 of Elliott Aviation FAA STC BEECH 300 Aviation Master Data List, No 2026-576DL, SA01352CH3. This STC is approved only for BEECH 300LW BEECH B200 BEECH B200C BEECH B200CT BEECH B200T BEECH B300 BEECH B300C Revision 2 or later approved revision. the product configuration as define 10015683 ELLIOTT AVIATION EASA.IM.A.S.01667 FAA STC ST02007CH BEECH 400 Certification for Reduced Vertical Separation 1. This STC is approved only for the product 24.01.2006 BEECH MU-300 Minimum (RVSM) operational capability and configuration as defined in the approved design BEECH MU-300-10 installation of Honeywell AZ-252 Air Data data referred to in the paragraph "Description". Computer and AM-250 Altimeter with optional Compatibility with other aircraft/engine BA-250 Altitude Indicator and AL-800 Altitude configurations shall be determined by the Preselector installer.2. Certification basi 10015693 ELLIOTT AVIATION EASA.IM.A.S.01681 FAA STC ST01486CH BEECH 400 BEECH MU-300 BEECH MU-300-10 Installation of a Honeywell Mark VI/VIII EGPWS Validation Basis of the Change: FAR 25, additionally JAA Leaflet No. 12 (TAWS) 10015716 ELLIOTT AVIATION EASA.IM.A.S.01713 ST02194CH FALCON 10 ST02194CH: Installation of UNS EFI-890R EFIS Certification basis iaw CRI A1 IM.A.S.01713 13.02.2007 10015721 ELLIOTT AVIATION EASA.IM.A.S.01720 FAA STC ST01666CH FALCON 10 ST01666CH: Installation of a Rockwell Collins 1. Certification basis iaw CRI A1 IM.A.S.01720 13.02.2007 TCAS 4000Traffic Alert and Collission Avoidance System (TCAS II) and TGL Nr. 8 10015757 ELLIOTT AVIATION EASA.IM.A.S.01791 FAA STC SA02206CH BEECH 200 Installation of Honeywell Digital Flight Data Limited to the aircraft types listed above with 03.03.2006 BEECH 200C BEECH 200CT BEECH 200T BEECH 300 BEECH 300C Recorder System (DFDR) Proline 21 Avionics Suite installed. 10015894 ELLIOTT AVIATION EASA.IM.A.S.02014 FAA STC SA02264CH BEECH 300 Airworthiness certification of Reduced Vaertical None 09.11.2006 BEECH 300LW seperation Minimum (RVSM) and installation of BEECH B200 BEECH B200C BEECH B200CT BEECH B300 BEECH B300C Air Data Systems 10015976 ELLIOTT AVIATION EASA.IM.A.S.02128 FAA ST5990CH-T FALCON 10 ST02333CH: Installation of a Universal Avionics SystemsCorporation(UASC) UNS- 1K+/L FLIGHT MANAGEMENTSYSTEM (FMS), Dual Universal Avionics Radio ControlUnits (RCU), and/or dual Rockwell Collins VIR-32Navigation Receiver 1. Certification basis FAR 25 Amdt 117 13.02.2007 10015978 ELLIOTT AVIATION EASA.IM.A.S.02130 SA01216CH BEECH 200 Installation of Honeywell (Allied Signal) MK-VI 1. Compatibility of this design change with 24.08.2006 BEECH 200C Enhanced Ground Proximity Warning System, previously approved modifications must be BEECH 200CT Universal Avionics Systems Corporation determined by the installer.2. Airplane Flight BEECH 300 Terrain Awareness Warning System and Manual Supplement, Elliott Aviation Report No. BEECH 300LW Universal Avionics Systems Multifunction EGPWS-FMS Rev 1, FAA approved August BEECH B200 BEECH B200C BEECH B200CT BEECH B200T BEECH B300 BEECH B300C Display 23, 2000, or later FAA approved revisio 04/01/2013 Page 204/462 19.07.2006
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016252 ELLIOTT AVIATION EASA.IM.A.S.02529 FAA STC SA02447CH BEECH 200 Installation of a Rockwell Collins IFIS-5000 27.02.2008 BEECH 200C BEECH 200CT BEECH 200T BEECH 300 BEECH 300C Integrated Flight Information system. 10016254 ELLIOTT AVIATION EASA.IM.A.S.02532 FAA STC ST02431CH FALCON 10 EASA Validation of FAA STC The aircraft must be equipped with Universal 13.05.2008 ST02431CHEASA Validation is limited to Avionics EFI-890R Electronic Flight Instrument Provisions for Installation of a Universal System (EFIS) as installed by Elliott Aviation’s Avionics Application Server Unit (ASU) on STC EASA.IM.A.S.01713.This EASA Approval Falcon 10 is limited to provisions for installation only with the ASU System deactiv 10016474 ELLIOTT AVIATION EASA.IM.A.S.02822 FAA STC ST02548CH FALCON 10 EASA Validation of FAA STC ST02548CHInstallation of an International Communications Group ICS-120 Iridium Satellite Telephone 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 10016475 ELLIOTT AVIATION EASA.IM.A.S.02823 FAA STC ST02547CH FALCON 10 EASA Validation of FAA STC Prior to installation of this modification the ST02547CHInstallation of a Universal Avionics installer must determine that the Systems Corporation UL-701 UniLink System interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install 10029872 ELLIOTT AVIATION FAA STC STC02784CH BEECHJET 400/400A Installation of Honeywell Digital Flight Data None Prior to installation of this modification it 28.04.2010 RecorderValidation of FAA STC STC02784CH 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. 10029873 ELLIOTT AVIATION FAA STC STC02783CH BEECHJET 400 Installation of an Artex C406-2 Emergency Locator Transmitter (ELT)Validation of FAA STC STC02783CH 10015890 EMBRAER - EMPRESA BRASILEIRA EASA.IM.A.S.02009 CTA STC2006S02-09 EMBRAER EMB-135BJ CTA STC2006S02-09 "Installation of a 30' 1. Limited to EMB-135BJ SN 145000802. LCD monitor and Playstation Entertainment Instructions for Continued Airworthiness Report System iaw Avionic Services master drawing No. 135-23-0008 Rev. 0 dtd. 9. Sep. 05 or list 135-23-001 Rev. D dtd. 28. Nov. 05 or later later accepted revision.2. This STC is approved revision approved only for the product configuration as defined in the approved design data 10027373 EMBRAER - EMPRESA BRASILEIRA P- EASA.IM.A.S.03273 ANAC STC 2009S05-14 EMB-500 Installation of a Honeywell HF Communications System, Model KHF-1050 andoptionally the Avtech Corporation SELCAL decoder, Model CSD-714. 10038234 EMBRAER GPX Ltda. (PC 722) REV. 1 EMB-135BJ/LR/ER EASA Validation of ANAC STC 2010S10-18. EMB-145 Electronic Flight Bag EMB-145ER/EU/EP/MP/LR/LU/MK (EFB)Installation.Description as per:ESCMSC002-Rev A, dated 17th January 2012.Master Documents List ESCCCD003- Rev B, dated 17th January 2012. 10038291 EMBRAER GPX Ltda. (PC 722) EMB-135BJ EASA validation of ANAC STC N°2011S09- 02Installation of a cabinet and a 17'' video monitor on EMB-135BJ aircraft 26.05.2008 26.05.2008 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. 28.04.2010 Required Markings and Placards:-.In close proximity to the 5A breaker in panel LH circuit breaker "HFPWR". In close proximity to the 30A breaker in circuit breaker of LPDU "HFAMPL". (If applicable) In close proximity to the 5A breaker in panel LH circuitbr Prior to installation of this modification the installer must determinethat the interrelationship between this modification and any otherpreviously installed modification will introduce no adverse effect uponthe airworthiness of the 23.01.2007 25.09.2009 None product.The installatio None 01.02.2012 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. 03.02.2012 04/01/2013 Page 205/462
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04/01/2013 Page 1/462 - EASA

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