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 10040249 JET AVIATION AG, ZURICH AIRPORT REV. 1 B200, B200C, B200GT, B200CGT ADS-B-OUT ComplianceOut: Dual Collins TDR-none Collins Pro Line 21 system & dual FMS- 11.09.2012 BRA B300, B300C 94D Transponder Mode S P/N 822-9210- 3000 & dual GPS-4000 008In: Dual Collins TDR-94D Transponder (EGNOScapable) are prerequisiteThe Mode S P/N 622-9210-409 & 1 approval holder shall fulfil the obligations dualannunciator/switch ADS-B 1/ADS-B 2 of Part 21, Paragraph21.A109.Prior to inhibit installation of this modification it must be determined thatthe interrelationsh 10040290 JET AVIATION AG, ZURICH AIRPORT BRA 10042873 JET AVIATION AG, ZURICH AIRPORT BRA 10013961 JET AVIATION FLUGZEUGWARTUNG GmbH 10013983 JET AVIATION FLUGZEUGWARTUNG GmbH 10014009 JET AVIATION FLUGZEUGWARTUNG GmbH 10014010 JET AVIATION FLUGZEUGWARTUNG GmbH 10014041 JET AVIATION FLUGZEUGWARTUNG GmbH 10014108 JET AVIATION FLUGZEUGWARTUNG GmbH 10014109 JET AVIATION FLUGZEUGWARTUNG GmbH 10014110 JET AVIATION FLUGZEUGWARTUNG GmbH 10014144 JET AVIATION FLUGZEUGWARTUNG GmbH 10014145 JET AVIATION FLUGZEUGWARTUNG GmbH 10014153 JET AVIATION FLUGZEUGWARTUNG GmbH 10014271 JET AVIATION FLUGZEUGWARTUNG GmbH 10014272 JET AVIATION FLUGZEUGWARTUNG GmbH 10014288 JET AVIATION FLUGZEUGWARTUNG GmbH 10014289 JET AVIATION FLUGZEUGWARTUNG GmbH B200, B200C, B200GT, B200CGT Mini Quick Access Recorder None The approval holder shall fulfil the 22.06.2012 B300, B300C (QAR)InstallationIn: Single or Dual Avionica obligations of Part 21, P/N 804-1205 miniQAR Mk III 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 B200, B200C, B200GT, B200CGT BARO-VNAV Temp. Comp. Activation & RF S/N: same as EASA TCDS with Rockwell Prior to the installation of this modification 21.12.2012 B300, B300C Legs Authorization Activation of Temperature Collins Proline 21 Avionics it must be determinedthat the Compensation on already approved APV interrelationship between this modification BARO-VNAVsystem and RF Legs and any otherpreviously installed Authorization (This functionality can be used in modification and/or repair will introduce the initial andintermediate approach segments, noadverse effect upon the airworthiness the final ph of the product. EASA.A.S.00645 LEARJET 55 Installation of Honeywell ACAS II CAS 67A and 1. FAA TCDS A10CE plus JAA TGL No 8 and 17.05.2005 Mode S XPDR MST 67A JAA TGL No 13 apply2. 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 EASA.A.S.01015 CESSNA 501-551 Installation of a Honeywell KTA 870 and ART2000 15.06.2005 EASA.A.S.01052 CESSNA 525- 525A Installation of a Dual MST 67A Mode S This STC is approved only for the product 13.06.2005 Transponder System. 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. EASA.A.S.01053 525 Installation of Dual Garmin GTX 330D Mode 17.11.2005 CESSNA 525A SAFM Supplement 2004-16-8 Revision A or later EASA approved RevisionMM Supplement 2005-16-10 Revision A or later EASA approved Revision EASA.A.S.01116 PA-42 SERIES Installation of Artex ELT 406. 23.06.2005 EASA.A.S.01213 CESSNA 650 Installation of SATCOM Universal TT-3000 16.11.2005 EASA.A.S.01214 CESSNA 650 Installation of Airshow Entertainer System Part 25 of the Federal Aviation Regulations effective February 1, 1965 as amended by Amendments 25-1 through 25-39; TGM JAA leafletNo. 17Weight and Balance Analysis, Report 2005-17-9, Rev. A 13.03.2006 EASA.A.S.01215 CESSNA 550-560-S550 Installation of ACAS II CAS 67A and Dual Mode - S Transponder RCZ-833 23.09.2005 EASA.A.S.01262 LEARJET 55 Installation of Secondary UNS 1F 23.06.2005 EASA.A.S.01263 LEARJET 55 Installation of ELT 406 29.06.2005 EASA.A.S.01274 GULFSTREAM ASTRA/SPX Upgrade of Universal UNS-1C to 1C+ 21.09.2005 EASA.A.S.01501 REV. 1 525, 525A Installation of Honeywell KMH 880 or KMH-980 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. 27.06.2011 EASA.A.S.01502 CESSNA 501 CESSNA 551 Installation of Honeywell RDS 84 WX System. 16.08.2005 EASA.A.S.01529 BEECH 1900 Installation of Universal Flight Manager System UNS-1L 25.01.2006 EASA.A.S.01531 BEECH 200 Installation of Universal Flight Management 24.10.2006 BEECH 200C System UNS-1L 04/01/2013 Page 292/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10014290 JET AVIATION FLUGZEUGWARTUNG GmbH EASA.A.S.01532 IAI ASTRA SPX Installation of Universal Cockpit Display System n/a 14.12.2005 10014297 JET AVIATION FLUGZEUGWARTUNG EASA.A.S.01541 BEECH 200 Installation of Universal Multifunction Display 31.08.2006 GmbH BEECH 200C BEECH B200 BEECH B200C MFD-640 10014299 JET AVIATION FLUGZEUGWARTUNG EASA.A.S.01543 ASTRA 1125 Installation of Collins TCAS 4000 Certification basis of the change: FAR Part 25, 28.08.2006 GmbH GULFSTREAM 100 additionally JAA Leaflet No. 8 Rev. 2 (ACAS II), JAA Leaflet No. 13 Rev. 1 (Mode S ELS), JAA Leaflet No. 18 (Mode S EHS) 10014300 JET AVIATION FLUGZEUGWARTUNG EASA.A.S.01544 WESTWIND ASTRA 1125 Installation of Garmin GNC 300XL Certification basis of the change: FAR Part 25, 28.08.2006 GmbH additionally EASA AMC 20-5 (GPS) 10014329 JET AVIATION FLUGZEUGWARTUNG EASA.A.S.01582 CESSNA 560 (CITATION V) Installation, Completion of custom Aircraft Ref. G-FM25004001 Rev. N/C: Limited to S/N 13.03.2006 GmbH Interior for BD700-1A10 Global Expressacc.: CDL D954000 Rev. KValidation of imported TCC STC: SA04-113 9145 10014345 JET AVIATION FLUGZEUGWARTUNG GmbH 10014346 JET AVIATION FLUGZEUGWARTUNG GmbH 10014351 JET AVIATION FLUGZEUGWARTUNG GmbH 10014366 JET AVIATION FLUGZEUGWARTUNG GmbH 10014370 JET AVIATION FLUGZEUGWARTUNG GmbH 10014374 JET AVIATION FLUGZEUGWARTUNG GmbH 10014457 JET AVIATION FLUGZEUGWARTUNG GmbH 10014458 JET AVIATION FLUGZEUGWARTUNG GmbH 10014541 JET AVIATION FLUGZEUGWARTUNG GmbH 10014553 JET AVIATION FLUGZEUGWARTUNG GmbH 10014647 JET AVIATION FLUGZEUGWARTUNG GmbH 10014726 JET AVIATION FLUGZEUGWARTUNG GmbH 10014741 JET AVIATION FLUGZEUGWARTUNG GmbH 10014742 JET AVIATION FLUGZEUGWARTUNG GmbH 10014922 JET AVIATION FLUGZEUGWARTUNG GmbH EASA.A.S.01608 BEECH 200 BEECH 200C BEECH B200 BEECH B200C EASA.A.S.01609 BEECH 200 BEECH 200C BEECH B200 BEECH B200C EASA.A.S.01616 LEARJET 35 LEARJET 35A EASA.A.S.01636 CESSNA 550 CESSNA 560 CESSNA S550 Installation of Blue Sky C-1000 SATCOM 31.08.2006 Installation of Universal TAWS 31.08.2006 Installation of Flight Data Recorder F1000 26.10.2005 Installation of Honeywell CAS 81 ACAS and MST 67A Mode-S XPDR EASA.A.S.01641 CONSTRUCCIONES C-212 Installation of CAS 67A ACAS II and dual MST 67A Mode-S XPDR EASA.A.S.01649 BEECH 300 BEECH 300LW BEECH B300 EASA.A.S.02511 CESSNA 525 CESSNA 525A EASA.A.S.02515 CESSNA 525 CESSNA 525A EASA.A.S.02628 LEARJET 35 LEARJET 35A Installation of Universal UNS-1L Softeware 802.XX 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. Instructions for Continued Airworthiness, Doc. No. 2005-33-10 Rev. B Installation of EGPWS MARK VIII Maintenance Manual Supplement 2005-9-10- Rev. B Installation of Skywatch HP Maintenance Manual Supplement 2005-10-10 Rev B Installation of Universal UNS 1L/K+ Certification Basis of the change: FAR Part 25, additionally EASA AMC 20-4 (B-RNAV), EASA AMC 20-5 (GPS), JAA TGL No. 10 Rev. 1 (P- RNAV) EASA.A.S.02651 PIPER PA-46-310P Installation of Garmin GTX 330 or Garmin GTX PIPER PA-46-350P 330D Transponder EASA.A.S.02802 LEARJET 35 Installation of Honeywell RDR 2000 and KMD LEARJET 35A 850. EASA.A.S.02903 CESSNA C650 Installation of Solid State Flight Data Recorder (SSFDR) F1000 EASA.A.S.02924 BEECH 1900 Installation of an Executive Power System Prior to installation of this modification the BEECH 1900C WET WING, (EPS) with Inverter and Power Outlet. installer must determine that the AIRLINER interrelationship between this modification and BEECH 1900D any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install EASA.A.S.02925 BEECH 1900 BEECH 1900C, AIRLINER BEECH 1900D Installation of a Satcom System for Passenger Communication. EASA.A.S.03169 CESSNA 650 CITATION III,VI,VII Installation of Honeywell CAS-67A and RCZ- 833 Mode S transponders. 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 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 04/01/2013 Page 293/462 14.11.2005 23.02.2006 13.07.2006 31.07.2006 28.07.2006 11.09.2006 27.04.2006 25.06.2007 04.05.2007 07.09.2007 07.09.2007 01.02.2008
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