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 10015444 JET AVIATION AG, BASEL EASA.IM.A.S.01185 - AIRBUS A319-115 Cabin interior outfitting Approval valid for S/N 2507 onlyThe aircraft is certified for private use only. It is prohibited to operate the aircraft for hire or offered for common carriage. The aircraft is a NO SMOKING aircraft. For other limitations, see flight manual supplement BCJ 20.12.2005 10015446 JET AVIATION AG, BASEL EASA.IM.A.S.01187 - LEARJET 31 LEARJET 31A LEARJET 35 LEARJET 35A LEARJET 36 LEARJET 36A LEARJET 55 LEARJET 55B LEARJET 55C LEARJET 60 10015463 JET AVIATION AG, BASEL EASA.IM.A.S.01210 - BOMBARDIER CL-600-1A11 (CL- 600 Activation of the Runway Awareness and Advisory System (RAAS). Flight Management System (FMS) Upgrade & Terrain Awareness Warning System (TAWS) Installation 1. 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. 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. 10015548 JET AVIATION AG, BASEL EASA.IM.A.S.01439 - MYSTERE FALCON 50 Installation of a Honeywell MK VII EGPWS none 15.11.2005 10015607 JET AVIATION AG, BASEL EASA.IM.A.S.01543 - MYSTERE FALCON 50 GPWS upgrade to EGPWS This STC is limited to Falcon 50 S/N 204. 17.08.2005 10015661 JET AVIATION AG, BASEL EASA.IM.A.S.01638 REV 1 FALCON 900 1. FMZ-2000 Software Upgrade;2. Prior to installation of this modification the 22.08.2008 Application of Honeywell Service Bulletin No. installer must determine that the 7018879-34-A6060. interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install 10015689 JET AVIATION AG, BASEL EASA.IM.A.S.01674 - GULFSTREAM IV Installation of a L3 F2100 Solid State Flight Data Record (FDR) and Teledyne Mini Flight Data Acquisition Unit 10015722 JET AVIATION AG, BASEL EASA.IM.A.S.01724 - AIRBUS A320-232 Cabin Interior OutfittingSee Master Data List B3202403-001 1. Limited to Gulfstream IV (S/N. 1011 - A6- HHH) 1. Approval valid only for MSN 2403.2. The aircraft is certified for private use only, not to be operated for commercial air transport.3. The aircaft is a No Smoking aircraft.4. The W-LAN System is limited to Cabin W-LAN, 10015729 JET AVIATION AG, BASEL EASA.IM.A.S.01748 BOEING 737-700 IGW Cabin Modification - Aft Lounge Modification - wich is not interfaced Approval valid only for MSN 28976 with FAA Replacement of IFE/CMS and Installation of Airshow 4000 STC No. ST09106AC-D installed 10015752 JET AVIATION AG, BASEL EASA.IM.A.S.01785 - BOEING 737-800 Installation of modified customized seats 1. Modification limited to Aircraft S/N 334732. 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 dete 10015769 JET AVIATION AG, BASEL EASA.IM.A.S.01808 - FALCON 2000 Cabin Reconfiguration Modification limited to Aircraft S/N 076 09.02.2006 10015774 JET AVIATION AG, BASEL EASA.IM.A.S.01818 - AIRBUS A320-111 CAIR TM System Installation The aircraft maximum number of passengers is 30.08.2006 AIRBUS A320-211 AIRBUS A320-212 AIRBUS A320-214 AIRBUS A320-231 AIRBUS A320-232 AIRBUS A320-233 reduced by 7 (seven) passengers. 10015775 JET AVIATION AG, BASEL EASA.IM.A.S.01819 REV 1 AIRBUS A319-111 Cameras InstallationSee Master Data List Prior to installation of this modification the 10.09.2007 AIRBUS A319-112 BA32023391-001 installer must determine that the AIRBUS A319-113 interrelationship between this modification and AIRBUS A319-114 any other previously installed modification will AIRBUS A319-115 introduce no adverse effect upon the AIRBUS A319-131 AIRBUS A319-132 AIRBUS A319-133 AIRBUS A320-111 AIRBUS A320-211 AIRBUS A320-212 AIRBUS A320-214 AIRBUS A320-231 AIRBUS A320-232 AIRBUS A320-233 airworthiness of the product. The install 04/01/2013 Page 290/462 30.05.2005 25.07.2005 15.11.2005 06.09.2006 15.11.2006 30.01.2006
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015779 JET AVIATION AG, BASEL EASA.IM.A.S.01825 - GULFSTREAM 1159 (G-II) Weather Radar Installation -- 05.05.2006 10034649 JET AVIATION AG, BASEL MF900 (EXCEPTED F900C) NZ2000 6.1 upgrade with CD820 CDU As per AFMS Doc. No. BF90034623-201-01 Prior to installation of this modification it 18.04.2011 replacement.Existing dual or triple Honeywell Rev. IR dated 17.03.2011. must be determined thatthe NZ2000 Flight Management System interrelationship between this modification isupgraded as follows:- NCU NZ2000 FMS and any other previouslyinstalled 1&2 version NZ5.2 or later is replaced with modification and/ or repair will introduce versionNZ6.1 - CD800/CD810 1&2 CDU no adverse effectupon the airworthiness replaced with CD820.No cha of the product. 10035212 JET AVIATION AG, BASEL EASA.A.S.03807 FALCON 900EX Activation of the Runway Awareness and Advisory System (RAAS) i.a.w. JetAviation Master Data List BF9EX34461-001 10035406 JET AVIATION AG, BASEL FALCON 2000 Iridium antenna installation.Structural justification of the installation of an Aircell low profiledual patch antenna on top of the fuselage between frames 17 and 18. 10039436 JET AVIATION AG, BASEL P-EASA.A.S.03778 REV. 1 A340-300 Airbus A340-300 "Olbia" VIP Cabin Interior Completion STC10039436Revision 1 to remove limitation 10040716 JET AVIATION AG, BASEL A319-115 VIP Cabin Interior Completion. See Master Data List BCJ03856-001. 10042418 JET AVIATION AG, BASEL A319-115 Cabin Interior OutfittingSee Master Data List BCJ04353-001 Rev. C 10014941 JET AVIATION AG, ZURICH AIRPORT BRA 10026896 JET AVIATION AG, ZURICH AIRPORT BRA 10027723 JET AVIATION AG, ZURICH AIRPORT BRA 10036985 JET AVIATION AG, ZURICH AIRPORT BRA EASA.A.S.03200 CESSNA 560 EHS integration into Aircraft.By upgrading both existing RCZ-833E to RCZ-833K and integrated Mode S Transponder Module XS- 852A to XS-852F, with the Honeywell Service Bulletin No. 7510700-23-6046. P-EASA.A.S.03967 HS 125 SERIES 700B Cockpit Voice Recorder InstallationBy installing a new L3 FA2100 Cockpit Voice Recorder (CVR) 525 / 525A / 525B MINIQAR installation; By installing an Avionica miniQAR MK II and the MKIII according to the Installation Instructions OPM-009. CESSNA 525 Removed Equipment:-Aerosonic VSI #1 & #2- Skywatch 497 TCAS I SystemNew installed equipment:-Honeywell TA/VSI Indicator #1 & #2-PS-578A XPDR/TCAS Control HeadCAS- 67A TCAS II System 1.,,Prior to installation of this modification 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 ins Restricted to S/N 173This approval only covers the structural installation of the antenna.Installation and activation of any related Satcom system must bejustified and covered by another suitable approval. 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. none Airstairs installation is not part of the approved configuration.Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introdu Approval valid only for MSN 3856. The aircraft is certified for private use only, not to be operated forcommercial air transport. The aircraft is a No Smoking aircraft. For other Limitations refer to Airplane Flight Manual SupplementBCJ03856-201-01 Rev. C 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. 08.07.2009 21.06.2011 21.06.2012 23.07.2012 S/N: 4353 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. 30.11.2012 Ref.: \-\ S/N:\Prerequisit equipment:- IC-600 CDG, P/N 7017000-80162- IC-600 CDG, P/N 7017000-81162- RCZ-833E ICU, P/N 7510700-866- RM-850 RMU, P/N 7012100- 825- GNS-XL FMS, P/N 18355-0101-0101For aircrafts equipped with a CAS-67A TCAS II- 08.10.2007 TPU 67-A, P/N 066- None 1) Prior to installation of this modification 20.08.2009 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 in S/N 525-0600 & ON, 525A-0001 & ON, 525B- 0135 & ON. 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 26.10.2009 S/N: 525-0322 F-HCPB product. none 24.10.2011 04/01/2013 Page 291/462
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04/01/2013 Page 1/462 - EASA

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