04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
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<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10<strong>01</strong>5779 JET AVIATION AG, BASEL <strong>EASA</strong>.IM.A.S.<strong>01</strong>825 - GULFSTREAM 1159 (G-II) Weather Radar Installation -- 05.05.2006<br />
10034649 JET AVIATION AG, BASEL MF900 (EXCEPTED F900C) NZ2000 6.1 upgrade with CD820 CDU As per AFMS Doc. No. BF9003<strong>462</strong>3-2<strong>01</strong>-<strong>01</strong> Prior to installation of this modification it 18.<strong>04</strong>.2<strong>01</strong>1<br />
replacement.Existing dual or triple Honeywell Rev. IR dated 17.03.2<strong>01</strong>1.<br />
must be determined thatthe<br />
NZ2000 Flight Management System<br />
interrelationship between this modification<br />
isupgraded as follows:- NCU NZ2000 FMS<br />
and any other previouslyinstalled<br />
1&2 version NZ5.2 or later is replaced with<br />
modification and/ or repair will introduce<br />
versionNZ6.1 - CD800/CD810 1&2 CDU<br />
no adverse effectupon the airworthiness<br />
replaced with CD820.No cha<br />
of the product.<br />
10035212 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.03807 FALCON 900EX Activation of the Runway Awareness and<br />
Advisory System (RAAS) i.a.w. JetAviation<br />
Master Data List BF9EX34461-0<strong>01</strong><br />
10035406 JET AVIATION AG, BASEL FALCON 2000 Iridium antenna installation.Structural<br />
justification of the installation of an Aircell low<br />
profiledual patch antenna on top of the<br />
fuselage between frames 17 and 18.<br />
10039436 JET AVIATION AG, BASEL P-<strong>EASA</strong>.A.S.03778 REV. 1 A340-300 Airbus A340-300 "Olbia" VIP Cabin Interior<br />
Completion STC10039436Revision 1 to<br />
remove limitation<br />
10<strong>04</strong>0716 JET AVIATION AG, BASEL A319-115 VIP Cabin Interior Completion. See Master<br />
Data List BCJ03856-0<strong>01</strong>.<br />
10<strong>04</strong>2418 JET AVIATION AG, BASEL A319-115 Cabin Interior OutfittingSee Master Data List<br />
BCJ<strong>04</strong>353-0<strong>01</strong> Rev. C<br />
10<strong>01</strong>4941 JET AVIATION AG, ZURICH AIRPORT<br />
BRA<br />
10026896 JET AVIATION AG, ZURICH AIRPORT<br />
BRA<br />
10027723 JET AVIATION AG, ZURICH AIRPORT<br />
BRA<br />
10036985 JET AVIATION AG, ZURICH AIRPORT<br />
BRA<br />
<strong>EASA</strong>.A.S.03200 CESSNA 560 EHS integration into Aircraft.By upgrading both<br />
existing RCZ-833E to RCZ-833K and<br />
integrated Mode S Transponder Module XS-<br />
852A to XS-852F, with the Honeywell Service<br />
Bulletin No. 7510700-23-6<strong>04</strong>6.<br />
P-<strong>EASA</strong>.A.S.03967 HS 125 SERIES 700B Cockpit Voice Recorder InstallationBy installing<br />
a new L3 FA2100 Cockpit Voice Recorder<br />
(CVR)<br />
525 / 525A / 525B MINIQAR installation; By installing an Avionica<br />
miniQAR MK II and the MKIII according to the<br />
Installation Instructions OPM-009.<br />
CESSNA 525 Removed Equipment:-Aerosonic VSI #1 & #2-<br />
Skywatch 497 TCAS I SystemNew installed<br />
equipment:-Honeywell TA/VSI Indicator #1 &<br />
#2-PS-578A XPDR/TCAS Control HeadCAS-<br />
67A TCAS II System<br />
1.,,Prior to installation of this modification the<br />
installer mustdetermine that the<br />
interrelationship between this modification and<br />
anyother previously installed modification will<br />
introduce no adverse effectupon the<br />
airworthiness of the product.2.,,The ins<br />
Restricted to S/N 173This approval only covers<br />
the structural installation of the<br />
antenna.Installation and activation of any<br />
related Satcom system must bejustified and<br />
covered by another suitable approval.<br />
Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
none Airstairs installation is not part of the<br />
approved configuration.Prior to<br />
installation of this modification it must be<br />
determined thatthe interrelationship<br />
between this modification and any other<br />
previouslyinstalled modification and/ or<br />
repair will introdu<br />
Approval valid only for MSN 3856. The aircraft<br />
is certified for private use only, not to be<br />
operated forcommercial air transport. The<br />
aircraft is a No Smoking aircraft. For other<br />
Limitations refer to Airplane Flight Manual<br />
SupplementBCJ03856-2<strong>01</strong>-<strong>01</strong> Rev. C<br />
Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
08.07.2009<br />
21.06.2<strong>01</strong>1<br />
21.06.2<strong>01</strong>2<br />
23.07.2<strong>01</strong>2<br />
S/N: 4353 Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
30.11.2<strong>01</strong>2<br />
Ref.: \-\ S/N:\Prerequisit equipment:- IC-600<br />
CDG, P/N 7<strong>01</strong>7000-8<strong>01</strong>62- IC-600 CDG, P/N<br />
7<strong>01</strong>7000-81162- RCZ-833E ICU, P/N<br />
7510700-866- RM-850 RMU, P/N 7<strong>01</strong>2100-<br />
825- GNS-XL FMS, P/N 18355-<strong>01</strong><strong>01</strong>-<strong>01</strong><strong>01</strong>For<br />
aircrafts equipped with a CAS-67A TCAS II-<br />
08.10.2007<br />
TPU 67-A, P/N 066-<br />
None 1) Prior to installation of this modification 20.08.2009<br />
the installer mustdetermine that the<br />
interrelationship between this modification<br />
and anyother previously installed<br />
modification will introduce no adverse<br />
effectupon the airworthiness of the<br />
product. 2) The in<br />
S/N 525-0600 & ON, 525A-00<strong>01</strong> & ON, 525B-<br />
<strong>01</strong>35 & ON.<br />
Prior to installation of this modification the<br />
installer must determinethat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
26.10.2009<br />
S/N: 525-0322 F-HCPB<br />
product.<br />
none 24.10.2<strong>01</strong>1<br />
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