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 />
10030964 JET AVIATION AG BASEL P-<strong>EASA</strong>.A.S.03518 REV. 1 A319-115 Airbus A319-115 "BCJ03632" VIP Cabin None This certificate is granted under the <strong>04</strong>.08.2<strong>01</strong>0<br />
Interior CompletionRevision 1: Update of the<br />
commitment from the applicant tocomply<br />
Instructions for Continued Airworthiness<br />
with the post STC actions as referred to<br />
in Jet Aviation's letterref. "Commitments<br />
to Post STC actions" dated 16 July<br />
2<strong>01</strong>0.Prior to installation of this<br />
modification it must be de<br />
10032331 JET AVIATION AG BASEL B747-400 Replacement of a dual Allied Signal High none Prior to installation of this modification it 27.10.2<strong>01</strong>0<br />
Frequency (HF) Radio by dualRockwell Collins<br />
must be determined thatthe<br />
Air Transport (RCAT) HFS-900D HF Radio<br />
interrelationship between this modification<br />
equipment (ARINC753) with HF Data Link<br />
and any other previouslyinstalled<br />
activation in accordance with Jet Aviation<br />
modification and/ or repair will introduce<br />
MasterData List Doc. No. B7428343-006 Rev<br />
no adverse effectupon the airworthiness<br />
D, date<br />
of the product.<br />
10037000 JET AVIATION AG BASEL P-<strong>EASA</strong>.A.S.03714 B747-400 Installation of Cabin Interior Doors in<br />
accordance with Jet AviationMaster Data List<br />
BHHM10<strong>01</strong>-0<strong>01</strong> Rev. B, dated 19th October,<br />
2<strong>01</strong>1 forB747-400 S/N 28343<br />
10037425 JET AVIATION AG BASEL FALCON 2000EX Change consists in activating WLAN WiFi<br />
function of existing Satcom/LANrouter<br />
equipment.<br />
100375<strong>04</strong> JET AVIATION AG BASEL <strong>EASA</strong>.A.S.03322 REV. 2 B737-700 EMS SATCOM AMT-3800<br />
Installation:Installation option between<br />
STA.727E to STA.787 and STA.727B to<br />
STA.727E(Major change to <strong>EASA</strong> STC No.<br />
<strong>EASA</strong>.A.S.03322 Rev.1)<br />
10038393 JET AVIATION AG BASEL A319-133 VIP Cabin Interior CompletionSee Master Data<br />
List BCJ<strong>04</strong>151-0<strong>01</strong><br />
10039269 JET AVIATION AG BASEL P-<strong>EASA</strong>.A.S.03779 REV. 1 A340-600 Airbus A340-600 "Eminence" VIP Cabin<br />
Interior CompletionRevision 1 to remove<br />
limitations<br />
10039356 JET AVIATION AG BASEL A340-211, A340-212, A340-213<br />
A340-311, A340-312, A340-313<br />
10039357 JET AVIATION AG BASEL A340-211, A340-212, A340-213<br />
A340-311, A340-312, A340-313<br />
Camera Unit and Structural provision<br />
installationThis STC installs one camera on the<br />
tail of the aircraft, watchingforward. This covers<br />
the mechanical installation of the camera unit<br />
andthe penetration of the pressure.<br />
This aircraft is not eligible for registration in a<br />
European country,because it does not comply<br />
with the JAA Special Conditions 1 and 2.<br />
Aircraft must be fitted with Dassault Aviation<br />
M3196 that installscomplete Aircell Axxes II<br />
system, including WiFi antennas.<br />
Prior to installation of this modification it 24.10.2<strong>01</strong>1<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 />
Prior to the installation of this modification 25.11.2<strong>01</strong>1<br />
it must be determinedthat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification and/or repair will introduce<br />
noadverse effect upon the airworthiness<br />
of the product.<br />
None. None. 02.12.2<strong>01</strong>1<br />
Approval valid only for MSN 4151.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 />
SupplementBCJ<strong>04</strong>151-2<strong>01</strong>-<strong>01</strong> Rev. B or<br />
Prior to installation of this modification it 15.02.2<strong>01</strong>2<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 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 />
11.05.2<strong>01</strong>2<br />
None. 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.<strong>04</strong>.2<strong>01</strong>2<br />
Tailwind 550/560 antenna installationThis STC None. Prior to installation of this modification it 30.<strong>04</strong>.2<strong>01</strong>2<br />
installs a tailwind SAT TV antenna and radome<br />
must be determined thatthe<br />
on top of thefuselage.<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 />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 286/<strong>462</strong>
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