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 />
10039715 JET AVIATION AG BASEL FALCON 2000 WLAN activationFor WLAN working in the 2.4<br />
Prior to installation of this modification it 24.05.2<strong>01</strong>2<br />
GHz frequency band<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 />
10<strong>04</strong><strong>01</strong>66 JET AVIATION AG BASEL 737-800 Iridium Antenna Structural Provisionsbetween<br />
fuselage station BS 727C & 727D<br />
10<strong>04</strong>0780 JET AVIATION AG BASEL B737-800 Forward VIP Lavatory reconfiguration- new<br />
shower system- relocation of handspray<br />
system- new vanity light system- new shower<br />
light system- new pax sign inside shower-<br />
adaptation of existing systems<br />
10<strong>04</strong>0974 JET AVIATION AG BASEL A330-2<strong>01</strong>, - 202, - 203<br />
A330-223, -243<br />
EMS Satcom AMT-3800 antenna<br />
installation.This modification installs EMS<br />
Satcom AMT-3800 high gain antenna,Diplexer<br />
Low Noise Amplifier, and associated structural<br />
provision.<br />
10<strong>04</strong>1576 JET AVIATION AG BASEL FALCON 10 Exchange to Universal Avionics FMS UNS-<br />
1LwOut: Universal Avionics FMS UNS-1Msp<br />
systemIn: Universal Avionics FMS UNS-1Lw<br />
system<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 />
26.06.2<strong>01</strong>2<br />
S/N: 33473 (A6-AUH) 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 />
26.07.2<strong>01</strong>2<br />
This STC approval has been granted for 100 Prior to installation of this modification it 10.08.2<strong>01</strong>2<br />
Flight Cycle (FC) or 6months, counted from the must be determined thatthe<br />
STC approval date, whichever occurred first. 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 />
S/N: 216 The approval holder shall fulfill the<br />
obligations of Part 21,Paragraph<br />
21.A109.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
10<strong>04</strong>1595 JET AVIATION AG BASEL B737-900ER EMS SATCOM AMT-3800 Installation. Approval valid only for S/N: 37560 This STC has been assessed for<br />
compatibility for installation on thesubject<br />
aircraft, which is equipped for lower cabin<br />
altitude under FAASTC ST<strong>01</strong>697SE.<br />
However, <strong>EASA</strong> has not yet approved<br />
the lower cabinaltitude STC. Therefore, if<br />
this aircraft is to be en<br />
<strong>01</strong>.10.2<strong>01</strong>2<br />
10<strong>04</strong>16<strong>04</strong> JET AVIATION AG BASEL REV. 1 B737-900ER VIP Cabin interior installation.Installation of<br />
table leaf adjacent to RH over-wing exit.See<br />
Master Data List BBJ37560-0<strong>01</strong> Rev. C (or<br />
later approved revision).<br />
28.09.2<strong>01</strong>2<br />
S/N: 37560 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 />
05.11.2<strong>01</strong>2<br />
10<strong>04</strong>2850 JET AVIATION AG BASEL REV. 1 GV-SP MDL BDBMW002-0<strong>01</strong> Rev. IR S/N: 5336 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 />
21.12.2<strong>01</strong>2<br />
10<strong>01</strong>4526 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.02611 B727-200 ADI/ HIS & FMS upgrade by:removing both<br />
existing 329B-8x ADI 329Bremoving both<br />
existing 331A-9G HISremoving both LTN-92<br />
CDUremoving both ALI 55B Radio Altimeter<br />
Indicatorsinstalling two new 5ATI E-ADI, p/n<br />
195000-21installing two new ATI E-HIS, p/n<br />
195000-<br />
Reg.: A9C-BA, S/N 21824. Valid for this serial<br />
number only.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 287/<strong>462</strong><br />
<strong>04</strong>.09.2007
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