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>4555 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.02653 BAE 146/AVRO 146 SERIES Cabin Interior Outfitting:Introducing a custom 1. Reg.: A6-RJK S/N: E1267.2. For<br />
12.<strong>04</strong>.2007<br />
passenger cabin with individual interior and limitations refer to Flight Manual Supplement<br />
seating, VIP lavatory, In-flight Entertainment /<br />
Cabin ManagementSystem w/ tail and cockpit<br />
camera, Iridium Satcom system, cabin poweroutlet<br />
system and oxygen ove<br />
BRJE1267-2<strong>01</strong>-<strong>01</strong>.<br />
10<strong>01</strong>4576 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.02681 BOEING 727-200 Cabin interior modification:According to the<br />
description in the Certification Plan, Doc. No.<br />
BACBA008-1.<br />
Reg.: A9C-BA, S/N: 218424Approval limited to<br />
S/N 21824 only.<br />
10<strong>01</strong>4613 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.02740 BOEING 737-100 SERIES Cabin ModificationGalley installation in the LH 1. Approval valid only for s/n 32774 with FAA-<br />
FWD Entrance AreaHigh Cabinet installation in STC No. ST09981SC installed;2. This STC<br />
the FWD RH Cabin<br />
is approved only for the product configuration<br />
as defined in the approved design data<br />
referred to in the paragraph "Description".<br />
Compatibility with other aircraft/<br />
10<strong>01</strong>4630 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.02770 AIRBUS A319-115 Cabin interior outfittingsee Master Data List<br />
BA3192949-0<strong>01</strong><br />
Limited to S/N 2949. 19.07.2007<br />
10<strong>01</strong>4644 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.02796 AIRBUS A319-100 Installation Of Additional Water Tank 24.<strong>04</strong>.2007<br />
10<strong>01</strong>4652 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.02807 MYSTERE FALCON 900 Wireless Access Service Point (WASP) 1. Applicable for S/N 109 only;2. This STC<br />
is approved only for the product configuration<br />
as defined in the approved design data<br />
referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined b<br />
29.09.2006<br />
10<strong>01</strong>4659 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.02816 BOEING 737-700 IGW Wireless LAN (WLAN) Activation This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
10<strong>01</strong>4738 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.02921 MYSTERE FALCON 50 MK-V EGPWS upgrade. 1. Required Avionics Configuration:• Collins<br />
ProLine II• Collins EFIS 84/85/86• Collins<br />
WXP 8502. This STC is approved only for<br />
the product configuration as defined in the<br />
approved design data referred to in the<br />
paragraph "Description". Compati<br />
10<strong>01</strong>4750 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.02935 BOEING 727-200 Activation of RAAS on MK-V or MK-VII<br />
EGPWS with Softwareversion -218-218 or<br />
higher up to -226-226<br />
10<strong>01</strong>4859 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.03083 BOMBARDIER BD-700-1A10 W-LAN Activation.By installing:A swivel dipole<br />
antenna in the cabin, a WLAN ON/OFF switch<br />
and new wiring between the router, antenna<br />
and the HD-710.<br />
10<strong>01</strong>4868 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.03092 AIRBUS A319-115 Wireless Local Area Network (WLAN)<br />
Activation.The modification includes the<br />
following:The antenna will be connected and<br />
the WLAN will be activated.A "WLAN OFF"<br />
switch will be installed to switch the Wireless<br />
LAN functionality 'on' and 'off'.<br />
S/N 21824 as initial installationSTC Valid for<br />
B727-200 Series with EGPWS MK-V or MK-<br />
VII with Softwareversion -218-218 or higher up<br />
to -226-226<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
10<strong>01</strong>4888 JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.03117 AIRBUS A319-115 Water Tanks Installation/The modification Prior to installation of this modification the<br />
includes the following:Installation of two installer must determine that the<br />
additional water tanks in the AFT lower lobe interrelationship between this modification and<br />
area between frame FR62 and frame FR65 on any other previously installed modification will<br />
the LH and RH side.<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
10<strong>01</strong>49<strong>04</strong> JET AVIATION AG, BASEL <strong>EASA</strong>.A.S.03139 GULFSTREAM III Super FMS Installation by:Removing the<br />
existing dual UNS-1Msp Flight Management<br />
System (FMS)and Install a new dual UNS-1L<br />
Super Flight Management System (FMS)a<br />
DTU-100 Data Transfer Unit.<br />
22.03.2007<br />
16.11.2006<br />
15.11.2006<br />
<strong>04</strong>.<strong>01</strong>.2007<br />
14.03.2007<br />
06.11.2007<br />
13.08.2007<br />
14.09.2007<br />
Reg.: TJ-AAW S/N 486Valid for this S/N only. 05.03.2008<br />
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