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>4193 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>335 BOEING MD 11<br />
Navigation - ATC system, Installation of<br />
29.06.2005<br />
BOEING MD 11F<br />
Upgrade for Enhanced Surveillance and<br />
associated Airplane Flight Manual Supplement.<br />
10<strong>01</strong>4196 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>338 BOEING 737-300<br />
BOEING 737-400<br />
BOEING 737-500<br />
Navigation - Introduction of ATC Mode S<br />
Enhanced Surveillance<br />
10<strong>01</strong>4216 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>377 BOEING 737-300 "Avionics Upgrade by- Installation of TCAS-<br />
Installation of Dual Mode S Transponder-<br />
Installation of Add. Parameters for Digital FDR-<br />
Digital Flight Data Acquisition Unit, Software<br />
Upgrade- Installation of Enhanced Ground<br />
Proximity Warning System"<br />
10<strong>01</strong>4218 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>379 AIRBUS A340-600 "Installation of Antenna and Receiver Transmit "The IEEE 802.11 a,b,g (as customized)<br />
System and Network Services". Acc.: STDD Wireless Local Area Network (WLAN)<br />
00-<strong>04</strong>/10M. Ref. to former LBA STCs: TA0810 introduced by this midification, may be<br />
and TA0811. AFM Suppllement: A-34-05/260- activated on board Airbus A340-600 Aircraft<br />
AFM. ICA: R-00-<strong>04</strong>/120<br />
for operation with commercial IEEE 802.11a,<br />
b, g & h compliant WLAN enabled portable<br />
electronic de<br />
10<strong>01</strong>4225 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>388 AIRBUS A320<br />
AIRBUS A321<br />
ATC, System Upgrade for Enhanced<br />
Surveillance, acc.: STDD 34-05/06M<br />
1. 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>4227 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>390 AIRBUS A330-300 Integration of Lower Deck Mobile Crew Rest 14.07.2005<br />
10<strong>01</strong>4228 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>391 AIRBUS A340-300 Integration of Lower Deck Mobile Crew Rest 14.07.2005<br />
10<strong>01</strong>4246 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>456 BOEING 767-300 ATC, System Upgrade for EHS Certification Basis of the Change: CS 25<br />
Change 0, additionally JAA Leaflet No 18<br />
(Mode-S EHS)<br />
10.<strong>04</strong>.2006<br />
10<strong>01</strong>4256 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>483 REV. 1 FOKKER F.28 MARK 0070 Installation of non-electrical Floor Path Marking<br />
14.09.2<strong>01</strong>2<br />
FOKKER F.28 MARK <strong>01</strong>00 System Guideline®<br />
10<strong>01</strong>4257 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>486 REV 1 AIRBUS A330-200<br />
Structural mounting provision for large antenna 1. <strong>EASA</strong> CS25, without Amendment,<br />
08.12.2006<br />
AIRBUS A330-300<br />
and random for Live TV Tailwind 560 Certification Specifications for Large<br />
Aeroplanes plus FAA Generic Issue Paper A-X<br />
"Structural Certification Criteria for Large<br />
Antenna Installations".2. This STC is approved<br />
only for the product configuration as defined in<br />
10<strong>01</strong>4258 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>487 AIRBUS A330-200<br />
AIRBUS A330-300<br />
Communication - Modification/Upgrade of the<br />
In-Flight Entertainment System, Installation of<br />
Tailwing 560 Live TV Equipment.<br />
<strong>EASA</strong> CS25, without Amendment,<br />
Certifications Specifications for Large<br />
Aeroplanes plus JAA INT/POL/25/3 Issue 2,<br />
JAA INT/POL/25/4 Issue 3, JAA Leaflet No.<br />
10<strong>01</strong>4260 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>488 REV 1 BOEING 777-200<br />
17.<br />
Rearrangement of VIP cabin interior (Majlis) & 1.This modification is limited to a/c serial<br />
systems and modification of pax entertainment number MSN29271.2. Occupancy of this zone<br />
system (IFE) including installation oftailwind is limited to Zero Passengers for Taxi, Take-off<br />
560 Live TV system.<br />
and Landing, pending substantiation of<br />
evacuation through the adjacent compartments<br />
10<strong>01</strong>4261 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>489 BOEING 777-200 Introduction of Tailwind 550 Antenna and Live This modification is limited to a/c serial number<br />
TV for VIP B777-200.<br />
MSN29271.<br />
10<strong>01</strong>4262 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>490 AIRBUS A300 ATC, System Upgrade for EHS Certification Basis of the Change: CS 25,<br />
additionaly JAA Leaflet No. 18 (Mod-S EHS)<br />
10<strong>01</strong>4269 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>498 BOEING 737-700 IGW Cabin and IFE Modification as defined in<br />
Supplemental Type Definition<br />
DocumentSTDD00 - 05/05 M, Issue <strong>01</strong>,<br />
Rev.00<br />
10<strong>01</strong>4281 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>518 BOEING 737-600 SERIES<br />
BOEING 737-700 SERIES<br />
BOEING 737-800 SERIES<br />
BOEING 737-900 SERIES<br />
Installation of Guideline-non-electrical Floor<br />
Path Marking System.<br />
10<strong>01</strong>4282 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>519 BOEING 747-400 VVIP Cabin InstallationSTDD 25-05 / 06M<br />
issue 1, STDD 25-05 / 19 issue1<br />
-- 19.10.2006<br />
10<strong>01</strong>4283 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>520 BOEING 757-300 Installation of Zonal Drying System 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 />
06.11.2007<br />
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26.07.2005<br />
<strong>01</strong>.09.2005<br />
12.08.2005<br />
22.07.2005<br />
07.<strong>04</strong>.2006<br />
12.06.2008<br />
29.06.2006<br />
13.03.2006<br />
25.10.2005<br />
25.10.2005
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