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>5134 LTB SAMMET GmbH <strong>EASA</strong>.A.S.03487 <strong>EASA</strong> STC <strong>EASA</strong>.A.S.C.<strong>01</strong>008 AND CESSNA 150D<br />
Installation of engine Rotax 912 F3 and 1. Spin is prohibited to all models.2. Aerobatic<br />
25.02.2008<br />
CESSNA 150E<br />
installation of Propeller Hoffmann HO- including Spin is prohibited to Cessna A150K,<br />
CESSNA 150F<br />
V352F/170FQ on Cessna Models 150H, FA150K, A150L and FA150L.3. Prior to<br />
CESSNA 150G<br />
F150H, A150K, FA150K, A150L, FA150L, installation of this modification the installer must<br />
CESSNA 150H<br />
150K, F150K, 150L and F150L only.Installation determine that the interrelationship between<br />
CESSNA 150J<br />
of engine Rotax 912 S3 (100PS) and this modification andany o<br />
CESSNA 150L<br />
CESSNA 150M<br />
CESSNA A150L<br />
CESSNA F150-G<br />
CESSNA F150-H<br />
CESSNA F150-J<br />
CESSNA F150-K<br />
CESSNA F150-L<br />
CESSNA F150-M<br />
CESSNA FA-150-K<br />
installation of Propeller<br />
10<strong>01</strong>3924 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02836 REV. 4 AIRBUS A318-112 Structural Floor Panel ReconfigurationThe 1. Side facing divans may not be used for taxi,<br />
18.12.2008<br />
limitation for divans that they must not be take off and landing after1315 FH or 14<br />
occupied for taxi, take off and landing has been months whatever occurs first, starting at June<br />
suspended for 1315 FH or 14 monthswhatever 26th, 2008.2. Prior to installation of this<br />
occurs first, starting at June 26th, 2008.The modification the installer must determine that<br />
modification is described in the<br />
the interrelationship betw<br />
10<strong>01</strong>3943 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.00382 REV 1 AIRBUS A340-300 Installation of Antenna and Receiver Transmit 1. "The IEEE 802.11 a, b, g (as customized)<br />
System and Network Services(acc.: STDD 00- Wireless Local Area Network (WLAN)<br />
03/11M issue 02)<br />
introduced by this modification, may be<br />
activated onboard Airbus A340-600 Aircraft for<br />
operation with commercial IEEE 802.11a, b, g<br />
& h compliant WLAN enabled portable<br />
electroni<br />
10<strong>01</strong>3964 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.00654 REV. 2 A340 Installation of non-electrical Floor Path Marking<br />
System Guideline®<br />
10<strong>01</strong>3967 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.007<strong>01</strong> REV 1 BOEING 747-300-400 Radome Installation for Live TV Antenna<br />
Installation<br />
10<strong>01</strong>3977 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>000 BOEING 767-300 Installation of an Optical Quick Access<br />
Recorder (OQAR) according to LHT<br />
Engineering Bulletin No. 767-EB31-0203,<br />
dated 09.09.<strong>04</strong> or later approved Revision for<br />
FOQA Purpose<br />
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 />
1. Maintenance requirements, Doc. No. C-<br />
AAL900-MR shall be incorporated in the<br />
aircraft maintenance documentation.2. This<br />
STC is approved only for the product<br />
configuration as defined in the approved design<br />
data. Compatibility with other aircraft/eng<br />
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 configurations<br />
shall be determined by the installer.<br />
10<strong>01</strong>3978 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>0<strong>01</strong> BOEING 737-300 Installation of an Optial Quick Access Recorder This STC is approved only for the product<br />
(OQAR) according to LHT Engineering Bulletin configuration as defined in the approved design<br />
No.737-EB31- 0202, dated 29.09.<strong>04</strong> or later data referred to in the paragraph "Description".<br />
approved Revision for FOQA Purpose. Compatibility with other Aircraft configurations<br />
shall be determined by the installer.<br />
10<strong>01</strong>4<strong>01</strong>3 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>056 REV. 1 A318/A319/A320/A321 Installation of non-electrical Floor Path Marking<br />
System Guideline®<br />
10<strong>01</strong>4<strong>04</strong>3 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>121 AIRBUS A330-200 A330-200 Air Algerie Quick Change VIP Kit<br />
OnePlus.<br />
10<strong>01</strong>4079 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>171 BOEING 777-300 Installation of PC Power and PC Data Outlets<br />
on the existing B/C Seats and installation of<br />
new ECO Class Seats with new P/N and PC-<br />
Power/PC-Data Outlets on Boeing 777-300<br />
A/C of Cathay Pacific Airways.<br />
10<strong>01</strong>4126 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>236 BOEING 747-2B4B<br />
BOEING 747-SP<br />
Flight Management System (FMS), Activation<br />
of Advisory VNAV Modeaccording to Lufthansa<br />
Technik Supplemental Type Definition<br />
Document STDD34-05/02M, Issue <strong>01</strong>, Rev 00,<br />
dated April 20, 2005 or laterapproved revision<br />
10<strong>01</strong>4158 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>286 BOEING 767-300 B-767- Cabin Layout Change - Air Europe 21.06.2005<br />
10<strong>01</strong>4191 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.<strong>01</strong>333 REV 1 BOEING 767 SERIES Installation of Guideline-Self Illuminating Floor<br />
Path Marking System.<br />
14.12.2005<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 315/<strong>462</strong><br />
15.11.2005<br />
14.09.2<strong>01</strong>2<br />
23.<strong>04</strong>.2009<br />
17.08.2005<br />
17.08.2005<br />
14.09.2<strong>01</strong>2<br />
31.03.2005<br />
<strong>01</strong>.03.2005<br />
30.05.2005
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