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>4872 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03097 BOMBARDIER CL-600-2B19 Installation of Structural Provisions for Cabin 11. For all flights with "Green Aircraft" and<br />
05.02.2008<br />
Completion<br />
"Structural Provisions for cabin completion"<br />
(293,7 [kg]) installed the installation of Ferry-Kit<br />
M/S TC 6<strong>01</strong>R16990 (867 [kg]) is necessary.2.<br />
With the installation of Ferry-Kit M/S TC<br />
6<strong>01</strong>R16990 (867 [kg])<br />
10<strong>01</strong>4873 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03098 AIRBUS A330-200 A330 - Installation of Zonal Drying System /The<br />
system is installed to get rid of the humidity<br />
between the cabin lining and the fuselage<br />
10<strong>01</strong>4893 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03123 REV 1 AIRBUS A319-100 PTU and/or Stretcher Installation on A319-100<br />
/Optional replacement of seats by up to 2<br />
Passenger Transport Units (PTU) and/or up to<br />
4 stretchers.<br />
• Detailed visual inspection of the Oxygen<br />
Discharge Plug at an interval of 750 FC ( C<br />
check ), as reported in the document<br />
Instruction for Continued Airworthiness, ref.<br />
Doc. A-00-07/641-ICA Issue 03, dated<br />
19.09.07<br />
10<strong>01</strong>4897 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03127 REV. 1 B777-200, B777-300 Installation of non-electrical Floor Path Marking<br />
System Guideline®<br />
14.09.2<strong>01</strong>2<br />
10<strong>01</strong>4906 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03142 REV. 6 A318-112 Structural Floor Panel Reconfiguration None - Prior to installation of this modification<br />
the installer mustdetermine that the<br />
interrelationship between this modification<br />
and anyother previously installed<br />
modification will introduce no adverse<br />
effectupon the airworthiness of the<br />
product.- The install<br />
07.10.2009<br />
10<strong>01</strong>4934 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03189 REV 5 AIRBUS A318-112 A318 ELITE – RAK – Structural Floor Panel –<br />
SFP - Retrofit<br />
10<strong>01</strong>4972 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03253 AIRBUS A340-212 WLAN InstallationDesign and implementation<br />
of Wireless Local Area Network System<br />
1. Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification<br />
andany other previously installed modification<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.2. The ins<br />
10<strong>01</strong>5<strong>01</strong>1 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03313 REV. 1 EMB-135/-145 SERIES Installation of non-electrical Floor Path Marking<br />
System Guideline®<br />
10<strong>01</strong>5<strong>04</strong>3 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03359 A300B4-603 / -605R A300B4-603 / -605R Cabin<br />
The installation of this STC has a prerequisite<br />
ReconfigurationCabin Reconfiguration from aircraft configuration.2. This STC is only<br />
current version (280 MC) to two possible applicable on aircraft in association with the<br />
versions (58 CC / 188 MC or 40 CC / 220 MC). <strong>EASA</strong> STC ref: <strong>EASA</strong>.A.S.02663.3. The<br />
Certification Review Item A-<strong>01</strong> has to be<br />
considered, in addition to the<br />
10<strong>01</strong>5<strong>04</strong>7 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03363 BOEING 767-300 Condor B767 Interior Modification • 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.• Th<br />
10<strong>01</strong>5072 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03402 AIRBUS A318-112 A318 ELITE - Project BAA; VIP Cabin<br />
completion.<br />
1. 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.2.<br />
10<strong>01</strong>5091 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03428 A3118 A318 – Ballast Weight Installation 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>5107 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03450 A300 F4-600R Structure modification for GPS antennae<br />
installationThis STC defines the structural<br />
modification for the installation of a dual GPS<br />
antennae, in place of the existing Gatelink<br />
antenna<br />
10<strong>01</strong>5120 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03469 REV. 1 D328 SERIES Installation of non-electrical Floor Path Marking<br />
System Guideline®<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 320/<strong>462</strong><br />
25.05.2007<br />
<strong>01</strong>.10.2007<br />
08.<strong>04</strong>.2009<br />
11.10.2007<br />
14.09.2<strong>01</strong>2<br />
<strong>04</strong>.03.2008<br />
29.08.2008<br />
07.11.2008<br />
12.08.2008<br />
08.05.2008<br />
14.09.2<strong>01</strong>2
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