04/01/2013 Page 1/462 - EASA

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EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10014872 LUFTHANSA TECHNIK AG EASA.A.S.03097 BOMBARDIER CL-600-2B19 Installation of Structural Provisions for Cabin 11. For all flights with "Green Aircraft" and 05.02.2008 Completion "Structural Provisions for cabin completion" (293,7 [kg]) installed the installation of Ferry-Kit M/S TC 601R16990 (867 [kg]) is necessary.2. With the installation of Ferry-Kit M/S TC 601R16990 (867 [kg]) 10014873 LUFTHANSA TECHNIK AG EASA.A.S.03098 AIRBUS A330-200 A330 - Installation of Zonal Drying System /The system is installed to get rid of the humidity between the cabin lining and the fuselage 10014893 LUFTHANSA TECHNIK AG EASA.A.S.03123 REV 1 AIRBUS A319-100 PTU and/or Stretcher Installation on A319-100 /Optional replacement of seats by up to 2 Passenger Transport Units (PTU) and/or up to 4 stretchers. • Detailed visual inspection of the Oxygen Discharge Plug at an interval of 750 FC ( C check ), as reported in the document Instruction for Continued Airworthiness, ref. Doc. A-00-07/641-ICA Issue 03, dated 19.09.07 10014897 LUFTHANSA TECHNIK AG EASA.A.S.03127 REV. 1 B777-200, B777-300 Installation of non-electrical Floor Path Marking System Guideline® 14.09.2012 10014906 LUFTHANSA TECHNIK AG EASA.A.S.03142 REV. 6 A318-112 Structural Floor Panel Reconfiguration None - Prior to installation of this modification the installer mustdetermine that the interrelationship between this modification and anyother previously installed modification will introduce no adverse effectupon the airworthiness of the product.- The install 07.10.2009 10014934 LUFTHANSA TECHNIK AG EASA.A.S.03189 REV 5 AIRBUS A318-112 A318 ELITE – RAK – Structural Floor Panel – SFP - Retrofit 10014972 LUFTHANSA TECHNIK AG EASA.A.S.03253 AIRBUS A340-212 WLAN InstallationDesign and implementation of Wireless Local Area Network System 1. Prior to installation of this modification the installer must determine that the interrelationship between this modification andany other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2. The ins 10015011 LUFTHANSA TECHNIK AG EASA.A.S.03313 REV. 1 EMB-135/-145 SERIES Installation of non-electrical Floor Path Marking System Guideline® 10015043 LUFTHANSA TECHNIK AG EASA.A.S.03359 A300B4-603 / -605R A300B4-603 / -605R Cabin The installation of this STC has a prerequisite ReconfigurationCabin Reconfiguration from aircraft configuration.2. This STC is only current version (280 MC) to two possible applicable on aircraft in association with the versions (58 CC / 188 MC or 40 CC / 220 MC). EASA STC ref: EASA.A.S.02663.3. The Certification Review Item A-01 has to be considered, in addition to the 10015047 LUFTHANSA TECHNIK AG EASA.A.S.03363 BOEING 767-300 Condor B767 Interior Modification • Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.• Th 10015072 LUFTHANSA TECHNIK AG EASA.A.S.03402 AIRBUS A318-112 A318 ELITE - Project BAA; VIP Cabin completion. 1. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product.2. 10015091 LUFTHANSA TECHNIK AG EASA.A.S.03428 A3118 A318 – Ballast Weight Installation Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install 10015107 LUFTHANSA TECHNIK AG EASA.A.S.03450 A300 F4-600R Structure modification for GPS antennae installationThis STC defines the structural modification for the installation of a dual GPS antennae, in place of the existing Gatelink antenna 10015120 LUFTHANSA TECHNIK AG EASA.A.S.03469 REV. 1 D328 SERIES Installation of non-electrical Floor Path Marking System Guideline® 04/01/2013 Page 320/462 25.05.2007 01.10.2007 08.04.2009 11.10.2007 14.09.2012 04.03.2008 29.08.2008 07.11.2008 12.08.2008 08.05.2008 14.09.2012
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10015142 LUFTHANSA TECHNIK AG EASA.A.S.03502 REV 1 LBA STC LBA.21E2.TA0270 BOMBARDIER CL-600-2B19 Replacement of Zonal Dryer related to EASA AD 2006-0140-E.The above reference EASA AD required the de-activation of Zonal Drying Systems installed via LBA STC LBA.21E2.TA0270 due to the potential for combustion of contaminants in the dryer unit. A new drye See related STC LBA.21E2.TA0270 05.08.2008 10015144 LUFTHANSA TECHNIK AG EASA.A.S.03504 REV 1 LBA STC LBA.21E2.0307 BOEING 737-700 Replacement of Zonal Dryer related to EASA AD 2006-0140-EThe above reference EASA AD required the de-activation of Zonal Drying Systems installed via LBA STC LBA.21E2.0307 due to the potential for combustion of contaminants in the dryer unit. A new dryer u See related STC LBA.21E2.0307 05.08.2008 10015145 LUFTHANSA TECHNIK AG EASA.A.S.03505 REV 1 LBA STC LBA.21E2.TA0636 BOEING 737-800 Replacement of Zonal Dryer related to EASA AD 2006-0140-E.The above reference EASA AD required the de-activation of Zonal Drying Systems installed via LBA STC LBA.21E2.TA0636 due to the potential for combustion of contaminants in the dryer unit. A new drye See related STC LBA.21E2.TA0636 05.08.2008 10015146 LUFTHANSA TECHNIK AG EASA.A.S.03506 REV 1 LBA STC TA0733 BOEING 747-400 Replacement of Zonal Dryer related to EASA AD 2006-0140-E.The above reference EASA AD required the de-activation of Zonal Drying Systems installed via LBA STC TA0733 due to the potential for combustion of contaminants in the dryer unit. A new dryer unit ha See related STC TA0733 05.08.2008 10015147 LUFTHANSA TECHNIK AG EASA.A.S.03507 REV 1 LBA STC LBA.21E2.TA0609 AIRBUS A330-200 Replacement of Zonal Dryer related to EASA AD 2006-0140-E.The above reference EASA AD required the de-activation of Zonal Drying Systems installed via LBA STC LBA.21E2.TA0609 due to the potential for combustion of contaminants in the dryer unit. A new drye See related STC LBA.21E2.TA0609 05.08.2008 10015158 LUFTHANSA TECHNIK AG EASA.A.S.03526 AIRBUS A318-112 A318 ELITE - Project Comlux 2; VIP Cabin Prior to installation of this modification the 12.12.2008 completion installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. 10015177 LUFTHANSA TECHNIK AG EASA.A.S.03554 AIRBUS A318-112 A318-112 - ELITE - Project HKInstallation of a Prior to installation of this modification the VIP cabin for a maximum of 19 passengers for installer must determine that the 28.01.2009 commercial and non-commercial operation. interrelationship between this modification and The design details are described in General any other previously installed modification Description S-00-08/731. will introduce no adverse effect upon the airworthiness of the product. 10015215 LUFTHANSA TECHNIK AG EASA.A.S.03630 AIRBUS A318-112 A318-112 - ELITE - Project Tanker 1. Prior to installation of this modification the 20.02.2009 1Installation of a VIP cabin for a maximum of installer must determine that the 16 passengers for non-commercial operation interrelationship between this modification and only. The design details are described in any other previously installed modification will General Description C-AAA024-SPA. introduce no adverse effect upon the airworthiness of the product.2. 10027345 LUFTHANSA TECHNIK AG P-EASA.A.S.03346 CL-600-2D24 Introduction of Datalink 2000+ Not Applicable Not Applicable 23.09.2009 10027505 LUFTHANSA TECHNIK AG P-EASA.A.S.03912 FOKKER F27 MARK 050 Installation of self-illuminating Floor Path Fokker F50 (F27 Mark 050) aircraft series in Prior to installation of this modification it 06.10.2009 Marking System. standard airline cabinconfiguration described must be determined thatthe as typical cabin layout in Engineering interrelationship between this modification BulletinF50-EB33-0343, Rev. 01, CH. 4.2. and any other previouslyinstalled Cabin layout with convertible seats(non fixed modification and/ or repair will introduce lateral position may result in covering no adverse effectupon the airworthiness of the product. 10028128 LUFTHANSA TECHNIK AG P-EASA.A.S.03435 A330-243 A330-200 - VIP Cabin Interior Completion as per AFMS A-00-09/009-AFM issue 5 as as per AFMS A-00-09/009-AFM issue 5 03.12.2009 listed in the associatedtechnical documentation as listed in the associatedtechnical documentation Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ 04/01/2013 Page 321/462
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04/01/2013 Page 1/462 - EASA

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