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 />
10039353 LUFTHANSA TECHNIK AG REV. 1 A319-111/-112/-113/-114/-115 Replacement of Litton MK-1 Global Positioning None Prior to installation of this modification it 08.08.2<strong>01</strong>2<br />
A319-131/-132/-133<br />
System Sensor Unit (GPSSU)by CMC<br />
must be determined thatthe<br />
A320-111/-211/-212/-214/-215 Electronics GPSSU CMA-5024(STC revised<br />
interrelationship between this modification<br />
A320-216/-231/-232/-233 for validity extension to A319 and A321<br />
and any other previouslyinstalled<br />
A321-111/-112/-131/-211 models)<br />
modification and/ or repair will introduce<br />
A321-212/-213/-231/-232<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10039798 LUFTHANSA TECHNIK AG REV. 1 B747-8 Installation of class 2 EFB docking station with<br />
display, cockpit doorsurveillance cameras an<br />
taxi aid cameras at vertical stabilizer and<br />
atfuselage belly.<br />
10039911 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.03922 777-200 AS PER 777-EB-21-0228 STDD 21-09/02M: B-777-200 - Zonal Drying<br />
System Installation<br />
10<strong>04</strong>0589 LUFTHANSA TECHNIK AG B747-8 Camera installation in the vertical stabilizer for<br />
ground manoeuvringservice.<br />
Only for EFB installation. No installation of the<br />
belly and tail fincamera in the frame of this<br />
STC.<br />
10<strong>04</strong>0628 LUFTHANSA TECHNIK AG 319-133 A319-133 ANJI VIP Cabin Completion - This design change approval is applicable on<br />
Aircraft model AirbusA319-133 CJ, aircraft<br />
serial number 4428.<br />
10<strong>04</strong>1<strong>04</strong>4 LUFTHANSA TECHNIK AG 737-800 VIP Cabin Interior Completion BBJ2 1) As per AFM limitations A-00-11/006-AFM,<br />
Issue05, Rev 00 :- The aircraft is certified for<br />
non-commercial use.- Required Crew: in case<br />
passengers are on board one (1) cabin<br />
attendantis required and has to be seated at<br />
door #1, left hand side.- Cabin WLAN:<br />
10<strong>04</strong>1482 LUFTHANSA TECHNIK AG A318-112 A318-100 - ELITE - Project Comlux3. Green<br />
aircraft completion to a VIPcabin configuration.<br />
10<strong>04</strong>2417 LUFTHANSA TECHNIK AG A320-211 Integration of the W-IFE (Wireless In-Flight<br />
Entertainment) system onA320.<br />
10<strong>01</strong>6808 LUFTTRANSPORT AS <strong>EASA</strong>.IM.R.S.<strong>01</strong>168 - EUROCOPTER FRANCE AS<br />
365N SERI<br />
Mast Measurement System / System for<br />
Measurement of ground stations fixed radio<br />
antenna for correct frequencies as signal<br />
effects<br />
10029513 M&D FLUGZEUGBAU GmbH & CO. KG P-<strong>EASA</strong>.A.S.029<strong>04</strong> GLASFLUEGEL 3<strong>04</strong>B Modification of Glasfluegel 3<strong>04</strong>B, S/N 324:<br />
retrofitting with winglets -modified wing tips:<br />
winglets.<br />
Prior to installation of this modification it 17.07.2<strong>01</strong>2<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
none Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other<br />
previouslyinstalledmodification and/ or<br />
repair will introduce no adverse effect<br />
upon theairworthiness of the product.<br />
<strong>01</strong>.06.2<strong>01</strong>2<br />
none Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other<br />
previouslyinstalledmodification and/ or<br />
repair will introduce no adverse effect<br />
upon theairworthiness of the product.<br />
12.07.2<strong>01</strong>2<br />
The Lufthansa Technik's Instructions for<br />
continued airworthinessA-00-11/172-ICA<br />
Issue 2, Revision 00 dated 13th July 2<strong>01</strong>2<br />
approved aspart of this <strong>EASA</strong> STC<br />
contains:- A Section 4 with additional<br />
Airworthiness Limitation Items (ALI) that<br />
supplement those fr<br />
1) LCA compatibility necessary:<br />
Lufthansa Technik AG has shown<br />
withinthe substantiation data package<br />
that the installations covered by<br />
thisSupplemental Type Certificate is<br />
compatible with FAA approved FAA<br />
STCST<strong>01</strong>697SE (identified as Low Cabin<br />
16.07.2<strong>01</strong>2<br />
17.08.2<strong>01</strong>2<br />
Altitude - LC<br />
Prior to installation of this modification it 07.07.2009<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.The ins<br />
This approval is limited to MSN <strong>01</strong>10. Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
29.11.2<strong>01</strong>2<br />
None 12.06.2006<br />
Limited to Glasfluegel 3<strong>04</strong>B, S/N 324. None. 29.03.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 325/<strong>462</strong>
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