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 />
10028238 LUFTHANSA TECHNIK AG P-<strong>EASA</strong>.A.S.03774 REV. 1 A318-112 A318-112 - Elite 11 - VIP Cabin Completion Not applicable 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 />
26.<strong>04</strong>.2<strong>01</strong>0<br />
10028693 LUFTHANSA TECHNIK AG P-<strong>EASA</strong>.A.S.03921 REV. 1 B737-300 Zonal Dryer System Installation in accordance<br />
with 737-EB21-0212<br />
10028830 LUFTHANSA TECHNIK AG P-<strong>EASA</strong>.A.S.03761 REV. 2 A319-133 A319-133 "GAF" VIP Cabin Completion,<br />
Revision 2To incorporate additional CMR in the<br />
ICA and MPD SupplementClosure of post<br />
certification action item D-08-<strong>01</strong>.<br />
10029134 LUFTHANSA TECHNIK AG A340-600 A340-600 Cabin Retrofit Etihad ETD06 The STC holder shall provide by 7th June 2<strong>01</strong>0<br />
Instructions for ContinuedAirworthiness on<br />
Electrical Wiring Interconnection System -<br />
EWIS ICA -in accordance with CS-25,<br />
Appendix H "Electrical Wiring<br />
InterconnectionSystem".<br />
10029677 LUFTHANSA TECHNIK AG A310-3<strong>04</strong> Fuselage - Structural provisions and Satcom<br />
antenna installation, Satcomequipment rack<br />
installation and VHF antenna installation.This<br />
STC installs Satcom and VHF antennae, as<br />
well as the provision forthe future support of a<br />
Satcom system installation.<br />
10030208 LUFTHANSA TECHNIK AG P-<strong>EASA</strong>.A.S.03776 REV. 2 A318-112 Installation of a VIP cabin for a maximum of 19<br />
passengers. The designdetails are described in<br />
General Description C-AAA057-SPA.Deletion<br />
of the Airworthiness Limitation Item reference<br />
530000-<strong>01</strong>-S forA318-112 Elite 14 MSN 4169<br />
10030228 LUFTHANSA TECHNIK AG A380-841/ -842 Installation of Class 2 EFB Laptop Cradle This STC is only intended for the defined Class<br />
2 EFB with Type A andType B software<br />
applications, in accordance with JAA<br />
Temporary GuidanceLeaflet TGL-36 and FAA<br />
Advisory Circular AC120-76A.Operation of<br />
type C software applications in accordance<br />
with FAAA<br />
10030374 LUFTHANSA TECHNIK AG A340-500 A340-500 Cabin retrofit ETD03This STC<br />
modifies the cabin layout by replacing First<br />
Class seats andall associated seat<br />
monuments.<br />
100312<strong>01</strong> LUFTHANSA TECHNIK AG A340-213 A340-200 - Installation of provisions for Live<br />
TV, Satcom, and W-LANThis STC installs<br />
several structural provisions for Live TV,<br />
Satcom, andW-LAN systems, relocates the<br />
existing upper Anti-Collision Light (ACL)and<br />
installs a additional upper ACL.<br />
None 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 />
20.10.2<strong>01</strong>0<br />
None. 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 />
16.08.2<strong>01</strong>0<br />
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 />
08.03.2<strong>01</strong>0<br />
Limited to: MSN 484 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 />
12.<strong>04</strong>.2<strong>01</strong>0<br />
None 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 />
19.07.2<strong>01</strong>1<br />
Prior to installation of this modification it 03.06.2<strong>01</strong>0<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 previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
11.06.2<strong>01</strong>0<br />
Limited to MSN 151 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 />
30.07.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 322/<strong>462</strong>
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