04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
<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>4494 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02556 BOMBARDIER CL-600-2B19 CL-600-2B19 - Cabin Completion - 16 PAX 1. Certification Basis of the Change: JAR-25<br />
Change 13, addtionally: CRI F-<strong>01</strong>, Executive<br />
Power System (Guidance Material)CRI D-<strong>01</strong>,<br />
Side Faching Divans (Deviation)CRI D-<strong>04</strong>,<br />
Door between passenger compartments with<br />
integrated blocking functionality (Deviatio<br />
29.03.2007<br />
10<strong>01</strong>45<strong>04</strong> LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02574 BOEING 747 Installation of an ATC Mode S - Enhanced<br />
Surveillance Upgrade in Boeing 747 series<br />
aircraft<br />
<strong>EASA</strong> approved Airplane Flight Manual<br />
Supplement, Lufthansa Technik Document A-<br />
34-06/135-AFM, Rev IR or later <strong>EASA</strong><br />
approved revisionis required part of this STC<br />
10<strong>01</strong>4507 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02580 REV. 1 A330 SERIES Installation of non-electrical Floor Path Marking<br />
System Guideline®<br />
10<strong>01</strong>4509 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02583 AIRBUS A300-600<br />
Installation of a new Stretcher for Kuwait<br />
AIRBUS A310-300<br />
Airways.<br />
10<strong>01</strong>4510 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02585 AIRBUS A320 Installation of a new Stretcher for Kuwait<br />
Airways<br />
10<strong>01</strong>4511 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02586 BOEING 777-200 SERIES Installation of a stretcher in the passenger Prior to installation of this modification the<br />
compartment for Kuwait Airways<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>4512 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02587 BOEING 747-400 Installation of a new stretcher for Kuwait<br />
Airlines B747-400 in accordance with<br />
Supplemental Type Definition Document<br />
STDD25-06 09MIss. <strong>01</strong>, Rev. <strong>01</strong> or later <strong>EASA</strong><br />
approved revision.<br />
10<strong>01</strong>4513 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02588 AIRBUS A340-300 Installation of a new Stretcher for Kuwait<br />
Airways<br />
10<strong>01</strong>4521 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02603 REV 1 AIRBUS A300-600 A300-600 Cabin Reconfiguration from Current<br />
Continental Version to Intercontinental Layout<br />
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 />
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 />
10<strong>01</strong>4552 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02648 AIRBUS A310-300 A310-300 Siberia Airlines Cabin<br />
Reconfiguration from 248 to 255 pax<br />
10<strong>01</strong>4563 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02663 REV. 1 A300 SERIES, A310 SERIES Installation of non-electrical Floor Path Marking<br />
System Guideline®<br />
10<strong>01</strong>4574 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02678 AIRBUS A319-115 Interior and systems installation incl. convertible Instruction for Continued Airworthiness,<br />
cabin configuration<br />
Airworthiness Limitations, Section 4.3, ref. C-<br />
AAA000-ICA, issue 2, dated January 12,<br />
2007or later approved revision<br />
10<strong>01</strong>4593 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02705 BOEING 737-700<br />
Upgrade Package of existing VIP Cabin As indicated in the applicable AFM<br />
BOEING 737-700 IGW<br />
Configuration from private Operation to Supplement:- A_00_<strong>01</strong>_311_AFM<br />
Commercial Operation<br />
Supplement Cabin TT&L for Private Operation-<br />
A_25_06_17M_ AFM Supplement Cabin TT&L<br />
for Commercial Operation.And as indicated in<br />
the LBA STC LBA.21E2.TA0307Compatibility<br />
of this design c<br />
10<strong>01</strong>4602 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02725 BOEING 747-100<br />
BOEING 747-200<br />
BOEING 747-300<br />
Installation of Pneumatic Metric Altimeter Certification Baisis of the Change: CS-25<br />
Amdt. 1<br />
10<strong>01</strong>4606 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02730 BOEING MD 11 Installation of a Rockwell Collins Tailwind 550<br />
Live TV system in Boeing MD-11 as detailed in<br />
STDD53-06/19M Supplemental Type Definition<br />
Document for Tailwind 550 Live TV installation<br />
MD-11<br />
09.11.2007<br />
10<strong>01</strong><strong>462</strong>0 LUFTHANSA TECHNIK AG <strong>EASA</strong>.A.S.02752 REV. 5 B737-700 IGW Revision of <strong>EASA</strong>.A.S.02752 Rev.4 per Major Once LCA is activated (installation of FAA STC Prior to installation of this modification it 03.12.2<strong>01</strong>2<br />
Change 0<strong>01</strong>0002741-0<strong>01</strong>:Operation at 8.99 psi ST<strong>01</strong>697SE as validatedper <strong>EASA</strong> STC must be determined thatthe<br />
maximum cabin differential pressure (Lower 10<strong>04</strong>2295) on an individual aircraft, the interrelationship between this modification<br />
CabinAltitude, LCA)Original STC Title: Design maintenancerequirements defined in Doc A-00- and any other previouslyinstalled<br />
and Implementation of VIP interior<br />
07/784-ICA will apply for the life ofthis aircraft. modification and / or repair will introduce<br />
andmiscellaneous aircraft systems.<br />
This limitation remains valid also in<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 318/<strong>462</strong><br />
<strong>04</strong>.08.2006<br />
14.09.2<strong>01</strong>2<br />
15.11.2007<br />
28.02.2008<br />
06.11.2007<br />
09.11.2007<br />
10.10.2007<br />
22.06.2006<br />
23.06.2006<br />
14.09.2<strong>01</strong>2<br />
26.<strong>01</strong>.2007<br />
18.08.2006<br />
25.08.2006
Change language