04/01/2013 Page 1/462 - EASA

EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue
10014007 SR TECHNICS SWITZERLAND Ltd. EASA.A.S.01047 REV. 1 B747-400 Reconfiguration of Virgin Atlantic Airways B747- none Associated instructions for continued 24.02.2011
400 from LHR to LGWconfiguration in
airworthiness, included in SRTechnics
accordance with SR Technics Master Data
Report C-747-25-1001-CS-13 Rev. 3,
ListC747-25-1001-MDL-01, Rev 3 or later
must be incorporated in theaircraft
approved revisions
maintenance documentation
10014568 SR TECHNICS SWITZERLAND Ltd. EASA.A.S.02672 REV. 1 A319-112 In-Flight telecommunication equipment - MSN 1077, 1084, 1089, 1136, 1147, 1155, Prior to installation of this modification it 10.02.2011
antenna installation(partial removal of GTE 1170, 1209, 1277
must be determined thatthe
Airfone System installed by FAA STC
interrelationship between this modification
ST00129NY-Dand SA1693GL) The Revision 1
and any other previouslyinstalled
was issued to reflect the transfer from SR
modification and/ or repair will introduce
TechnicsIreland to SR Technics Switzerland
no adverse effectupon the airworthiness
LTD
of the product
10029069 SR TECHNICS SWITZERLAND Ltd. REV. 1 B747-400 Reconfiguration of Virgin Atlantic Airlines B747- This STC is limited to the following
Prior to installation of this modification it 24.02.2011
400 Aft Upper Deck inaccordance with SR A/C:1.,,B747-4Q8, G-VFAB, Tab # RT945, must be determined thatthe
Technics Master Data List C747-25-1005-MDL MSN 24958.2.,,B747-4Q8, G-VHOT, Tab # interrelationship between this modification
Rev. 0. orlater approved revisions
RT946, MSN 26326.3.,,B747-4Q8, G-VBIG, and any other previouslyinstalled
Tab # RT947, MSN 26255.4.,,B747-41R, G- modification and/ or repair will introduce
VWOW, Tab # RM052, MSN 32745.5.,,B747- no adverse effectupon the airworthiness
41R, G-VROC, Tab # RM053,
of the product.
10031834 SR TECHNICS SWITZERLAND Ltd. REV. 3 B767-300 Cabin reconfiguration - Air Seychelles 767-
300Aircraft reconfiguration by replacing the
existing J-class seat with anew electrically
powered seat. There are adaptations to the
existingPSU, Y-class cabins to suit new layout.
10034187 SR TECHNICS SWITZERLAND Ltd. A330-300 Virgin Atlantic Airways (VAA) A330-300 EIS
Cabin Reconfiguration (59W /255Y).This STC
reconfigures the cabin layout from 48 W class
seat / 265 Yclass seat to 59 W class seat / 255
Y class seat, with associatedadaptations.
10038294 SR TECHNICS SWITZERLAND Ltd. A310 Amiri Flight A310-300 Cabin RefurbishmentBy
refurbish the existing Cabin by:- Removal of the
existing seats and installation of new seats in
theFirst, Business and Economy class.-
Replace the existing IFE system- Installation of
a new VCC, class dividers,
10040981 SR TECHNICS SWITZERLAND Ltd. A340-541 VIP Cabin RefurbishmentThe modification
consist of the following items:-,,Refurbishment
of existing cabin materials-,,Deletion of a
double seat and installation of aft stowage-
,,Installation of a book cabinet-,,Upgrade of the
IFE equipment (monitors, playe
10042831 SR TECHNICS SWITZERLAND Ltd. A330-223 Cabin reconfigurationBy changing the existing
Air Berlin Business Class InteriorConfiguration
into a new Etihad Business Class Interior
Configuration.
10038822 ST AEROSPACE MOBILE, INC. FAA STC ST13005AT-T B757-200 Conversion of Passenger Configuration to
Cargo/Passenger CombinationConfiguration
None. Prior to installation of this modification it
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
26.11.2012
1-,,This STC must be implemented together
with EASA STC ref : 10031808Rev 01 (and
associated Approved Model List), or later
revisions approvedby EASA. 2-,,This STC is
applicable to A330-300 following MSN :-,,1195
-,,1201 -,,1206 -,,1215 -,,1231
Prior to installation of this modification it 14.03.2011
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product
S/N: 0667 A7-AFE Prior to installation of this modification it
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
03.02.2012
S/N: 0495 A7-HHH Prior to installation of this modification it
must be determined thatthe
interrelationship between this modification
and any other previouslyinstalled
modification and/ or repair will introduce
no adverse effectupon the airworthiness
of the product.
10.08.2012
S/N: 0403 / 0432 / 0444 / 0454 / 0469 / 0476 /
0493The IFE System must be deactivated for
any flight before EMI testing isfinally
accomplished.For any other limitation refer to
the existing AMES AFMS, Doc.
No.AFS_M14800101_MGR_06102011, latest
approved Rev
This STC is limited to a/c serial number 25622
onlyAs per the Temporary Deviation a/c
converted under this STC cannot beoperated
after 23/12/2013 unless incorporating design
changes to theMain Deck Cargo Door.This
STC cannot be installed on aeroplanes with
Approval is valid only for MSN mentioned
aboveDue to some missing passenger
seats placards, the Airline
ServicesLimited Engineering Change
Notice, C330-25-0704-ECN-03, Rev. 2,
needs tobe accomplished prior the first
passenger flight on 27. December
2012.Pr
An approved Cargo Loading System
must be installed concurrently
beforeoperations.An approved FWD 9g
barrier must be installed concurrently
beforeoperations.ST Aerospace Minor
Modifications EDC/EASA/DOA/023 and
EDC/EASA/DOA/41must be installed
concurrently
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22.03.2012