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 />
10033224 DECA AVIATION ENGINEERING<br />
O-LSA07-225/D,ISSUE 1 P-180 AVANTI II TCA STC No. O-LSA07-225/D Issue 1 "Import None Prior to installation of this modification it <strong>04</strong>.<strong>01</strong>.2<strong>01</strong>1<br />
LIMITED<br />
Configuration - InteriorCompletion (including<br />
must be determined thatthe<br />
various cabin installations)"<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 />
10038463 DECA AVIATION ENGINEERING<br />
LIMITED<br />
10<strong>04</strong>0912 DECA AVIATION ENGINEERING<br />
LIMITED<br />
TCCA STC NO. O-LSA09-344/D CL-600-2B19 Iridium Antenna Installation. Restricted to ASN 8092. 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 />
17.02.2<strong>01</strong>2<br />
REV. 1 TCCA STC NO. O-LSA00-829/D BD-700-1A10 Baggage Door Locking System Modification Restricted to ASN 9003 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 />
28.08.2<strong>01</strong>2<br />
10<strong>01</strong>5489 DECA AVIATION ENGINEERING LTD <strong>EASA</strong>.IM.A.S.<strong>01</strong>251 - A321-211, SN 675 Interior reconfiguration 20J/152 Y seating<br />
arrangement<br />
10<strong>01</strong>5492 DECA AVIATION ENGINEERING LTD <strong>EASA</strong>.IM.A.S.<strong>01</strong>254 TCCA STC O-LSA<strong>04</strong>-008/D A320-232 Passenger Seat Cushion Assembly<br />
Replacement on B/E Aerospace, seat typ:<br />
D3111F11xx-<strong>01</strong> series<br />
10<strong>01</strong>5493 DECA AVIATION ENGINEERING LTD <strong>EASA</strong>.IM.A.S.<strong>01</strong>255 TCCA STC O-LSA05-<strong>01</strong>8/D A320-232 Reconfiguration of existing 180 passenger all<br />
economy seating arrangement<br />
10<strong>01</strong>5494 DECA AVIATION ENGINEERING LTD <strong>EASA</strong>.IM.A.S.<strong>01</strong>256 TCCA STC O-LSA02-327/D A319-112, A320-211, A320-212,<br />
A320-214, A320-231, A320-232<br />
Flight Warning Computer Altitude Callout<br />
Reconfiguration<br />
1. This STC is limited to A321 MSN 675.2. This<br />
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<br />
18.07.2005<br />
1. This STC is limited to the A320 MSN 496. 18.10.2005<br />
1. This STC is limited to the A320 MSN<br />
496.2. This STC is approved only for the<br />
product configuration as defined in the<br />
approved design data referred to in the<br />
paragraph "Description". Compatibility with<br />
other aircraft/engine configurations shall be<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>5587 DECA AVIATION ENGINEERING LTD <strong>EASA</strong>.IM.A.S.<strong>01</strong>498 TCCA STC O-LSA<strong>01</strong>-428/D ISS3 A320-232 Emergency exit sign Relocation 1) Limited to the A320 MSN 4962) This STC is<br />
approved only for the product configuration as<br />
defined in the approved design data referred to<br />
in the paragraph "Description". Compatibility<br />
with other aircraft/engine configurations shall<br />
be determined by the i<br />
10<strong>01</strong>5791 DECA AVIATION ENGINEERING LTD <strong>EASA</strong>.IM.A.S.<strong>01</strong>849 TCCA LSTC O-LSA02-653/D ISS 3 A318-112, A320-214 Passenger seat leather dress cover<br />
replacement<br />
10<strong>01</strong>6241 DECRANE AEROSPACE PATS<br />
<strong>EASA</strong>.IM.A.S.02513 REV. 1 FAA STC ST00741LA-D BOEING 737-700 Installation of Canadian Marconi CMA-21<strong>01</strong><br />
AIRCRAFT,<br />
High Gain SATCOM Antenna. This STC<br />
revises and supersedes <strong>EASA</strong> STC<br />
<strong>EASA</strong>.IM.A.S.02513. The revisionwas issued<br />
to reflect the transfer from Hollingshead<br />
International toDecrane Aerospace PATS<br />
Aircraft.<br />
10<strong>01</strong>6649 DECRANE AEROSPACE PATS<br />
AIRCRAFT,<br />
<strong>EASA</strong>.IM.A.S.03093 REV. 1 FAA STC ST02057LA BOEING 737-700 SERIES<br />
BOEING 737-800 SERIES<br />
Installation of Electronic Equipment Rack in Aft<br />
Bulk Cargo Compartment. This STC revises<br />
and supersedes <strong>EASA</strong> STC<br />
<strong>EASA</strong>.IM.A.S.03093. The revisionwas issued<br />
to reflect the transfer from Hollingshead<br />
International toDecrane Aerospace PATS<br />
Aircraft.<br />
18.10.2005<br />
18.10.2005<br />
25.10.2005<br />
This STC is limited to: A319 MSN 1846, A319<br />
MSN 1598 and A320 MSN 1686<br />
12.05.2006<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.The ins<br />
18.11.2009<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.The ins<br />
18.11.2009<br />
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