04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
<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>4348 SOGERMA SERVICES <strong>EASA</strong>.A.S.<strong>01</strong>612 REV 1 AIRBUS A340-642 This STC deals with the installation of 4 new 1. This STC is approved only to allow airline<br />
<strong>04</strong>.<strong>01</strong>.2008<br />
double seats in Y class (Kyoto<br />
customer to install on a trial basis a few seats<br />
manufacturer)Note: This revision reflects the on one aircraft (MSN 706).2. The limitations<br />
transfer of this STC from EADS Sogerma and conditions defined in the <strong>EASA</strong> Datasheet<br />
Services to Sogerma Services.<br />
are applicable.A copy of this STC and of the<br />
MAS/MDL must be encl<br />
10<strong>01</strong>4365 SOGERMA SERVICES <strong>EASA</strong>.A.S.<strong>01</strong>635 REV 1 A340-642 This STC deals with the installation of a 2 new<br />
triple seats in W class (Contour design<br />
seats).Note: This revision reflects the transfer<br />
of this STC from EADS Sogerma Services to<br />
Sogerma Services.<br />
10<strong>01</strong>4416 SOGERMA SERVICES <strong>EASA</strong>.A.S.<strong>01</strong>73 REFV 1 AIRBUS A340-642 Installation in upper class side facing Britax<br />
Malcom seats equipped with the inflatable<br />
restraints, monuments, a bar and a chandelier<br />
according to MAS SOG-25-597 issue 4 (dated<br />
02/07/<strong>04</strong>) and reference documents : Airplane<br />
Flight Manual A340-600 1.02.00 P<br />
1. This STC is approved only to allow airline<br />
customer to install on a trial basis a few seats<br />
on one aircraft (MSN 706).2. The limitations<br />
and conditions defined in the <strong>EASA</strong> Datasheet<br />
are applicable.A copy of this STC and of the<br />
MAS/MDL must be encl<br />
10<strong>01</strong>4428 SOGERMA SERVICES <strong>EASA</strong>.A.S.02474 REV 1 DC-9-21 Modification Janus Phase I: Cancellation of the 1. This STC is limited to the MSN 47308.<br />
restriction of flights in icing conditionsNote: This<br />
revision reflects the transfer of this STC from<br />
EADS Sogerma Services to Sogerma<br />
Services.<br />
<strong>04</strong>.<strong>01</strong>.2008<br />
10<strong>01</strong>4476 SOGERMA SERVICES <strong>EASA</strong>.A.S.02538 REV 1 AIRBUS A320-211 Cabin modification from 155 to 167 Y/CNote:<br />
This revision reflects the transfer of this STC<br />
from EADS Sogerma Services to Sogerma<br />
Services.<br />
1. This STC is limited to the A320 MSN 615. <strong>04</strong>.<strong>01</strong>.2008<br />
10<strong>01</strong>4862 SOGERMA SERVICES <strong>EASA</strong>.A.S.03086 AIRBUS A300 MODEL B2-1C Replacement of the obsolete RCA weather 1. This STC is limited to the MSN 0032.<br />
29.05.2007<br />
radar by a Honeywell RDR-4B colour display This STC is approved only for the product<br />
radar system with predictive windshear configuration as defined in the approved design<br />
function.<br />
data referred to in the paragraphs "Description"<br />
and “Associated Technical Documentation”.<br />
Compatibility with other airc<br />
10<strong>01</strong>4899 SOGERMA SERVICES <strong>EASA</strong>.A.S.03129 A310-325 Installation of ATC mode S Enhanced<br />
Surveillance (EHS)This Supplement Type<br />
Certificate consists in the installation of new<br />
1. This STC is limited to A310-325 aircraft<br />
model:- MSN 636- MSN 6442. Prior to<br />
installation of this modification the installer must<br />
ATC EHS in order to be compliant with the new determine that the interrelationship between<br />
ATC mode S ‘Enhanced Surveillance’ this modification and any other previously<br />
regulation.<br />
installed modification will i<br />
10<strong>01</strong>5<strong>01</strong>3 SOGERMA SERVICES <strong>EASA</strong>.A.S.03315 AIRBUS A340-313 Virgin Atlantic A340 Cabin Modification. 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.<br />
10<strong>01</strong>5078 SOGERMA SERVICES <strong>EASA</strong>.A.S.03412 AIRBUS A320 SERIES Installation of passenger entertainment cabin<br />
audio system on seatsNote: This STC<br />
supersede DGAC France STC 180-SF-<strong>01</strong>75.<br />
10<strong>01</strong>5079 SOGERMA SERVICES <strong>EASA</strong>.A.S.03413 DGAC FRANCE STC 180-SF-<strong>01</strong>74 AIRBUS A320 SERIES Sony Video System InstallationNote: This STC<br />
supersede DGAC France STC 180-SF-<strong>01</strong>74.<br />
10<strong>01</strong>5080 SOGERMA SERVICES <strong>EASA</strong>.A.S.03414 DGAC FRANCE STC 072-MJ-0857 AIRBUS A300 MODEL B2-1A Installation of a GPS/HIS adapterNote: This<br />
STC supersede DGAC France STC 072-MJ-<br />
0857.<br />
10<strong>01</strong>5081 SOGERMA SERVICES <strong>EASA</strong>.A.S.03415 DGAC STC F-C180-SF-0242; <strong>EASA</strong> AIRBUS A320 SERIES Cabin conversion modificatiom "20 B/C - 148<br />
Y/C"Note: This STC supersede DGAC France<br />
STC F-C180-SF-0242 and <strong>EASA</strong> 20<strong>04</strong>-9168.<br />
10<strong>01</strong>5082 SOGERMA SERVICES <strong>EASA</strong>.A.S.03416 DGAC FRANCE STC F-C072MJ0864; AIRBUS A300-600 Installation of an ELT 96 emergency locator<br />
transmitterNote: This STC supersede DGAC<br />
France STC F-C072MJ0864 and <strong>EASA</strong> 20<strong>04</strong>-<br />
4595.<br />
10<strong>01</strong>5083 SOGERMA SERVICES <strong>EASA</strong>.A.S.03417 DGAC FRANCE STC 180-SF-0229; E AIRBUS A320 SERIES Cabin conversion from 180 Y/C to 16 B/C +<br />
169 Y/CNote: This STC supersede DGAC<br />
France 180-SF-0229 and <strong>EASA</strong> 20<strong>04</strong>-3515.<br />
10<strong>01</strong>5084 SOGERMA SERVICES <strong>EASA</strong>.A.S.03418 DGAC FRANCE STC 180-SF-0221; E AIRBUS A320 SERIES Installation of BENNET seat containerNote:<br />
This STC supersede DGAC France 180-SF-<br />
0221 and <strong>EASA</strong> 20<strong>04</strong>-2036.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 416/<strong>462</strong><br />
<strong>04</strong>.<strong>01</strong>.2008<br />
07.<strong>01</strong>.2008<br />
19.07.2007<br />
12.06.2008<br />
<strong>04</strong>.<strong>01</strong>.2008<br />
<strong>04</strong>.<strong>01</strong>.2008<br />
<strong>04</strong>.<strong>01</strong>.2008<br />
<strong>04</strong>.<strong>01</strong>.2008<br />
<strong>04</strong>.<strong>01</strong>.2008<br />
<strong>04</strong>.<strong>01</strong>.2008<br />
<strong>04</strong>.<strong>01</strong>.2008
Change language