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
10013940 EADS SOGERMA EASA.A.S.00376 REV 1 AIRBUS A310-304 Royal Jordanian ATC Mode S Enhanced 1. The Aircraft Flight Manual Supplement No
07.01.2008
Surveillance installation according to EADS AFM-34-974 issue B dated 29 November
Sogerma Modification Approval Sheet SOG-34- 2004, or later EASA-approved revision, is a
974 issue 3 dated 29 November 2004.Note: required part of this STC.2. Prior to
This revision reflects the transfer of this STC installation of this modification the installer must
from EADS Sogerma Services to Sogerma
Servic
determine that the interrelationsh
10013941 EADS SOGERMA EASA.A.S.00377 REV 1 AIRBUS 310-325 Cabin Modification from 18F/C-180Y/C to Prior to installation of this modification the
07.01.2008
18B/C-188Y/C according to the modification installer must determine that the
approval sheet MAS No SOG-25-957 issue 1 interrelationship between this modification and
dated 6October 2004 or later EASA-approved any other previously installed modification will
revision.Note: This revision reflects the transfer introduce no adverse effect upon the
of this STC from EADS Sogerma Services airworthiness of the product. The install
10013950 EADS SOGERMA EASA.A.S.00432 REV 1 AIRBUS 310-325 Modification of ATLAS/KSSU galleys into full Prior to installation of this modification the
ATLAS standard in accordance with
installer must determine that the
Modification Approval Sheet reference SOG-25-interrelationship
between this modification and
958 Issue 01 dated 14 October 2004. All any other previously installed modification will
documents related to this STC are listed in the introduce no adverse effect upon the
Master Drawing List reference MDL-25-958 Iss airworthiness of the product. The install
10014005 EADS SOGERMA EASA.A.S.01042 REV 1 AIRBUS A340-300 Installation of an upper class with side facing
Britax Malcom seats with inflatable restraints,
monument, bar and chandelier, and
modification of the premium and economy
class by repitching.Note: This revision reflects
the transfer of this STC from EADS So
1. This STC is limited to Airbus A340-300
MSN 214, 002, 003, 164 and 225.2. A copy
of this STC and of the MAS/MDL must be
enclosed in the files of each modified aircraft.
10014022 EADS SOGERMA EASA.A.S.01077 REV 1 AIRBUS A330-203 Qatar Airways - Cabin Modification.
1. The approval of this modification is limited
Modification number: SOG-25-886 issue to the identified aircraft. The limitations and
1Note: This revision reflects the transfer of this conditions defined in the EASA Datasheet are
STC from EADS Sogerma Services to also applicable. A copy of the STC approval
Sogerma Services.Model: Airbus A330-203 and the MDL must be enclosed in the files of
MSN 463 and 504
each modified aircraft.
10014076 EADS SOGERMA EASA.A.S.01168 REV 1 AIRBUS A330-243 Cabin configuration for Gulf Air. All documents Prior to installation of this modification the
related to this STC are listed in the Modification installer must determine that the
SOG-25-1075 iss. 01 (or later EASA-aproved interrelationship between this modification and
revision).Note: This revision reflects the transfer any other previously installed modification will
of this STC from EADS Sogerma Services to introduce no adverse effect upon the
Sogerma Services.Mod
airworthiness of the product. The install
10014077 EADS SOGERMA EASA.A.S.01169 REV 1 AIRBUS A310 Installation of an ATC Mode S EHS. ATC
mode S modification for compliance with
Enhance Surveillance. Replacement of the
Rockwell Collins TRP-720 ATC by TRP-901
ATC.Note: This revision reflects the transfer of
this STC from EADS Sogerma Services to
Sogerma
07.01.2008
10014087 EADS SOGERMA EASA.A.S.01179 REV 1 DC-9-21 ELT Kannad 406 AF modification (SOG-25-
1106)Note: This revision reflects the transfer of
this STC from EADS Sogerma Services to
Sogerma Services.
1. This STC is limited to the DC-9 MSN 4708 04.01.2008
10014113 EADS SOGERMA EASA.A.S.01219 REV 1 ATR 42-320 SERIES Pseudo-Lisse configuration; RESSAC 1. In RALI configuration:-the mass of under
04.01.2008
configuration and RALI configuration.Note: This wing POD is limited to 72kg (POD equipped);-
revision reflects the transfer of this STC from the new design for the titanium pin on POD
EADS Sogerma Services to Sogerma rear attachment must be applied according to
Services.Model: Aerospatiale ATR 42-320 the EADS Sogerma Services waiver No.
MSN 078
A3002.2. The lighting issues are cert
10014114 EADS SOGERMA EASA.A.S.01220 REV 1 AEROSPATIALE ATR 42-320 ELT Kannad 406 AF ModificationNote: This
revision reflects the transfer of this STC from
EADS Sogerma Services to Sogerma
Services. Model: Aerospatiale ATR 42-320
MSN 078
Prior to installation of this modification the
installer must determine that the
interrelationship between this modification and
any other previously installed modification will
introduce no adverse effect upon the
airworthiness of the product. The install
10014169 EADS SOGERMA EASA.A.S.01302 REV 1 AIRBUS A321-200 A321 Livingston - Cabin Modification from 196 Prior to installation of this modification the
Y/C to 210 Y/C with relocation of two attendant installer must determine that the
seats.Note: This revision reflects the transfer of interrelationship between this modification and
this STC from EADS Sogerma Services to any other previously installed modification will
Sogerma Services.Model: Airbus A321-200 introduce no adverse effect upon the
MSN 1950 & 1970
airworthiness of the product. The install
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