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 />
10032781 SOCIETE D'ETUDE ET DE GESTION DR300/108, DR300/120,<br />
A-07-09-Filtre Ed. 0 - Installation of remote oil None Prior to installation of this modification it <strong>01</strong>.12.2<strong>01</strong>0<br />
DR300/125, DR300/140<br />
filter kit<br />
must be determined thatthe<br />
DR300/180 R, DR315, DR340,<br />
interrelationship between this modification<br />
DR360, DR380, DR400/100,<br />
and any other previouslyinstalled<br />
DR400/120 D, DR400/125,<br />
modification and/ or repair will introduce<br />
DR400/120, DR400/120 A,<br />
no adverse effectupon the airworthiness<br />
DR400/140, DR400/140 B,<br />
DR400/160, DR400/160 D,<br />
DR400/180 S, DR400/200 R,<br />
DR400/180, DR400/180 R,<br />
DR400/2+2, DR400/500,<br />
DR400/NGL<br />
of the product.<br />
10036788 SOCIETE D'ETUDE ET DE GESTION REV. 1 1900 SERIES Installation of a partition in the rear cabin area. 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.<br />
03.<strong>01</strong>.2<strong>01</strong>2<br />
10038783 SOCIETE D'ETUDE ET DE GESTION 1. AS350B/BB/BA/D/B1/B2 Front Lower Cowling Modification (Reference None AS350B3 change is also applicable to 14.03.2<strong>01</strong>2<br />
2. AS350B3 (SEE CONDITIONS) H-<strong>01</strong>-11-Capot)Separation of cowling in two<br />
helicopters incorporatingmodifications OP-<br />
3. AS355E/F/F1/F2/N/NP halves reassembled by fasteners.Note: This<br />
3369 and OP-4305. Prior to installation of<br />
STC is also applicable to front lower cowlings<br />
this modification it must be determined<br />
modified asper STC <strong>EASA</strong>.R.S.<strong>01</strong>359).<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modifica<br />
10039483 SOCIETE D'ETUDE ET DE GESTION <strong>EASA</strong>.R.S.<strong>01</strong>391 REV. 1 1- AS350B, AS350BA<br />
Installation of an Outside Aerial Picture This STC does not approve Installation of an The installation of this modification by 07.05.2<strong>01</strong>2<br />
1- AS350B3, AS350D<br />
System.Revision 1 adds installation of Outside Aerial PictureSystem on AS350B3 third persons is subject towritten<br />
1- AS350BB, AS350B1, AS350B2 AILIMOUNT III camera system.<br />
helicopters incorporating modification OP- permission of the approval holder and<br />
2- AS355E, AS355F, AS355F1<br />
4305(Arriel2D engine installation). Compliance holding and disposal ofthe approved<br />
2- AS355F2, AS355N, AS355NP<br />
against the requirements ofapplicable appropriate documentation.Prior to<br />
certification basis for AS350B3 helicopters installation of this modification it must be<br />
determined thatthe interre<br />
10039562 SOCIETE D'ETUDE ET DE GESTION REV. 1 1900 Installation of a galley in accordance with<br />
SOCIETE D'ETUDE ET DEGESTION<br />
AERONAUTIQUE (SEGA) Master Document<br />
ListA-11-03-TwinJet-GalleyII_MDoL Edition 1<br />
April 2<strong>01</strong>2<br />
None None 05.06.2<strong>01</strong>2<br />
10038292 SOFINARE R182<br />
Installation of integrated Flight System Garmin None. None. 03.02.2<strong>01</strong>2<br />
TR182<br />
G-500 and DoubleNav/Com/GPS systems<br />
GNS-430W.<br />
10039948 SOFINARE 1900D INSTALLATION OF TERRAIN AWARENESS None (Applicable to All Models Beechcraft The approval holder shall fulfil the <strong>04</strong>.06.2<strong>01</strong>2<br />
AND WARNING SYSTEM (TAWS).<br />
1900D Airplanes)<br />
obligations of Part 21,<br />
Paragraph21A.109.Prior to installation of<br />
this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/or<br />
repair<br />
10<strong>01</strong>3935 SOGERMA SERVICES <strong>EASA</strong>.A.S.0034 REV. 1 AIRBUS A310-3<strong>04</strong> Aircraft modification for 8.33 kHz spacing on<br />
VHF system in accordance with Modification<br />
Approval Sheet SOG 23-878 Issue 1 dated<br />
<strong>01</strong>July 20<strong>04</strong> or later <strong>EASA</strong>-approved<br />
revision.Note: This revision reflects the transfer<br />
of this STC from EADS Sogerma Services to<br />
07.<strong>01</strong>.2008<br />
10<strong>01</strong>4149 SOGERMA SERVICES <strong>EASA</strong>.A.S.<strong>01</strong>27 REV 1 AIRBUS A320-211 Cabin layout change from 144 pax to 155 pax<br />
configuration in accordance with the Master<br />
Drawing List ref. MDL-25-861, issue B, dated<br />
August 6, 20<strong>04</strong> or later <strong>EASA</strong> approved<br />
revision.Note: This revision reflects the transfer<br />
of this STC from EADS Sogerma Serv<br />
10<strong>01</strong>4307 SOGERMA SERVICES <strong>EASA</strong>.A.S.<strong>01</strong>551 REV 1 ATR 42-320 Additional probes in RALI configuration in<br />
accordance with MAS SOG-<strong>01</strong>-459 issue 1<br />
dated 30/11/05Note: This revision reflects the<br />
transfer of this STC from EADS Sogerma<br />
Services to Sogerma Services.<br />
1. MSN 078 Associated STC<br />
No.<strong>EASA</strong>.A.S.<strong>01</strong>219 Revision 1<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 415/<strong>462</strong><br />
07.<strong>01</strong>.2008<br />
<strong>04</strong>.<strong>01</strong>.2008
Change language