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 />
10<strong>01</strong>4927 SOCIETE D'ETUDE ET DE GESTION <strong>EASA</strong>.A.S.03177 BEECH 90 Installation of a support base for a stretcher. 08.10.2007<br />
10<strong>01</strong>5255 SOCIETE D'ETUDE ET DE GESTION <strong>EASA</strong>.A.S.03707 BEECH 1900 Installation of a galley. 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<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.<br />
10<strong>01</strong>5294 SOCIETE D'ETUDE ET DE GESTION <strong>EASA</strong>.A.S.03838 PIPER PA-34 Pneumatic deicer removal. 1. 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.2.<br />
10<strong>01</strong>7182 SOCIETE D'ETUDE ET DE GESTION <strong>EASA</strong>.R.S.<strong>01</strong>315 EUROCOPTER FRANCE AS<br />
355F1<br />
Installation of rack and sending/reception<br />
antennae.<br />
10<strong>01</strong>7237 SOCIETE D'ETUDE ET DE GESTION <strong>EASA</strong>.R.S.<strong>01</strong>423 EUROCOPTER FRANCE AS 350 Modification H-25-<strong>04</strong>-07-SFP - installation of<br />
deployable antenna mounted on landing gear.<br />
10<strong>01</strong>7238 SOCIETE D'ETUDE ET DE GESTION <strong>EASA</strong>.R.S.<strong>01</strong>424 EUROCOPTER FRANCE AS 355<br />
SERIE<br />
10027064 SOCIETE D'ETUDE ET DE GESTION P-<strong>EASA</strong>.A.S.03925 REV. 1 MS893 A, B, E, E-D<br />
MS894 A, C, E<br />
RALLYE 235 A, C, E, E-D, F<br />
Modification H-25-<strong>04</strong>-07-SFP - installation of<br />
deployable antenna mounted on landing gear.<br />
Reduction of maximum take off and landing<br />
weights to 1000 kg.<br />
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<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.<br />
This STC provides approval for the installation<br />
and deployment of the antenna. A separate<br />
approval is required for the installationand<br />
operation of any equipment transmitting<br />
through the antenna.The installation of this<br />
modification by third persons is sub<br />
This STC provides approval for the installation<br />
and deployment of the antenna. A separate<br />
approval is required for the installationand<br />
operation of any equipment transmitting<br />
through the antenna.Prior to installation of this<br />
modification the installer must<br />
MS894 models: seating capacity limited to 3<br />
persons, pilot included.Rallye 235 models:<br />
seating capacity limited to 3 persons,<br />
pilotincluded. Fuel tanks capacity limited to 240<br />
l (2*120l).The airplane configurations listed in<br />
attachment 1 are excluded from<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
16.<strong>01</strong>.2009<br />
21.<strong>04</strong>.2009<br />
12.06.2008<br />
25.09.2008<br />
25.09.2008<br />
Prior to installation of this modification the 08.<strong>01</strong>.2<strong>01</strong>0<br />
installer must determinethat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
10027989 SOCIETE D'ETUDE ET DE GESTION P-<strong>EASA</strong>.A.S.03973 DHC-8-100, -200, -300 Installation of ELT KANNAD 406 AF- None<br />
product.The installatio<br />
Upon completion of the change the 24.11.2009<br />
COMPACT or ARTEX ME406<br />
aircraft maintenance program must<br />
beupdated to reflect the recurrent<br />
inspections as defined by<br />
KANNADDOC08038C or ARTEX<br />
Document 570-1600 Rev. G or later<br />
revision of thedocuments approved by<br />
<strong>EASA</strong> The approval holder shall<br />
10028678 SOCIETE D'ETUDE ET DE GESTION <strong>EASA</strong>.R.S.<strong>01</strong>561 EUROCOPTER FRANCE AS 350<br />
SERIE<br />
31.07.2009<br />
10028679 SOCIETE D'ETUDE ET DE GESTION <strong>EASA</strong>.R.S.<strong>01</strong>560 EUROCOPTER FRANCE AS 355<br />
SERIE<br />
31.07.2009<br />
10028814 SOCIETE D'ETUDE ET DE GESTION P-<strong>EASA</strong>.R.S.<strong>01</strong>492 REV. 3 1. AS350 B, AS350 B1, AS350 B2 Modifications H-25-05-06-SFP and H-25-05-06- This STC is not applicable to AS350B3 model Prior to installation of this modification the 26.07.2<strong>01</strong>2<br />
1. AS350 B3, AS350 BA<br />
SFPAnt - Installation of arack and<br />
helicopters withmodification OP-4305 (Arriel installer must determinethat the<br />
1. AS350 D, AS350 BB<br />
transmitting/receiving antennaeNotes: Initial 2D engine installation) incorporated.<br />
interrelationship between this modification<br />
2. AS355 E, AS355 F, AS355 F1 issue of this STC covered installation of a rack -<br />
and any otherpreviously installed<br />
2. AS355 F2, AS355 N, AS355 NP modificationH-25-05-06-SFPRevision 1 to this<br />
modification will introduce no adverse<br />
STC added installation of transmitt<br />
effect uponthe airworthiness of the<br />
product.<br />
10029480 SOCIETE D'ETUDE ET DE GESTION AS350 B2 Installation system for "EC120 type" seats on<br />
Eurocopter AS350B2 -modification H-08-09-<br />
Siège<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.<br />
26.03.2<strong>01</strong>0<br />
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