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>6792 FUGRO AIRBORNE SURVEYS <strong>EASA</strong>.IM.R.S.<strong>01</strong>140 TCCA STC SH 98-37 EUROCOPTER FRANCE AS 350 Installation of Fugro Airborne Surveys Electro- 1. STC SH 98-37 Supplemental Flight Manual<br />
11.10.2005<br />
B<br />
Magnetometer Boom & Geosurvey Equipment 4537-<strong>01</strong> Revision <strong>01</strong> approved 18 July 2000<br />
EUROCOPTER FRANCE AS 350 installation<br />
or later approved revisions.2. DECA Aviation<br />
B1<br />
Flight Manual Supplement No. 453707<br />
EUROCOPTER FRANCE AS 350<br />
Revision 1, dated 18 July 2000 or later<br />
B2<br />
approved revision3. This STC is approved only<br />
EUROCOPTER FRANCE AS 350<br />
B3<br />
EUROCOPTER FRANCE AS 350<br />
BA<br />
EUROCOPTER FRANCE AS 350<br />
D<br />
EUROCOPTER FRANCE AS<br />
355E<br />
EUROCOPTER FRANCE AS<br />
355F<br />
EUROCOPTER FRANCE AS<br />
355F1<br />
EUROCOPTER FRANCE AS<br />
355F2<br />
for<br />
10<strong>01</strong>6428 G&D AERO PRODUCTS INC. <strong>EASA</strong>.IM.A.S.02767 FAA STC SA7063NM BEECH 200<br />
BEECH 300<br />
Installation of Acrylic window liners None 05.03.2008<br />
10<strong>01</strong>4342 GAMA ENGINEERING Ltd. <strong>EASA</strong>.A.S.<strong>01</strong>602 BEECH 200 Major Avionic Upgrade 06.<strong>04</strong>.2006<br />
10<strong>01</strong>4355 GAMA ENGINEERING Ltd. <strong>EASA</strong>.A.S.<strong>01</strong>620 BEECH 200, SUPER KING AIR Major Avionic System Upgrade 19.12.2005<br />
10<strong>01</strong>4357 GAMA ENGINEERING Ltd. <strong>EASA</strong>.A.S.<strong>01</strong>622 REV. 1 BEECH B200C, SUPER KING AIR Ground Use Battery 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 />
10.03.2<strong>01</strong>1<br />
10<strong>01</strong>4389 GAMA ENGINEERING Ltd. <strong>EASA</strong>.A.S.<strong>01</strong>675 REV. 1 BAE.125 SERIES 800 Title: Upgrade of the dual Flight Management<br />
System (FMS).Description of change: The<br />
original dual Honeywell FMZ-900 FMS<br />
isupgraded to a dual Honeywell FMZ-2000<br />
FMS.<br />
The installer must determine whether this<br />
design change is compatiblewith previously<br />
approved modifications.<br />
Prior to installation of this modification it 05.10.2<strong>01</strong>2<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 />
10<strong>01</strong>4502 GAMA ENGINEERING Ltd. <strong>EASA</strong>.A.S.02570 BEECH 200 Mode S Transponder Installation. Beech 200 Series. As per AFMS7060<strong>01</strong> Issue<br />
1<br />
06.02.2008<br />
10<strong>01</strong>4542 GAMA ENGINEERING Ltd. <strong>EASA</strong>.A.S.02629 REV. 1 A340-311, A340-312, A340-313. Child Restraint System - CRS - Installation in Limitations in accordance with § 4 - Limitations Prior to installation of this modification it 10.12.2<strong>01</strong>2<br />
A340-300<br />
of the above mentionedDDP, ref. No. DDP- must be determined thatthe<br />
1785-026.All cabin interiors must be evaluated interrelationship between this modification<br />
for compatibility of the ChildRestraint System and any other previouslyinstalled<br />
(CRS). The CRS is not approved for<br />
modification and/ or repair will introduce<br />
aeroplanes that arenot defined by § 4 no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong>4543 GAMA ENGINEERING Ltd. <strong>EASA</strong>.A.S.02630 REV. 1 A340-643 Child Restraint System - CRS - Installation in<br />
A340-600<br />
Limitations in accordance with § 4 - Limitations Prior to installation of this modification it 10.12.2<strong>01</strong>2<br />
of the above mentionedDDP, ref. No. DDP- must be determined thatthe<br />
1785-026.All cabin interiors must be evaluated interrelationship between this modification<br />
for compatibility of the ChildRestraint System and any other previouslyinstalled<br />
(CRS). The CRS is not approved for<br />
modification and/ or repair will introduce<br />
aeroplanes that arenot defined by § 4 no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong>4544 GAMA ENGINEERING Ltd. <strong>EASA</strong>.A.S.02631 REV. 1 B747-400 Installation of MAGE Child Restraint System as 1. This STC only covers the installation of the Prior to installation of this modification it 20.06.2<strong>01</strong>2<br />
detailed in ModificationLeaflet for Modification MAGE Child RestraintSystem on Virgin Atlantic must be determined thatthe<br />
no. B744-1795.<br />
Airways Boeing 747-400 Aircraft, as defined interrelationship between this modification<br />
inMAGE DDP1785-026 and in accordance with and any other previouslyinstalled<br />
the instructions and limitationsdefined in MAGE modification and/ or repair will introduce<br />
Crew Manual Supplement TN 17<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong><strong>462</strong>6 GAMA ENGINEERING Ltd. <strong>EASA</strong>.A.S.02764 HAWKER 800 XP Installation of a L-3 Avionics F1000 Flight Data<br />
Recorder.<br />
This Installation is intended for compliance with<br />
JAR-OPS 1.715. This STC however grants no<br />
operational approval to this installation, that will<br />
need to be obtained from the State of registry<br />
for the particular aircraft involved as defined in<br />
JAR OPS 1.715<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 226/<strong>462</strong><br />
17.10.2006
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