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 />
10029406 GAMA ENGINEERING Ltd. REV. 1 1. 35-33, 35-A33, 35-B33 Amendment to existing STC 10029406 to add None Prior to installation of this modification it 03.<strong>01</strong>.2<strong>01</strong>1<br />
2. 35-C33, 35-C33A, E33, E33A TAWS-B functionality andinclude optional<br />
must be determined thatthe<br />
3. E33C, F33, F33A, F33C, H35 GAD43 autopilot interface unit.<br />
interrelationship between this modification<br />
4. J35, K35, M35, N35, P35<br />
and any other previouslyinstalled<br />
5. S35, V35, V35A, V35B<br />
modification and/ or repair will introduce<br />
6. 36, A36, A36TC, B36TC<br />
no adverse effectupon the airworthiness<br />
7. 95-55, 95-A55, 95-B55<br />
8. 95-C55, D55, E55, 58, 58P<br />
9. 58TC<br />
of the product.<br />
10029499 GAMA ENGINEERING Ltd. BEECH 90 Navigation/ communications systems upgrade. 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 />
29.03.2<strong>01</strong>0<br />
10029724 GAMA ENGINEERING Ltd. P-<strong>EASA</strong>.A.S.03861 REV. 1 PA-28 Installation of Garmin G500/G600 EFIS<br />
PFD/ND.<br />
This change is limited to the configuration Prior to installation of this modification the 15.<strong>04</strong>.2<strong>01</strong>0<br />
defined in Change StatementCS1050-02 Issue installer must determinethat the<br />
1 or later approved revision.<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product.<br />
10029726 GAMA ENGINEERING Ltd. REV. 1 PIPER PA-28 16.<strong>04</strong>.2<strong>01</strong>0<br />
1003<strong>04</strong>65 GAMA ENGINEERING Ltd. P-<strong>EASA</strong>.R.S.<strong>01</strong>596 BO105 Mounting boom for camera<br />
CAT-A-operation is prohibited (CAT-A- The approval holder shall fulfill the 16.06.2<strong>01</strong>0<br />
installation.Certification of the installation of a operation is excluded<br />
obligations of Part 21,<br />
mounting boom which can be usedfor fromcertification).Maximum weight for cameras Paragraph21.A109.Prior to installation of<br />
installation of a camera. The camera<br />
used is 43.1 kg and maximum frontal area this modification it must be determined<br />
installation provisions and themaximum weight is1470 sqcm.The used camera has to be thatthe interrelationship between this<br />
and frontal area of cameras which can be used certified separately.<br />
modification and any other<br />
with themountin<br />
previouslyinstalled modification and/ or<br />
repai<br />
10030863 GAMA ENGINEERING Ltd. P-<strong>EASA</strong>.A.S.03823 EXTRA EA-300 / L External camera installation None None 09.07.2<strong>01</strong>0<br />
10031729 GAMA ENGINEERING Ltd. PIPER PA-34 ALL SERIES Installation of Garmin G500/G600 PFD/ND This change is limited to the configuration Prior to installation of this modification it 08.09.2<strong>01</strong>0<br />
defined in Change StatementCS11<strong>01</strong>-<strong>01</strong> Issue must be determined thatthe<br />
1 or later approved revision.<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 />
10031769 GAMA ENGINEERING Ltd. REV. 1 SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
10032795 GAMA ENGINEERING Ltd. REV. 1 112, 112TC, 112B, 112TCA,<br />
114, 114A, 114B, 114TC<br />
Child Restraint System - CRS - Installation in<br />
Various Aircraft<br />
Aspen EFD1000 Software Version 2.3.1<br />
upgrade<br />
Limitations in accordance with § 4 - Limitations<br />
of the above mentionedDDP, ref. No. DDP-<br />
1898-<strong>01</strong>2All cabin interiors must be evaluated<br />
for compatibility of the ChildRestraint System<br />
(CRS). The CRS is not approved for<br />
aeroplanes that arenot defined by § 4 o<br />
Procedures for extending the listing of<br />
approved aeroplane installationsin § 4 of<br />
the above referenced DDP are defined in<br />
Certification Plan No.TN 1898-005.Prior<br />
to installation of this modification it must<br />
be determined thatthe interrelationship<br />
06.07.2<strong>01</strong>2<br />
None<br />
between t<br />
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 />
03.05.2<strong>01</strong>2<br />
10033225 GAMA ENGINEERING Ltd. PA-44-180 & PA-44-180T Installation of Garmin G500/G600 PFD/ND 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 />
05.<strong>01</strong>.2<strong>01</strong>1<br />
10033770 GAMA ENGINEERING Ltd. P-<strong>EASA</strong>.A.S.03723 CESSNA 310 Introduction of EXP5000 electronic primary<br />
flying display and dualGNS430W GPS<br />
navigation/communication units.<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. The in<br />
27.07.2009<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 228/<strong>462</strong>
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