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 />
10038296 INAER MAINTENANCE S.A.U. DGAC-E NO 138 1. BELL 206B, 206L<br />
Transfer of STC "DGAC-E No. 138"<br />
None Prior to installation of this modification it 08.03.2<strong>01</strong>2<br />
2. AB206B<br />
(Certificado de componente aeronáuticoNo.<br />
must be determined thatthe<br />
138 de 09-08-1996), Power lines cleaning<br />
interrelationship between this modification<br />
system with high pressurewater with "DGAC-E<br />
and any other previouslyinstalled<br />
Certificate Data Sheet No. 138" from<br />
modification and/ or repair will introduce<br />
Heliservicio toInaer Maintenance S.A.U. (DOA<br />
no adverse effectupon the airworthiness<br />
No. <strong>EASA</strong>.21J.1<br />
of the product.<br />
10<strong>04</strong>0333 INAER MAINTENANCE S.A.U. P.68 C<br />
P.68 OBSERVER<br />
P.68 OBSERVER 2<br />
"External load mount". Installation of a mount to<br />
hold external loads inthe existing<br />
photogrammetric hatch, according to<br />
Certification Plan"INAER.M11/037/25-PdC",<br />
Revision 0, Date: 21/06/2<strong>01</strong>2.<br />
10<strong>04</strong>0926 INAER MAINTENANCE S.A.U. REV. 1 B200GT "Stretcher kit Avfab 32-<strong>01</strong>17". Installation of a<br />
stretcher kit replacingLH seats (rows 2 and 3),<br />
according to Certification Plan<br />
"INAER.M12/<strong>04</strong>4/25-PdC", Revision 0, Date:<br />
27/07/2<strong>01</strong>2.<br />
10029799 INDIGOSAT 208 / 208B Installation of IndigoOne Satellite Tracking and<br />
Communication System(Kit Part No.<br />
IGO1_MA1236_<strong>01</strong>R1-1) in accordance with<br />
CASA (Australia)STC SVA 513<br />
10<strong>01</strong>6562 INFINION CERTIFICATION<br />
ENGINEERING<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 />
26.06.2<strong>01</strong>2<br />
None The installation of this modification by<br />
third persons is subject towritten<br />
permission of the approval holder and<br />
holding and disposal ofthe approved<br />
appropriate documentation. Prior to<br />
installation of this modification it must be<br />
determined thatthe interr<br />
Effected S/N see in Installation Manual IS-IM-<br />
2007-0<strong>01</strong>, Issue C<br />
<strong>EASA</strong>.IM.A.S.02948 REV. 1 TCCA STC SA06-30 BAE JETSTREAM 3100 Concorde RG-380 Battery Installation. 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. The install<br />
10<strong>01</strong>5538 INFLIGHT CANADA Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>422 REV. 1 TCCA STC C-LSA95-037/D AIRBUS A320-232 SONY TRANS COM Passenger Entertainment<br />
System installationNote: This STC had to be<br />
revised due to a correction to the holder of the<br />
original STC.<br />
10<strong>01</strong>6609 INFLIGHT CANADA Inc. <strong>EASA</strong>.IM.A.S.03029 TCCA STC O-LSA03-127/D BOMBARDIER CL-600-2B19 Honeywell SCS-1000 Mini-M Aero SATCOM<br />
System and Securaplane Camera Installation.<br />
10027294 INFLIGHT CANADA Inc. P-<br />
<strong>EASA</strong>.IM.A.S.03187<br />
REV. 4 TCCA STC SA09-28 737-800 Rockwell Collins dPAVES Overhead<br />
Passenger Entertainment System, TCCASTC<br />
Number: SA09-28 Issue 3 dated Nov 16, 2009.<br />
This revision consistsin removing the limitation<br />
on EWIS ICA<br />
10030534 INFLIGHT CANADA Inc. REV. 1 TCCA STC O-LSA08-<strong>04</strong>5/D 767-300 Audio Video on Demand (AVOD) and In-Seat<br />
Power Supply (ISPS) SystemInstallation<br />
1. This STC is limited to the A320 MSN's 496<br />
and 5252. This STC is approved only for the<br />
product configuration as defined in the<br />
approved design data referred to in the<br />
paragraph "Description". Compatibility with<br />
other aircraft/engine configurations<br />
1. DECA Aviation / Inflight Canada<br />
Modification Summary MS03055, Revision 4,<br />
dated 16 October 20<strong>04</strong>, or later approved<br />
revision.2. DECA Aviation / Inflight Canada<br />
Instructions for Continued Airworthiness<br />
ICA03055, Revision 2, dated 12 October 20<strong>04</strong>,<br />
or<br />
08.08.2<strong>01</strong>2<br />
Prior to installation of this modification it 21.<strong>04</strong>.2<strong>01</strong>0<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 />
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 />
16.09.2008<br />
27.11.2006<br />
<strong>04</strong>.12.2008<br />
<strong>04</strong>.06.2<strong>01</strong>2<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 />
10.09.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 277/<strong>462</strong>
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