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>4518 DAO AVIATION A/S <strong>EASA</strong>.A.S.02596 Avionics upgrade with following equipment<br />
(DFE-DO-0075-EPL-<strong>01</strong> Equipment and Parts<br />
List.(Rev. 1)1 GMA 347 Audiopanel<br />
Garmin 1 GNS<br />
13.07.2006<br />
10<strong>01</strong>6712 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.00710 REV. 1 TCCA STC SH<strong>04</strong>-7 BELL 205A<br />
530 COM/ NAV/ GPS Garmin<br />
1 GNS<br />
Installation of D412-702 Shoulder Harness Kits. Prior to installation of this modification the<br />
09.08.2007<br />
BELL 205A-1<br />
Transport Canada STC No SH<strong>04</strong>-7 issue 1 installer must determine that the<br />
BELL 205B<br />
dated 6th February 20<strong>04</strong>. The purpose of these interrelationship between this modification and<br />
BELL 212<br />
kits is to add shoulder harnesses to existing any other previously installed modification will<br />
BELL 214B<br />
seats that are only equipped with lap belts. introduce no adverse effect upon the<br />
BELL 214B-1<br />
BELL 412<br />
BELL 412 EP<br />
airworthiness of the product. The install<br />
10<strong>01</strong>6723 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>021 SH<strong>04</strong>-31 BELL 205A-1<br />
BELL 205B<br />
BELL 212<br />
BELL 214B<br />
BELL 214B-1<br />
BELL 412<br />
BELL 412 CF<br />
BELL 412 EP<br />
Installation of Replacement Window Kits 02.<strong>01</strong>.2006<br />
10<strong>01</strong>6748 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>074 TCCA STC SH<strong>04</strong>-30, ISSUE 2 ROBINSON R22 ALPHA Validation of TCCA STC SH<strong>04</strong>-30 for the 1. Installation and Maintenance in accordance<br />
14.06.2005<br />
ROBINSON R22 BETA<br />
installation of Cabin Floor Protectors. with the above referenced Technical<br />
Documentation.2. This STC is approved only<br />
for the product configuration as defined in the<br />
approved design data referred to in the<br />
paragraph "Description". Compatibility with<br />
10<strong>01</strong>6749 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>075 TCCA STC SH<strong>04</strong>-40, ISSUE 1 ROBINSON R44<br />
ROBINSON R44 II<br />
10<strong>01</strong>6750 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>076 TCCA STC SH05-7, ISSUE 1 ROBINSON R44<br />
ROBINSON R44 II<br />
10<strong>01</strong>6756 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>085 SH05-10, ISSUE 1 BELL 205B<br />
BELL 212<br />
BELL 214B<br />
BELL 214B-1<br />
BELL 412<br />
BELL 412 CF<br />
BELL 412 EP<br />
10<strong>01</strong>6757 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>086 SH94-38, ISSUE 2 SIKORSKY S-76A<br />
SIKORSKY S-76C<br />
10<strong>01</strong>6758 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>087 TCCA STC SH05-14 ROBINSON R22 ALPHA<br />
ROBINSON R22 BETA<br />
10<strong>01</strong>6759 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>088 TCCA STC SH05-13 ROBINSON R44<br />
ROBINSON R44 II<br />
10<strong>01</strong>6814 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>179 TCCA STC SH<strong>01</strong>-5 ISSUE 2 BELL 206A<br />
BELL 206L<br />
BELL 206L-1<br />
BELL 206L-3<br />
BELL 206L-4<br />
BELL 407<br />
Validation of TCCA STC SH<strong>04</strong>-40 for the<br />
installation of Cabin Floor Protectors.<br />
Validation of TCCA STC SH05-7 for the<br />
Installation of a Cold Weather Baffle Kit for<br />
Cold Weather operation of Robinson R44 and<br />
R44II.<br />
1. Installation must be performed in<br />
accordance with Installation Instructions IIN-<br />
D<strong>04</strong>4-719.2. Maintenance in accordance with<br />
Instructions for Continued Airworthiness ICA-<br />
D<strong>04</strong>4-719.3. This STC is approved only for the<br />
product configuration as defined in the<br />
1. Installation must be performed in<br />
accordance with Installation Instructions IIN-<br />
D<strong>04</strong>4-717.2. Maintenance in accordance with<br />
Instructions for Continued Airworthiness ICA-<br />
D<strong>04</strong>4-717.3. This STC is approved only for the<br />
product configuration as defined in the<br />
14.06.2005<br />
14.06.2005<br />
Spacedoor Installation 02.<strong>01</strong>.2006<br />
Installation of Cargo Mirrors 25.<strong>01</strong>.2006<br />
Installation of Replacement Window Kits in<br />
accordance with TCCA STC SH05-14.<br />
Installation of Replacement Window Kit in<br />
accordance with TCCA STC SH05-13.<br />
1. Installation, Operation and Maintenance<br />
must be held in accordance with the above<br />
referenced Technical Documentation. 2. This<br />
STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Descrip<br />
1. This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
Landing Gear Crosstubes This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 161/<strong>462</strong><br />
14.06.2005<br />
13.06.2005<br />
03.07.2006
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