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>6984 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>389 REV. 1 TCCA STC SH93-4 SEE <strong>EASA</strong> APPROVED MODEL Bearpaw Installation none Prior to installation of this modification it 22.09.2<strong>01</strong>0<br />
LIST<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>6991 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>398 TCCA STC SH92-20, ISSUE 2; FAA BELL 2<strong>04</strong>B<br />
BELL 205A<br />
BELL 205A-1<br />
10<strong>01</strong>6996 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>405 REV. 2 TCCA STC SH94-14 1. AS350B/B1/B2/B3/BA/D/D1<br />
1. EC130B4<br />
2. AS355E/F/F1/F2/N/NP<br />
D2<strong>04</strong>-575/D205-576 Cabin Heating Systems,<br />
Transport Canada STC SH92-20 Issue 2 dated<br />
14 May 1992<br />
D350-607, D130-7<strong>01</strong> Basket InstallationsThis<br />
revision adds the models AS355N and NP.<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 will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
03.09.2008<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 />
24.<strong>01</strong>.2<strong>01</strong>1<br />
10<strong>01</strong>7030 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>449 REV. 1 TC STC SH05-45 BELL 206A<br />
BELL 206B<br />
D206-746 Shroud Air Flow Heater System. 16.<strong>04</strong>.2008<br />
10<strong>01</strong>7031 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>451 TCCA STC SH99-221 ISSUE 1 EUROCOPTER FRANCE EC 120 D120 -638 Bearpaw Installation. 1. Prior to installation of this modification the<br />
13.08.2008<br />
B<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>7032 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>452 TCCA STC SH<strong>01</strong>-25 ISSUE 1 EUROCOPTER FRANCE EC 120 D120 -639 Wearplate Installation. 1. Prior to installation of this modification the<br />
13.08.2008<br />
B<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>7033 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>456 TCCA STC SH08-5 EUROCOPTER FRANCE AS 350 D350-766 interior Trim Kit Installations<br />
B<br />
EUROCOPTER FRANCE AS 350<br />
B1<br />
EUROCOPTER FRANCE AS 350<br />
B2<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 350<br />
D1<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 />
EUROCOPTER FRANCE AS<br />
355N<br />
EUROCOPTER FRANCE AS<br />
355NP<br />
30.<strong>04</strong>.2008<br />
10<strong>01</strong>7059 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>492 REV. 1 TCCA STC SH08-40 BELL 212<br />
Replacement Glareshield Installation. Prior to installation of this modification the<br />
<strong>04</strong>.05.2009<br />
BELL 412<br />
installer must determine that the<br />
BELL 412 EP<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. The in<br />
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