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>7074 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>516 REV. 1 TCCA STC SH91-20 AS350 AS350B1, AS350B2 D350-561 Cargo Mirror installations. none Prior to installation of this modification the 03.09.2<strong>01</strong>0<br />
AS350B3, AS350BA , AS350C<br />
installer must determinethat the<br />
AS350D, AS350D1<br />
interrelationship between this modification<br />
AS355E, AS355F, AS355F1<br />
and any otherpreviously installed<br />
AS355F2, AS355N, AS355NP<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product. The installati<br />
10<strong>01</strong>7075 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>518 TC STC SH08-37 ISSUE 1 BELL 205A-1<br />
D205-778 Comfort Seat Installation Prior to installation of this modification the<br />
09.<strong>01</strong>.2009<br />
BELL 205B<br />
installer must determine that the<br />
BELL 212<br />
interrelationship between this modification and<br />
BELL 214B<br />
any other previously installed modification<br />
BELL 214B-1<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.The<br />
10<strong>01</strong>7077 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>526 REV. 2 TCCA STC SH92-16 1. 2<strong>04</strong>B, 205A-1<br />
D212-580 Cargo Mirror/LED Pulse Light None Prior to installation of this modification the 26.11.2<strong>01</strong>0<br />
2. 212, 412, 412EP<br />
InstallationThis revision adds the LED Pulse<br />
installer must determinethat the<br />
3. 214B, 214B-1<br />
light installation to the CargoMirrors.<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 />
10<strong>01</strong>7078 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>528 TCCA STC SH08-08 BELL 205A<br />
Replacement Engine Mount Installation (kit Prior to installation of this modification the<br />
26.02.2009<br />
BELL 205A-1<br />
205-770)<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.<br />
10<strong>01</strong>7079 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>529 TCCA STC SH08-53 AGUSTA AB-412<br />
Procedure Trim Installations (kit D412-775). Prior to installation of this modification the<br />
25.02.2009<br />
AGUSTA AB-412EP<br />
installer must determine that the<br />
BELL 2<strong>04</strong>B<br />
interrelationship between this modification and<br />
BELL 205A-1<br />
any other previously installed modification<br />
BELL 205B<br />
will introduce no adverse effect upon the<br />
BELL 212<br />
BELL 214B<br />
BELL 214B-1<br />
BELL 412<br />
BELL 412 EP<br />
airworthiness of the product.<br />
10027063 DART AEROSPACE Ltd. P-<br />
REV. 1 TCCA STC SH08-38 205A-1, 205B, 212,<br />
SH08-38 Issue 1 "D412-769 Aft Facing Seat For Instructions for Continued Airworthiness Prior to installation of this modification the 05.11.2009<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>493<br />
412, 412EP<br />
Installation"<br />
see Report ICA-D412-769Rev. 0 dated 24 installer must determinethat the<br />
June 2008.<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product. The installati<br />
10028823 DART AEROSPACE Ltd. P-<br />
TCCA STC SH09-16 EC130B4 Traffic Advisory System Installation. None. Prior to installation of this modification it 12.02.2<strong>01</strong>0<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>554<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 />
10028917 DART AEROSPACE Ltd. P-<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>556<br />
10029207 DART AEROSPACE Ltd. P-<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>485<br />
TCCA STC SH09-<strong>04</strong> BELL 2<strong>04</strong>B, 205A-1,<br />
BELL 212, 214B, 214B-1,<br />
BELL 412, 412EP<br />
"Full Vertical Reference Door for Left Hand<br />
Vertical ReferenceOperations"<br />
Full compliance has not been demonstrated for<br />
airworthiness standards29.1303(g)(h)(i)(j),<br />
29.1321(b) and 29.1523(b) for single<br />
pilotoperation from the Left Seat resulting in a<br />
Restricted Categoryclassification. When<br />
conducting vertical reference work from<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 />
TCCA STC SH99-11 ISSUE 5 2<strong>04</strong>B, 205A-1 "Adjustable Engine Mount Kit" 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 />
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