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 />
10029712 DART AEROSPACE Ltd. P-<br />
TCCA STC SH07-36 A119 & AW119 MKII TCA STC SH07-36 Issue 2 "Replacement Not Applicable Prior to installation of this modification it 15.<strong>04</strong>.2<strong>01</strong>0<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>380<br />
Windows Kit" - D119-755-<strong>01</strong>1/-14 -This STC<br />
must be determined thatthe<br />
involves removing of the existing window and<br />
interrelationship between this modification<br />
installing a flatwindow (-<strong>01</strong>1) in LH or RH crew<br />
and any other previouslyinstalled<br />
door or installing a bubble window (-14)in the<br />
modification and/or repair will introduce<br />
RH crew door)<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10031514 DART AEROSPACE Ltd. TCCA STC SH05-4 AS350 B, B1, B2, B3, BA, D Installation of an Auxiliary Side Locker Fuel<br />
Tank.<br />
10032253 DART AEROSPACE Ltd. TCCA STC SH09-37 ISSUE 1 1. 214B, 214B-1<br />
2. 212, 412, 412 EP<br />
3. 2<strong>04</strong>B, 205A-1<br />
10033253 DART AEROSPACE Ltd. TCCA STC SH10-44 206, A, A1, B, B1<br />
L, L1, L3, L4, 407<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 />
20.08.2<strong>01</strong>0<br />
D412-791 Safety Enhancement kits 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 />
05.11.2<strong>01</strong>0<br />
Automatic Door Opener Kits (Cabin and<br />
Baggage Doors).<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 />
07.<strong>01</strong>.2<strong>01</strong>1<br />
10034340 DART AEROSPACE Ltd. TCCA STC SH10-49 429 Installation of UltraPaws. 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 />
25.03.2<strong>01</strong>1<br />
10034634 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>560 TCCA STC SH92-18 AS350B, BA, B1, B2, B3, D, D1 D350-567 Vertical Reference Window<br />
Installations. Addition of AS350Dl tolist of<br />
models.This STC revises and supersedes<br />
DGAC France STC 84-5[1103, dated<br />
27September 2002.<br />
None Prior to installation of this modification the 17.07.2009<br />
installer must determinethat the<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 />
10034636 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>561 TCCA STC SH92-18 AS355E, F, F1, F2, N, NP D350-567 Vertical Reference Window None Prior to installation of this modification the 31.07.2009<br />
Installations.This STC is a revision of and<br />
installer must determinethat the<br />
supersedes DGAC-F STC 168-5111<strong>04</strong> dated<br />
interrelationship between this modification<br />
27September 2002 for addition of AS355N and<br />
and any otherpreviously installed<br />
NP to list of models.<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product. The installati<br />
10034637 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>453 TCCA STC SH02-33 1. AS350 D, B, B1, B2, BA, B3<br />
1. (OP-3369 OPTION<br />
EXCLUDED)<br />
2. AS355 E, F, F1, F2, N<br />
10035429 DART AEROSPACE Ltd. REV. 2 TCCA STC SH11-1 206L, 206L-1, 206L-3, 206L-4<br />
407<br />
Installation of Dual High Back Seat, Left<br />
Forward Position (Modificationapproved by<br />
TCCA under STC SH02-33 issue 1)<br />
D407-797 Heli Utility Basket and Heli Access<br />
Step Installation, Revisionto STC 10035429 to<br />
add D407-797-311 Heli Access Step.<br />
None Prior to installation of this modification the 03.06.2009<br />
installer must determinethat the<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 />
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 />
28.11.2<strong>01</strong>1<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 166/<strong>462</strong>
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