04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
<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>6815 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>180 SH<strong>04</strong>-54 ISSUE1 BELL 2<strong>04</strong>B<br />
BELL 205A<br />
BELL 205A-1<br />
BELL 205B<br />
BELL 212<br />
BELL 214B<br />
BELL 214B-1<br />
BELL 412<br />
Installation of Fuel Purge Canister 26.<strong>04</strong>.2007<br />
10<strong>01</strong>6816 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>181 SH05-11 BELL 2<strong>04</strong>B<br />
BELL 205A<br />
BELL 205A-1<br />
BELL 212<br />
BELL 214B<br />
BELL 214B-1<br />
BELL 412<br />
BELL 412 EP<br />
D212-722 Avionics Console None 30.06.2006<br />
10<strong>01</strong>6822 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>187 SH05-44 BELL 206A<br />
BELL 206L-1<br />
BELL 206L-3<br />
BELL 206L-4<br />
BELL 407<br />
D206/407-728 Skid tube wear plates. 09.10.2007<br />
10<strong>01</strong>6828 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>198 SH03-6 BELL 2<strong>04</strong>B<br />
D205-594 Extended height landing GearTCCA Maintenance of the Extended Height Landing<br />
03.10.2006<br />
BELL 205A<br />
STC SH03-6<br />
Gear must be in accordance with Dart<br />
BELL 205A-1<br />
Aerospace Ltd. ICA-D205-594, Revision 2,<br />
BELL 212<br />
dated 18 July 2005, or later approved<br />
BELL 214B<br />
revisions.Operation of the Bell 214B and 214B-<br />
BELL 214B-1<br />
1 model types with the Extended Height<br />
Landing Gear<br />
10<strong>01</strong>6833 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>2<strong>04</strong> SH96-69 BELL 205A<br />
Installation of Heli Access Steps i.a.w.<br />
02.06.2006<br />
BELL 205A-1<br />
BELL 205B<br />
BELL 212<br />
BELL 214B<br />
BELL 214B-1<br />
BELL 412<br />
BELL 412 EP<br />
Transport Canada STC SH96-69, issue 7<br />
10<strong>01</strong>6866 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>242 TCCA STC SH96-120 BELL 2<strong>04</strong><br />
D205-541 Heli-Utility Basket in accordance 1. VFR Only;2. Doors to be closed at all<br />
29.09.2006<br />
BELL 205A<br />
with Transport Canada STC SH96-120, Issue times during flight;3. Maximum Load 136 kg<br />
BELL 205A-1<br />
3, dated May 16, 2006<br />
(300 lb) or 100kg (220lb) if middle support is<br />
BELL 205B<br />
not installed;4. This STC is approved only for<br />
BELL 212<br />
the product configuration as defined in the<br />
BELL 214B<br />
BELL 214B-1<br />
BELL 412<br />
BELL 412 CF<br />
BELL 412 EP<br />
approved design data r<br />
10<strong>01</strong>6876 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>253 TCCA STC SH<strong>04</strong>-17 ROBINSON R44 Installation of D<strong>04</strong>4-715 Cargo Mirrors i.a: with None<br />
TCCA STC SH<strong>04</strong>-17<br />
11.12.2006<br />
10<strong>01</strong>6877 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>254 TCCA STC SH<strong>04</strong>-12 ROBINSON R22 ALPHA Installation of D022-716 Cargo Mirrors i.a. with<br />
12.12.2006<br />
ROBINSON R22 BETA<br />
TCCA STC SH<strong>04</strong>-12<br />
10<strong>01</strong>69<strong>01</strong> DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>278 REV. 1 EUROCOPTER DEUTSCHLAND D135-751 Skidtube and Skidtube Extension<br />
10.12.2008<br />
EC-135-<br />
Installation iaw FAA STC SR<strong>01</strong>709SE.<br />
10<strong>01</strong>6903 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>280 REV. 2 TCCA STC SH06-27 AS350B, AS350B1, AS350B2 Cross Tube Installation in accordance with None Prior to installation of this modification it 03.09.2<strong>01</strong>0<br />
AS350B3, AS350BA, AS350D Transport Canada STC SH06-27,Issue 1,<br />
must be determined thatthe<br />
AS355E, AS355N, AS355NP dated 16 August 2006.<br />
interrelationship between this modification<br />
AS355F, AS355F1, AS355F2<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>6908 DART AEROSPACE Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>289 REV. 1 TCCA STC SH06-39 ISSUE 2 AGUSTA A119, AW119 MKII TCA STC No. SH06-39 Issue 2 - "Heli-Utility<br />
Basket Installation" - Thisinstallation consists in<br />
a box, fixed to the landing gear, for<br />
goodstransportation.<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 />
10.02.2<strong>01</strong>1<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 162/<strong>462</strong>
Change language