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>6725 EUROCOPTER CANADA Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>023 REV. 1 TCCA STC SH 96-32 AS350BA, AS350B2, AS350B3 Left-side pilot configuration Note: Revision of None Prior to installation of this modification it 13.12.2<strong>01</strong>0<br />
<strong>EASA</strong> STC ref. <strong>EASA</strong>.IM.R.S.<strong>01</strong>023 being a<br />
must be determined thatthe<br />
validation ofTCCA STC SH 96-32 at issue 7.<br />
interrelationship between this modification<br />
This STC revision is validation of TCCASTC<br />
and any other previouslyinstalled<br />
SH 96-32 at issue 11 and includes the left-side<br />
modification and/ or repair will introduce<br />
pilot configurationchange made to<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong>6728 EUROCOPTER CANADA Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>031 TCCA STC SH 97-15 AS 350 B/BA/B1/B2/B3/D Installation of LH and/or RH Cargo pods 1. This STC is approved only for the product<br />
(Squirrel Cheeks")Master Drawing List MDL-94- configuration as defined in the approved design<br />
0<strong>04</strong> and associated maintenance<br />
data referred to in the paragraph "Description".<br />
instructionsFlight manual supplement FMS- Compatibility with other aircraft/engine<br />
ECL-9, revision 2 or later TCCA approved configurations shall be determined by the<br />
revisions<br />
installer.<br />
10<strong>01</strong>6747 EUROCOPTER CANADA Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>073 TCCA STC SH 96-31 AS 350 B/BA/BB/D/B1/B2/B3<br />
AS 355 E/F/F1/F2<br />
EUROCOPTER FRANCE AS<br />
355F2<br />
Relocation of higher capacity battery to tail<br />
boomMaster Drawing List MDL-<strong>04</strong>-003 and<br />
MDL-96-0<strong>01</strong> associated installation procedure<br />
and maintenance instructions.Flight Manual<br />
Supplement attached to STC SH96-31 issue 6,<br />
approved 25 March 1996 or later TCCA ap<br />
10<strong>01</strong>6825 EUROCOPTER CANADA Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>195 TCCA STC SH00-1 ISSUE 3 AS 350 B, AS 350 B1, AS 350 B2 Installation of high visibility main and aft cabin<br />
AS 350 B3, AS 350 BA, AS 350 D doorsrefer to TCCA STC SH00-1 issue N°3,<br />
July 25, 2003<br />
10<strong>01</strong>6845 EUROCOPTER CANADA Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>221 TCCA STC SH05-18 AS 350 B/B1/B2/B3/BA/D/D1 Installation of Forward Short High-visibility<br />
Doors (350-202414).<br />
10<strong>01</strong>6935 EUROCOPTER CANADA Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>321 TCCA STC SH97-34 ISSUE 3 AS 350 B/B1/B2/B3/BA/D<br />
AS 355 E/F/F1/F2/N<br />
Installation of Forward Opening Rear Cargo<br />
Doors.(Modification approved by TCCA under<br />
STC SH97-34 Issue 3).<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 />
Refer to TCCA STC SH00-1 issue N°3, July<br />
25, 2003<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 />
1; This STC is approved only for the production<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.Installation of th<br />
10<strong>01</strong>7000 EUROCOPTER CANADA Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>410 TCCA STC SH03-33 EC 130 B4 Cargo Pods Installation 12.06.2008<br />
10038250 EUROCOPTER CANADA Ltd. TCCA STC SH94-29 1- AS350B, BA, B1, B2, B3, D Title: Left-Hand Litter KitDescription: Installation Configuration must be in accordance with Prior to installation of this modification it 31.<strong>01</strong>.2<strong>01</strong>2<br />
2- AS355E, F, F1, F2, N, NP of Left-Hand Litter Kit P/N 350-200034 or Eurocopter Canada MasterDrawing List No. must be determined thatthe<br />
P/N350-20<strong>01</strong>94 in accordance with Eurocopter MDL-99-0<strong>01</strong>, Issue F, or later approved interrelationship between this modification<br />
Canada Master Drawing List No.MDL-99-0<strong>01</strong>. revisions.Approved configurations are listed in and any other previouslyinstalled<br />
The Left-Hand Litter Kit provides med-evac the attached table.<br />
modification and/ or repair will introduce<br />
capabilities fornon-EMS dedicate<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>04</strong>1637 EUROCOPTER CANADA Ltd. TCCA STC SH12-10 EC130B4 Door handle installation (P/N 120-200<strong>01</strong>4)This<br />
STC is the validation of TCCA STC SH12-10<br />
(issue date -February 10,2<strong>01</strong>2)<br />
10<strong>04</strong>1736 EUROCOPTER CANADA Ltd. TCCA STC SH11-35 EC130B4 Glare Shield Modification P/N 130-885114This<br />
STC is the validation of TCCA STC SH11-35<br />
(issue No. 1 dtdSeptember 20, 2<strong>01</strong>1)<br />
10033870 EUROCOPTER DEUTSCHLAND GmbH P-<strong>EASA</strong>.R.S.<strong>01</strong>568 EC120B Installation on an EC120B helicopter of a<br />
ETSO-certified (ETSO C113)Moving Map<br />
system (MT VisionAir EPIII)<br />
12.10.2005<br />
12.10.2005<br />
12.05.2006<br />
05.07.2007<br />
18.10.2007<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 />
03.10.2<strong>01</strong>2<br />
None The approval holder shall fulfill the<br />
obligations of Part 21,<br />
Paragraph21.A.118A. Prior to installation<br />
of this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or re<br />
11.10.2<strong>01</strong>2<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 />
15.02.2<strong>01</strong>1<br />
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