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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 />

<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 210/<strong>462</strong>

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