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>7144 HELIKOPTER AIR TRANSPORT GmbH <strong>EASA</strong>.R.S.<strong>01</strong>247 EC 135 Installation of Laser Scannig Equipment Limited to SN 025, 050, 053, 072, 097, 127,<br />
128, 160, 168, 181, 182, 187, 196, 199, 205,<br />
210, 220, 221, 305, 308, 325, 359, 368<br />
and387.<br />
<strong>01</strong>.06.2006<br />
10027677 HELIKOPTER AIR TRANSPORT GMBH P-<strong>EASA</strong>.R.S.<strong>01</strong>499 EC 135 T1 (CDS)<br />
Engineering Order EO 85-002, dated 21 Installation does not constitute operational Prior to installation of this modification the 20.10.2009<br />
EC 135 T2 (CPDS)<br />
September 2009 "Replacement ofSiren Hooks approval.Approval of PCDS (Personal Carrying installer must determinethat the<br />
EC 135 T2+<br />
with Onboard Talon Systems".<br />
Device System) for external loadoperation interrelationship between this modification<br />
must be granted by the competent authority. and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
product.<br />
10033490 HELIKOPTER AIR TRANSPORT GmbH EC 135 T1(CDS)<br />
Replacement of Onboard Talon System with Installation does not constitute operational Prior to installation of this modification it 25.<strong>01</strong>.2<strong>01</strong>1<br />
EC 135 T2(CPDS), EC 135 T2+ improved IAOSI hook AS 21-17<br />
approval. Approval of PCDS(Personal Carrying must be determined thatthe<br />
Device System) for external load operation interrelationship between this modification<br />
must begranted by the competent authority. and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10034657 HELIKOPTER AIR TRANSPORT GmbH EC135 T2 Dual GNS430W Installation in Autopilot<br />
helicopter<br />
10<strong>01</strong>6751 HELI-LYNX <strong>EASA</strong>.IM.R.S.<strong>01</strong>078 TCCA STC SH05-8, ISSUE 1 EUROCOPTER FRANCE AS<br />
355E<br />
EUROCOPTER FRANCE AS<br />
355F<br />
EUROCOPTER FRANCE AS<br />
355F1<br />
EUROCOPTER FRANCE AS<br />
355F2<br />
10<strong>01</strong>6752 HELI-LYNX <strong>EASA</strong>.IM.R.S.<strong>01</strong>079 SH<strong>04</strong>-27 EUROCOPTER FRANCE AS<br />
355F1<br />
EUROCOPTER FRANCE AS<br />
355F2<br />
10<strong>01</strong>6818 HELI-LYNX <strong>EASA</strong>.IM.R.S.<strong>01</strong>183 SH05-41 EUROCOPTER FRANCE AS<br />
355E<br />
EUROCOPTER FRANCE AS<br />
355F<br />
EUROCOPTER FRANCE AS<br />
355F1<br />
EUROCOPTER FRANCE AS<br />
355F2<br />
10<strong>01</strong>6819 HELI-LYNX <strong>EASA</strong>.IM.R.S.<strong>01</strong>184 SH05-40 EUROCOPTER FRANCE AS<br />
355E<br />
EUROCOPTER FRANCE AS<br />
355F<br />
EUROCOPTER FRANCE AS<br />
355F1<br />
EUROCOPTER FRANCE AS<br />
355F2<br />
Installation of Anticipator of Govenor<br />
CablesAss.Refer to installation manual IM, PA<br />
<strong>04</strong> <strong>01</strong>5 91 <strong>01</strong> issue 1 or later approved<br />
Heli-Lynx AS 355 FX System modifications, as<br />
per Transport Canada STC n° SH<strong>04</strong>-27<br />
Installation of One or Two Concorde RG 355<br />
Laed-Acid Batteries accorging to TCCA STC<br />
SH05-41 issue N°2 approved September 09,<br />
2005<br />
Installation of Purolator De-icing Fuel Filter p/n<br />
1743640-<strong>01</strong><br />
The installation is limited to Aircraft Serial<br />
Numbers 0220 and 0221<br />
1. Refer to instructions for continued<br />
airworthiness ICA PA <strong>04</strong> <strong>01</strong>5 05 <strong>01</strong> issue 1 or<br />
later approved and associated maintenance<br />
instructions.2. This STC is approved only for<br />
the product configuration as defined in the<br />
approved design data referred to i<br />
Refer to STC SH05-41 and Flight Manual<br />
Supplement<br />
This STC is the <strong>EASA</strong> validation of Transport<br />
Canada STC n0 SH05-40, issue 1, dated<br />
September 9*, 2005,<br />
The approval holder shall fulfill the<br />
obligations of Part 21,Paragraph<br />
21.A109.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 270/<strong>462</strong><br />
18.<strong>04</strong>.2<strong>01</strong>1<br />
10.10.2005<br />
<strong>04</strong>.<strong>04</strong>.2007<br />
16.03.2006<br />
25.<strong>04</strong>.2008
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