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 />
10029936 ECT INDUSTRIES REV. 1 AS350B, AS350B1, AS350B2 Installation of DTSV2 Data Transmission Modification not approved for aircraft equipped The approval holder shall fulfil the 30.07.2<strong>01</strong>2<br />
AS350BA, AS350BB, AS350B3 System.Revision 1 introduces corrections of with weather radar orAFCS (Automatic Flight obligations of Part 21,<br />
the tracking system installation.<br />
Control System).Modification not approved for Paragraph21.A118A. Prior to installation<br />
AS350B3 model helicopters withmodification of this modification it must be determined<br />
OP-4305 (Arriel 2D engine installation) thatthe interrelationship between this<br />
incorporated.<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repa<br />
1003<strong>01</strong>43 ECT INDUSTRIES AS355E, AS355F, AS355F1,<br />
AS355F2, AS355N, AS355NP<br />
Installation of DTSV2 Tracking System None None 27.05.2<strong>01</strong>0<br />
10030338 ECT INDUSTRIES P-<strong>EASA</strong>.R.S.<strong>01</strong>510 AS350B, AS350B1, AS350B2, Installation of a tracking system (DTS - Data Modification not approved for aircraft equipped Prior to installation of this modification it 11.06.2<strong>01</strong>0<br />
AS350BA, AS350BB, AS350B3 Transmission System)<br />
with weather radar orAFCS (Automatic Flight must be determined thatthe<br />
Control System)<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 />
10033164 ECT INDUSTRIES P-<strong>EASA</strong>.R.S.<strong>01</strong>505 REV. 3 EC135 P1(CPDS)<br />
EC135 P2(CPDS), EC135 P2+<br />
EC135 T1(CPDS)<br />
EC135 T2(CPDS), EC135 T2+<br />
EC135 NVIS Lighting SystemInstallation of a<br />
Night Vision Imaging Lighting system, to<br />
enableoperation with Night Vision Goggles.-<br />
Avionic type 1- P/N: 60D-1000-000, into<br />
helicopters with CPDS andconventional<br />
flight/navigation instruments-Avionic type 2-<br />
P/N:<br />
None The first installation of this kit must be<br />
supervised by the STC holder.This<br />
rotorcraft employs Night Vision Imaging<br />
System lighting, commonlynamed NVIS<br />
lighting, that has been certified to ensure<br />
the aircraft iscompatible with night vision<br />
goggles (NVG).<br />
10037841 ECT INDUSTRIES EC135 P1, EC135 P2, EC135 P2+ Installation of Brite Saver Usage Monitoring Only for EC135/EC635 variants with CPDS-<br />
EC135 T1, EC135 T2, EC135 T2+ SystemInstallation of a Brite Saver Usage Cockpit<br />
EC635 P2+<br />
Monitoring System. This modificationis defined<br />
EC635 T1(CPDS), EC635 T2+ in CONFAD-<strong>01</strong>15-92-EN.<br />
10<strong>04</strong>2<strong>01</strong>2 ECT INDUSTRIES AS 350 B,AS 350 B1,AS 350 B2<br />
AS 350 B3,AS 350 BA,AS 350 BB<br />
Installation of Data Tracking System DTS-<br />
Alpha.Modification as defined in STC Data List,<br />
doc. SDL-DTSALPHA-AS350 Rev.<strong>04</strong><br />
10032345 EICHELSDOERFER GmbH RF5 STC "Installation engine Rotax 912 and<br />
propeller HO-V352F-S1/S170FQ inthe<br />
powered sailplane Fournier RF 5"<br />
10<strong>04</strong>0934 EIRTECH AVIATION SERVICES LIMITED REV. 1 737-600,-700,-800,-900,-900ER Cabin Altitude and Take-off Configuration<br />
warnings and indications -Activation.<br />
27.<strong>01</strong>.2<strong>01</strong>2<br />
Prior to installation of this modification it 03.<strong>01</strong>.2<strong>01</strong>2<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 />
Modification not approved for rotorcraft Prior to installation of this modification it 31.10.2<strong>01</strong>2<br />
equipped with AFCS (AutomaticFlight Control must be determined thatthe<br />
System) or Weather Radar.Modification not interrelationship between this modification<br />
approved for AS350B3 model helicopters and any other previouslyinstalled<br />
withmodification OP-4305 (Arriel 2D engine modification and/ or repair will introduce<br />
installation) incorporated.<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
Limited to Fournier RF 5, S/N 5<strong>01</strong>2 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 />
28.10.2<strong>01</strong>0<br />
This change is not applicable to an aircraft with<br />
High Altitude LandingCapability.<br />
10<strong>01</strong>6491 EJM AEROSPACE SERVICES <strong>EASA</strong>.IM.A.S.02853 FAA STC ST02534AT BOEING 747-400 Installation of a Matsushita Avionics Systems This STC is approved only for the product<br />
Corporation System 3000 In-Flight<br />
configuration as defined in the approved design<br />
Entertainement System on a Singapore Airlines data. Compatibilty with other aircraft/engine<br />
Boeing 747-400 in accordance with Master configurations shall be determined by the<br />
Drawing List MDL 10321, Rev. H. dated<br />
29/<strong>04</strong>/2003, or later FAA approved revision.<br />
installer.<br />
10028392 EJM AEROSPACE SERVICES FAA STC ST02531AT B747-400 Installation of a Matsushita Avionics Systems<br />
Corporation System 3000In-Flight<br />
Entertainment system on a Singapore Airlines<br />
Boeing 747-400type aircraft in accordance with<br />
Master Drawing List MDL10270, Rev. G,dated<br />
06 June 2003 or later FAA approved revisio<br />
Prior to installation of this modification it 26.10.2<strong>01</strong>2<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 />
18.08.2008<br />
Not Applicable Airplane Flight Manual Supplement, Doc. <strong>04</strong>.<strong>01</strong>.2<strong>01</strong>0<br />
Nr. 14526003 dated June 4, 2002or later<br />
approved revision is required as part of<br />
this STC<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 199/<strong>462</strong>
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