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 />
10038431 EMTEQ ENGINEERING REV. 1 FAA STC ST03345AT B737-300/-400/-500 Validation of FAA STC No. ST03345AT issued None Prior to installation of this modification it 16.02.2<strong>01</strong>2<br />
27 October 2006. Installationof Elementary<br />
must be determined thatthe<br />
Surveillance System / Enhanced Surveillance<br />
interrelationship between this modification<br />
System(ELS/EHS) in the Boeing 737-300/-400/-<br />
and any other previouslyinstalled<br />
500 series aircraft. Installationof EHS capable<br />
modification and/ or repair will introduce<br />
Mode S transponders and ELS capabl<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>04</strong><strong>01</strong>85 EMTEQ ENGINEERING FAA STC ST03846AT ATR 42-200/-300/-320<br />
ATR 42-500<br />
ATR 72-1<strong>01</strong>/-102/-2<strong>01</strong>/-202<br />
ATR 72-211/-212/-212A<br />
Installation of the IMS Flight Deck Ressources<br />
SkyTab 32<strong>01</strong> ElectronicFlight Bag (EFB)<br />
SystemThis STC is installing the SkyTab 32<strong>01</strong><br />
EFB mount arm/device andelectrical supply, as<br />
well as a Satellite Weather Receiver together<br />
withits antenna.<br />
10<strong>01</strong>6117 ENGINE TECHNOLOGIES, INC. <strong>EASA</strong>.IM.A.S.02309 FAA STC SA10588SC CIRRUS SR22 Validation of FAA STC SA10588SC<br />
"Installation of modified Teledyne Continental<br />
Motors IO-550-N engine equipped with<br />
turbonormalizing system"<br />
10<strong>01</strong>6699 ENGINE TECHNOLOGIES, INC. <strong>EASA</strong>.IM.E.S.<strong>01</strong><strong>01</strong>3 SE10589SC TELEDYNE IO-550-G Installation of turbonormalizing system in<br />
accordance with Engine Technologies, Inc.<br />
Master Drawing List Number ETI-G2-1, Rev.<br />
NC, dated November 1, 2006, or later FAA<br />
approved revision.<br />
10029711 ERWIN AERO INTERNATIONAL LTD. REV. 1 TCCA LSTC C-LSA09-321/D DHC-6-300 Avionics to installed in acc. with PAA Design<br />
Group Modification DataSummary: R0910773,<br />
Issue A, approved 31 December 2009 with<br />
TransportCanada approved Flight Manual<br />
Supplements in acc. to TCCA STCC-LSA09-<br />
321/D<br />
10029999 ESG ELEKTRONIKSYSTEM- P-<strong>EASA</strong>.R.S.<strong>01</strong>419 BK 117 C-2 FLIR Mission Work Station PTA-THInstallation<br />
of a FLIR Star Safire HD System and an<br />
Operator Console inaccordance with ESG<br />
GmbH MDL 0005-MDL-006 based on ESG<br />
change no. 0005.<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 />
15.06.2<strong>01</strong>2<br />
Installation of STC SE10589SC<br />
(<strong>EASA</strong>.IM.E.S.<strong>01</strong><strong>01</strong>3) is requiredAn oxygen<br />
system meeting requirements of CS23.1441<br />
through 23.1449 must be installed in<br />
conjunction with this STCThe installer must<br />
determine, if this design is compatible with<br />
previously approve<br />
1. Approval of this change in type design<br />
applies to the above model engine only. This<br />
approval should not be extended to enginesof<br />
this model on which other previously approved<br />
modifications are incorporated unless it is<br />
determined that the interrelatio<br />
11.05.2007<br />
02.<strong>04</strong>.2007<br />
Limited to: S/N 840 only 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 />
19.<strong>04</strong>.2<strong>01</strong>0<br />
-ESG GmbH Minor Change 0003 and STC<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>489 have to beinstalled as<br />
prerequisite for the installation of this<br />
modification.-This approval does not include<br />
the operation of laser pointer or laserilluminator<br />
devices.<br />
Prior to installation of this modification it 10.05.2<strong>01</strong>0<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 />
10030259 ESG ELEKTRONIKSYSTEM- MBB-BK 117 B-2 Star SAFIRE and Mission Console<br />
This approval does not include the operation of Prior to installation of this modification it 07.06.2<strong>01</strong>0<br />
BK117Installation of FLIR Star Safire HD laser pointer or laserilluminator devices. must be determined thatthe<br />
System on a bolster step on the RHside,<br />
interrelationship between this modification<br />
mission console, equipment rack, operator and<br />
and any other previouslyinstalled<br />
observer seats onadapter plates in the cabin, in<br />
modification and/ or repair will introduce<br />
accordance with ESG GmbH MDL0<strong>01</strong>2-MDL-<br />
no adverse effectupon the airworthiness<br />
006 based o<br />
of the product.<br />
10<strong>04</strong>2409 ESG ELEKTRONIKSYSTEM- <strong>EASA</strong>.R.S.<strong>01</strong>577 EC135 P1, EC135 P2,<br />
EC135 P2+, EC135 T1,<br />
EC135 T2, EC135 T2+.<br />
Trakka A800 Searchlight InstallationGimbal<br />
installation of a 800W searchlight and related<br />
electrical andmechanical provisions.<br />
10<strong>01</strong>6724 EUROCOPTER CANADA Ltd. <strong>EASA</strong>.IM.R.S.<strong>01</strong>022 REV. 1 TCCA STC SH96-39 AS 350 BA/B2/B3 Two place forward passenger seat (RH) 1. Refer to Flight manual supplement<br />
attached to STC SH96-39 issue 5 approved 12<br />
April 1996 or later approved revision.2. This<br />
STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Des<br />
- Activation and/or use of IR-Filter is not Prior to installation of this modification it 29.11.2<strong>01</strong>2<br />
approved- Activation and/or use of Laser is not must be determined thatthe<br />
approved<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 />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 209/<strong>462</strong><br />
19.12.2005
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