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>7052 DART AEROSPACE USA, Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>477 FAA STC SR00914SE EUROCOPTER FRANCE SA Installation of DART Bearpaws P/N D315-670- 1. Prior to installation of this modification the<br />
06.02.2009<br />
315B<br />
<strong>01</strong>1 - Validation of FAA STC SR00914SE. 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.2.<br />
10<strong>01</strong>7053 DART AEROSPACE USA, Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>478 FAA STC SR00848SE EUROCOPTER FRANCE SA Installation of Dart Aerospace Skidtube P/N 1. Prior to installation of this modification the<br />
06.02.2009<br />
315B<br />
D315-668-<strong>01</strong>1 (LH) and -<strong>01</strong>2 (RH). Validation installer must determine that the<br />
of FAA STC SR00848SE.<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.2.<br />
10<strong>01</strong>7063 DART AEROSPACE USA, Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>499 FAA STC SR<strong>01</strong>853SE EUROCOPTER DEUTSCHLAND 117-762 Skitube Installation in accordance with Prior to installation of this modification the<br />
10.11.2008<br />
MBB-BK<br />
FAA STC SR<strong>01</strong>853SE.<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 />
10<strong>01</strong>7084 DART AEROSPACE USA, Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>551 FAA STC SR<strong>01</strong><strong>04</strong>3SE AGUSTA A119 Cargo Mirror Installation.Note: This STC<br />
supersedes ENAC STC N-CS-<strong>01</strong>4 being the<br />
validation of FAA STC SR<strong>01</strong><strong>04</strong>3SE dated 25<br />
January 2002.<br />
10029107 DART AEROSPACE USA, Inc. N-CS-022 FAA STC SR00949SE A119, AW119MKII FAA STC SR00949SE dated 21 August 2008<br />
"Bearpaw Installation"<br />
10033942 DART AEROSPACE USA, Inc. CAA UK 28081 AND<br />
28082<br />
FAA STC SR00646SE 1. AS350 B, AS350 B1, AS350 B2 D350-636 Skidtube Installations Note: This<br />
1. AS350 B3, AS350 BA, AS350 D STC supersedes CAA Approval Notes 28081<br />
2. AS355 E, AS355 F, AS355 F1 and 28082 and addsmodels AS355N and NP<br />
2. AS355 F2, AS355 N, AS355 NP to applicability.<br />
10038103 DART AEROSPACE USA, Inc. REV. 1 FAA STC SR<strong>01</strong><strong>04</strong>2SE EC135 P1(CDS)<br />
EC135 P1(CPDS)<br />
EC135 P2(CPDS), EC135 P2+<br />
EC135 T1(CDS), EC135<br />
T1(CPDS)<br />
EC135 T2(CPDS), EC135 T2+<br />
Dart D135-692-<strong>01</strong>1 Bearpaws in accordance<br />
with Dart Aerospace DrawingList No. MDL-<br />
D135-692, and installation of this system.This<br />
<strong>EASA</strong> STC is based on validation of FAA STC<br />
SR<strong>01</strong><strong>04</strong>2SE iaw the PTVP.<br />
10038656 DART AEROSPACE USA, Inc. REV. 1 FAA STC SR02138SE AW139 <strong>EASA</strong> Validation of FAA STC SR02138SE<br />
"Installation of Dart D139-799Maintenance<br />
Kits".<br />
1. 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.2.<br />
11.05.2009<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 />
05.03.2<strong>01</strong>0<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 />
21.02.2<strong>01</strong>1<br />
Approval of this change in type design applies<br />
only to Eurocopter EC135rotorcraft, which are<br />
equipped with standard skidtubes, high<br />
gearskidtubes, or float skidtubes as defined in<br />
the installationinstructions.<br />
Prior to installation of this modification it 27.<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 />
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 />
19.03.2<strong>01</strong>2<br />
10<strong>04</strong>0294 DART AEROSPACE USA, Inc. REV. 1 FAA STC SR02024SE A119, AW119MKII Validation of FAA STC SR02024SE: D119-646 None Prior to installation of this modification it 06.07.2<strong>01</strong>2<br />
Replacement Sikdtube Ins.<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 />
10<strong>04</strong>1447 DASSAULT AIRCRAFT SERVICES (DAS) FAA STC ST02964NY-D MF50 Installation of Crane Eldec "SmartStem" Tire<br />
Pressure Sensor (TPS)System.Validation of<br />
FAA STC N° ST02964NY-D.<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 />
18.09.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 168/<strong>462</strong>
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