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 />
10038915 MECAER AVIATION GROUP S.P.A. MBB-BK117 C-2 EC145 VIP MB Interiors Drawing No. None Prior to installation of this modification it 23.03.2<strong>01</strong>2<br />
6EC10000X0<strong>01</strong>-0<strong>01</strong><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 />
10039438 MECAER AVIATION GROUP S.P.A. REV. 1 AW109SP Installation of Cabinet Five Star P/N<br />
6A10AD002-0<strong>01</strong> in AW109SP.Modification in<br />
accordance with MECAER Notice of Design<br />
Change NDC6A10AD-003 issue A dated<br />
24/<strong>04</strong>/2<strong>01</strong>2.<br />
This STC approval does not include the<br />
installation of the in-flightentertainment<br />
equipment inside the Cabinet Five Star.<br />
10<strong>04</strong>2023 MECAER AVIATION GROUP S.P.A. AW139 Ballast Installation P/N 6AB1AD<strong>01</strong>8-0<strong>01</strong> This STC is only installable on AW139<br />
Helicopters equipped withAgustaWestland<br />
Active Vibration Control System P/N<br />
4G1830F0<strong>01</strong>11 or4G1830F00211.<br />
10<strong>01</strong>5810 MEGGITT (ADDISON), Inc. <strong>EASA</strong>.IM.A.S.<strong>01</strong>879 FAA STC NO ST09494SC CESSNA 182S<br />
CESSNA 182T<br />
CESSNA T182T<br />
10<strong>01</strong>6754 METRO AVIATION, Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>083 FAA STC SH3880SW EUROCOPTER DEUTSCHLAND<br />
MBB-BK<br />
Installation of an R134a vapour cycle airconditioning<br />
system<br />
Installation of a Vapor Cycle Air Conditioner in<br />
accordance with FA STC SH3880SW<br />
10<strong>01</strong>6780 METRO AVIATION, Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>120 FAA STC SR<strong>01</strong>606NY-D EUROCOPTER DEUTSCHLAND Installation of Spectrolab SX-5 Starbust<br />
MBB-BK<br />
searchlight according to FAA STC SR<strong>01</strong>606NY-<br />
D<br />
10<strong>01</strong>6823 METRO AVIATION, Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>188 REV. 1 FAA STC SR09163RC EUROCOPTER EC 135 Installation of mechanically driven vapor cycle Prior to installation of this modification the<br />
air condition system i.a.w. FAA STC<br />
installer must determine that the<br />
SR09163RC as amended by 18-06-<br />
interrelationship between this modification and<br />
2007.Major change to <strong>EASA</strong> STC<br />
any other previously installed modification will<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>188, addition of models and introduce no adverse effect upon the<br />
incorporation of technical modifications. airworthiness of the product. The install<br />
10<strong>01</strong>6976 METRO AVIATION, Inc. <strong>EASA</strong>.IM.R.S.<strong>01</strong>377 FAA STC SR09230RC EUROCOPTER DEUTSCHLAND<br />
EC-135<br />
10035563 MICHELIN NORTH AMERICA, INC. FAA STC ST03642AT CL-600-2C10, CL-600-2D15<br />
CL-600-2D24<br />
10<strong>01</strong>5379 MICRO AERODYNAMICS, INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>058 FAA STC SA00763SE PIPER PA-30<br />
PIPER PA-39<br />
Prior to installation of this modification it 16.05.2<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 />
Prior to installation of this modification it 05.11.2<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 />
This STC is approved only for the product<br />
10.<strong>04</strong>.2006<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 />
1. This STC is approved only for the product<br />
31.05.2005<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 />
None 13.09.2006<br />
Installation of landing gear skid extensions 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 />
Installation of Michelin's tire(s) P/N 029-9<strong>01</strong>-0<br />
on the main gear and/orP/N 036-897-0 on the<br />
nose landing gear of Bombardier CL-600-<br />
2C10,CL-600-2D15, CL-600-2D24 aircraft<br />
wheel assembly.<br />
Installation of Vortex Generators on the Wing 1. This STC is approved only for the product<br />
leading edge, and vertical fin surfaces.Drawing configuration as defined in the approved design<br />
Package MA2122 Rev. IR dated 25 October data referred to in the paragraph "Description".<br />
1999, or later approved revision.AFM Compatibility with other aircraft/engine<br />
Supplement for PA-30 & PA-39 dated 13 July configurations shall be determined by the<br />
2005.Installation Manual MA2123 Rev. IR da installer.<br />
14.<strong>04</strong>.2008<br />
26.11.2007<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 />
30.06.2<strong>01</strong>1<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 332/<strong>462</strong><br />
08.08.2005
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