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>04</strong><strong>04</strong>56 AEROTEC CONCEPT EC225LP SYSTEME ANTI-GIRATOIRESling load S/N 2797 and 2824VFR onlyRequired pre- None <strong>04</strong>.07.2<strong>01</strong>2<br />
stabilization system<br />
modification: Aerotec minor modification<br />
AE11142MAS(Logging EC255 LP) and use of<br />
the dedicated RFM 'SELECTEUR DE<br />
MISSION:UPPER/LOWER (Transport de<br />
charge externe à l’élingue)', <strong>EASA</strong><br />
approval10037964<br />
10<strong>01</strong>7251 AEROTEC SARL <strong>EASA</strong>.R.S.<strong>01</strong>452 REV. 1 SA365N AEROTEC modification IRB (installation radio This STC is limited to SA 365N S/N 6080 This STC is approved only for the product <strong>01</strong>.03.2<strong>01</strong>0<br />
de bord) n° 0928. (Note for internal record: & S/N 6147 and can beinstalled only by configuration as defined inthe approved<br />
This application is to amend an existing AEROTEC technical staff in accordance with: - design data referred to in the paragraphs<br />
<strong>EASA</strong>STC (Ref P-<strong>EASA</strong>.R.S.<strong>01</strong>452) to add AEROTEC STC file Mod n° 0809. for S/N "Description" and"Associated Technical<br />
the S/N 6147)<br />
6080-AEROTEC STC file Mod n° 0928. for Documentation" Prior to installation of this<br />
S/N 6147<br />
modification it must be determined<br />
thatthe inter<br />
10<strong>01</strong>4631 AEROTECHNIC GMBH <strong>EASA</strong>.A.S.02773 DORNIER DO 228-212 Installation of mission equipment for maritime<br />
surveillance.<br />
10<strong>01</strong>6766 AGUSTAWESTLAND PHILADELPHIA <strong>EASA</strong>.IM.R.S.<strong>01</strong>097 TCCA STC SH284NE AGUSTA A-109<br />
AGUSTA A-109 AII<br />
Restricted to S/N 8181, 8183.RUAG changes<br />
<strong>EASA</strong>.A.C.<strong>04</strong>131 and <strong>EASA</strong>.A.C.<strong>04</strong>132 must<br />
be installed concurrently.<br />
Installation of Alternate Static Pressure Source 1. This STC is approved only for the product<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.Configuration A is el<br />
10031050 AGUSTAWESTLAND PHILADELPHIA FAA STC SR02767NY AW119MKII Installation of an Artex ME406P ELT 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.- If th<br />
23.07.2<strong>01</strong>0<br />
10031114 AGUSTAWESTLAND PHILADELPHIA FAA STC SR02777NY AW119MKII Installation of a SX-5 Searchlight and cargo<br />
Hook Heated rearview mirror<br />
10031274 AGUSTAWESTLAND PHILADELPHIA FAA STC SR02265NY A119/AW119MKII Installation of pedal extensions on A119,<br />
AW119MKII helicopters<br />
26.07.2007<br />
<strong>04</strong>.07.2005<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 productIf the h<br />
28.07.2<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- If the<br />
06.08.2<strong>01</strong>0<br />
10031277 AGUSTAWESTLAND PHILADELPHIA FAA STC SR02789NY AW119MKII Installation of a Border Guard Configuration 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 productIf the h<br />
06.08.2<strong>01</strong>0<br />
10031316 AGUSTAWESTLAND PHILADELPHIA FAA STC SR02428NY A119 / AW119MKII <strong>EASA</strong> Validation FAA STC SR02428NY for<br />
A119 / AW119MKII - High VisibilityCrew Doors<br />
10039055 AGUSTAWESTLAND PHILADELPHIA FAA STC SR02444NY A119<br />
AW119 MKII<br />
<strong>EASA</strong> Validation of FAA STC SR02444NY<br />
"Installation of the OffshoreConfiguration in<br />
accordance with Agusta Aerospace Master<br />
Data ListAAC-ENG-06-051 Rev.C"<br />
None The modified crew doors of this STC may<br />
be used to replace either one ofthe<br />
existing doors or both. Prior to installation<br />
of this modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
09.08.2<strong>01</strong>0<br />
None.<br />
previouslyinstalled modif<br />
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 />
03.<strong>04</strong>.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 43/<strong>462</strong>
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