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>0937 F&M ENTERPRISES INC. FAA STC SE7559SW 1. C-75 SERIES, C-85 SERIES Install adapter to permit use of a spin-on oil Engines modified in accordance with this STC In order to install this modified engine in 06.08.2<strong>01</strong>2<br />
2. C090 SERIES, O-200 SERIES filter in accordance withF. & M. Enterprises' will not differ inperformance or operating an aeroplane, or to installthe modification<br />
Installation Instructions for Model TAF-Long limitations for unmodified engines.Only the on an engine in an aeroplane it will be<br />
OilFilter, dated October 26, 1998, or later FAA following filters are eligible for this<br />
necessary toapply for approval of a minor<br />
approved revision.<strong>EASA</strong> Validation of FAA installation:Champion No. CH48108A.C No. modification to the aeroplane.<br />
STC SE7559SW<br />
OF-53A<br />
Theinstaller must determine whether this<br />
design change<br />
10<strong>04</strong>0938 F&M ENTERPRISES INC. FAA STC SE09356SC 1. O-470 SERIES<br />
Install F. & M. Enterprises' Model C6LC, C6LC- None In order to install this modified engine in 06.08.2<strong>01</strong>2<br />
2. IO-470 SERIES<br />
S, or C6LC-L oil filteradapter for a spin-on oil<br />
an aeroplane, or to installthe modification<br />
3. IO-520 SERIES<br />
filter in accordance with F. & M.<br />
on an engine in an aeroplane it will be<br />
Enterprises'Installation Instructions dated<br />
necessary toapply for approval of a minor<br />
October 26, 1998, or later FAA<br />
modification to the aeroplane.<br />
approvedrevision.<strong>EASA</strong> Validation of FAA STC<br />
Theinstaller must determine whether this<br />
SE09356S<br />
design change<br />
10<strong>04</strong>0939 F&M ENTERPRISES INC. FAA STC SE08409SW 1. C-125 SERIES<br />
Installation of F. & M. Enterprises Model CO- Engines modified in accordance with this STC In order to install this modified engine in 06.08.2<strong>01</strong>2<br />
2. C-145 SERIES, O-300 SERIES 300 or C6SC spin-on oilfilter adapter, in will not differ inperformance or operating an aeroplane, or to installthe modification<br />
3. GO-300 SERIES<br />
accordance with F. & M. Enterprises<br />
limitations for unmodified engines.<br />
on an engine in an aeroplane it will be<br />
4. IO-360 SERIES<br />
installationinstructions for Model CO-300 dated<br />
necessary toapply for approval of a minor<br />
5. TSIO-360 SERIES<br />
October 26, 1998, or ModelC6SC dated<br />
modification to the aeroplane.<br />
October 5, 2005, or later FAA approved rev<br />
Theinstaller must determine whether this<br />
design change<br />
10<strong>01</strong>5468 F. ATLEE DODGE AIRCRAFT SERVICES <strong>EASA</strong>.IM.A.S.<strong>01</strong>221 FAA STC SA02115AK PIPER PA-12<br />
Fabrication and installation of F.Atlee Dodge 1. Any Piper aircraft incorporating this change<br />
09.06.2005<br />
PIPER PA-12S<br />
30.5 gallon wing fuel tank sight gages must be equipped with F. Atlee Dodge 30.5<br />
PIPER PA-14<br />
gallon wing fuel tanks in accordance withFAA<br />
PIPER PA-18-150<br />
STC SA649AL, SA00092SE, or<br />
PIPER PA-18A-150<br />
SA5781NM.2.This STC is approved only for<br />
PIPER PA-18AS-150<br />
the product configuration as defined in the<br />
PIPER PA-18S-150<br />
approved<br />
10<strong>01</strong>6731 FARGO MANUFACTURING <strong>EASA</strong>.IM.R.S.<strong>01</strong>055 FAA STC SR<strong>01</strong>926CH MD HELICOPTERS MD900 Install 61.8 gallon crashworthy auxiliary fuel This STC is approved only for the product<br />
30.03.2005<br />
tank on the aft cabin baggage bay floor 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 />
10<strong>01</strong>7067 FARGO MANUFACTURING <strong>EASA</strong>.IM.R.S.<strong>01</strong>503 FAA STC SR<strong>01</strong>813CH MD HELICOPTERS MD900 Installation of Auxiliary Fuel System Kit in This STC is limited to the installation of Fargo<br />
15.12.2008<br />
accordance with FAA STC SR<strong>01</strong>813CH Manufacturing Co. 52.5-gallon, crashworthy<br />
auxiliary fuel tank pursuant to FAA<br />
STCSR<strong>01</strong>238CH as referred in FAA STC<br />
SR<strong>01</strong>813CH. The 55-gallon installation and the<br />
28-gallon installation are not included in thi<br />
10<strong>01</strong>5060 FEDERATION FRANCAISE DE VOL A<br />
VOILE<br />
10030091 FEDERATION FRANCAISE DE VOL A<br />
VOILE<br />
10032277 FIBERGLAS-TECHNIK RUDOLF<br />
LINDNER<br />
<strong>EASA</strong>.A.S.03383 Winglet Retrofitting. 2.2 Supplemental Flight Manual <strong>01</strong>.02.2008<br />
ASW20F STC M-<strong>01</strong>/09-A<strong>01</strong> Winglet Installation on<br />
ASW20F<br />
None None 20.05.2<strong>01</strong>0<br />
GROB G 103 "TWIN II" STC "Reparatur Twin ll" Even if parts from a "Twin ll "Acro" are used, - Further conditions according to the 22.10.2<strong>01</strong>0<br />
the combined sailplanewill be always a "Twin ll" conditions of the STC "ReparaturTwin ll"-<br />
(without Acro). / Auch wenn Teile eines Twinll Weitere Festlegungen entsprechend den<br />
"Acro" verwendet werden, das neu<br />
Bedingungen des STC "ReparaturTwin<br />
entstandene Segelflugzeug ist immerein "Twin ll"Prior to installation of this modification it<br />
ll" (ohne Acro).<br />
must be determined thatthe<br />
interrelationship between t<br />
10<strong>01</strong>5983 FIELD AVIATION COMPANY INC. <strong>EASA</strong>.IM.A.S.02135 SA93-81 BOMBARDIER DHC-6<br />
BOMBARDIER DHC-6 SERIES<br />
200<br />
BOMBARDIER DHC-6 SERIES<br />
300<br />
Roof Access Steps Installation -- 13.11.2006<br />
10<strong>01</strong>6003 FIELD AVIATION COMPANY Inc. <strong>EASA</strong>.IM.A.S.02164 O-LSA06-179/D ISSUE 1 (TCCA LI BEECH B200 SUPER KING AIR Installation of a single Universal UNS-1F Flight Aircraft Serial BB-1547 onlyThe UNS-1F Flight<br />
05.02.2007<br />
Management System complete with dual Management System is approved for En-route,<br />
Universal GLS-1250 DGPS Receivers (SCAT- Terminal and Non Precision Approach<br />
1).Transport Canada LSTC O-LSA06-179/D<br />
Issue 2.<br />
Operations only.<br />
10<strong>01</strong>6129 FIELD AVIATION COMPANY Inc. <strong>EASA</strong>.IM.A.S.02323 REV. 1 TCCA STC SA07-80 BOMBARDIER DHC-8-311 Retrofit of Swedish Coastguard Maritime Patrol Limitations UNS-1F Flight Management<br />
<strong>01</strong>.07.2008<br />
Modification.TCCA STC Number: SA07-80, Systems approved for En-route, Terminal and<br />
Issue 2 dated 26 February 2008<br />
Non Precision approach operations<br />
oniy.External Mission LAN System not<br />
approved for airborne operations.External<br />
Nokia Cellular Telephone System not approved<br />
for airborne use.<br />
10<strong>01</strong>6225 FIELD AVIATION COMPANY INC. <strong>EASA</strong>.IM.A.S.02476 TCCA C-LSA07-021/D BOMBARDIER CL-600-2B19 Installation of Corporate Shuttle Interior. Limited to serial no. 8<strong>04</strong>9 09.10.2007<br />
10<strong>01</strong>6299 FIELD AVIATION COMPANY INC. <strong>EASA</strong>.IM.A.S.02596 TCCA STC C-LSA07-322/D BOMBARDIER CL-600-2B19 Installation of Life Rafts. Aircraft Serial No. 8<strong>04</strong>9 only 12.10.2007<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 214/<strong>462</strong>
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