04/01/2013 Page 1/462 - EASA

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EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10040937 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 06.08.2012 2. C090 SERIES, O-200 SERIES filter in accordance withF. & M. Enterprises' will not differ inperformance or operating an aeroplane, or to installthe modification Installation Instructions for Model TAF-Long limitations for unmodified engines.Only the on an engine in an aeroplane it will be OilFilter, dated October 26, 1998, or later FAA following filters are eligible for this necessary toapply for approval of a minor approved revision.EASA Validation of FAA installation:Champion No. CH48108A.C No. modification to the aeroplane. STC SE7559SW OF-53A Theinstaller must determine whether this design change 10040938 F&M ENTERPRISES INC. FAA STC SE09356SC 1. O-470 SERIES Install F. & M. Enterprises' Model C6LC, C6LC- None In order to install this modified engine in 06.08.2012 2. IO-470 SERIES S, or C6LC-L oil filteradapter for a spin-on oil an aeroplane, or to installthe modification 3. IO-520 SERIES filter in accordance with F. & M. on an engine in an aeroplane it will be Enterprises'Installation Instructions dated necessary toapply for approval of a minor October 26, 1998, or later FAA modification to the aeroplane. approvedrevision.EASA Validation of FAA STC Theinstaller must determine whether this SE09356S design change 10040939 F&M ENTERPRISES INC. FAA STC SE08409SW 1. C-125 SERIES Installation of F. & M. Enterprises Model CO- Engines modified in accordance with this STC In order to install this modified engine in 06.08.2012 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 3. GO-300 SERIES accordance with F. & M. Enterprises limitations for unmodified engines. on an engine in an aeroplane it will be 4. IO-360 SERIES installationinstructions for Model CO-300 dated necessary toapply for approval of a minor 5. TSIO-360 SERIES October 26, 1998, or ModelC6SC dated modification to the aeroplane. October 5, 2005, or later FAA approved rev Theinstaller must determine whether this design change 10015468 F. ATLEE DODGE AIRCRAFT SERVICES EASA.IM.A.S.01221 FAA STC SA02115AK PIPER PA-12 Fabrication and installation of F.Atlee Dodge 1. Any Piper aircraft incorporating this change 09.06.2005 PIPER PA-12S 30.5 gallon wing fuel tank sight gages must be equipped with F. Atlee Dodge 30.5 PIPER PA-14 gallon wing fuel tanks in accordance withFAA PIPER PA-18-150 STC SA649AL, SA00092SE, or PIPER PA-18A-150 SA5781NM.2.This STC is approved only for PIPER PA-18AS-150 the product configuration as defined in the PIPER PA-18S-150 approved 10016731 FARGO MANUFACTURING EASA.IM.R.S.01055 FAA STC SR01926CH MD HELICOPTERS MD900 Install 61.8 gallon crashworthy auxiliary fuel This STC is approved only for the product 30.03.2005 tank on the aft cabin baggage bay floor configuration as defined in the approved design data referred to in the paragraph "Description". Compatibility with other aircraft/engine configurations shall be determined by the installer. 10017067 FARGO MANUFACTURING EASA.IM.R.S.01503 FAA STC SR01813CH MD HELICOPTERS MD900 Installation of Auxiliary Fuel System Kit in This STC is limited to the installation of Fargo 15.12.2008 accordance with FAA STC SR01813CH Manufacturing Co. 52.5-gallon, crashworthy auxiliary fuel tank pursuant to FAA STCSR01238CH as referred in FAA STC SR01813CH. The 55-gallon installation and the 28-gallon installation are not included in thi 10015060 FEDERATION FRANCAISE DE VOL A VOILE 10030091 FEDERATION FRANCAISE DE VOL A VOILE 10032277 FIBERGLAS-TECHNIK RUDOLF LINDNER EASA.A.S.03383 Winglet Retrofitting. 2.2 Supplemental Flight Manual 01.02.2008 ASW20F STC M-01/09-A01 Winglet Installation on ASW20F None None 20.05.2010 GROB G 103 "TWIN II" STC "Reparatur Twin ll" Even if parts from a "Twin ll "Acro" are used, - Further conditions according to the 22.10.2010 the combined sailplanewill be always a "Twin ll" conditions of the STC "ReparaturTwin ll"- (without Acro). / Auch wenn Teile eines Twinll Weitere Festlegungen entsprechend den "Acro" verwendet werden, das neu Bedingungen des STC "ReparaturTwin entstandene Segelflugzeug ist immerein "Twin ll"Prior to installation of this modification it ll" (ohne Acro). must be determined thatthe interrelationship between t 10015983 FIELD AVIATION COMPANY INC. EASA.IM.A.S.02135 SA93-81 BOMBARDIER DHC-6 BOMBARDIER DHC-6 SERIES 200 BOMBARDIER DHC-6 SERIES 300 Roof Access Steps Installation -- 13.11.2006 10016003 FIELD AVIATION COMPANY Inc. EASA.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 05.02.2007 Management System complete with dual Management System is approved for En-route, Universal GLS-1250 DGPS Receivers (SCAT- Terminal and Non Precision Approach 1).Transport Canada LSTC O-LSA06-179/D Issue 2. Operations only. 10016129 FIELD AVIATION COMPANY Inc. EASA.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 01.07.2008 Modification.TCCA STC Number: SA07-80, Systems approved for En-route, Terminal and Issue 2 dated 26 February 2008 Non Precision approach operations oniy.External Mission LAN System not approved for airborne operations.External Nokia Cellular Telephone System not approved for airborne use. 10016225 FIELD AVIATION COMPANY INC. EASA.IM.A.S.02476 TCCA C-LSA07-021/D BOMBARDIER CL-600-2B19 Installation of Corporate Shuttle Interior. Limited to serial no. 8049 09.10.2007 10016299 FIELD AVIATION COMPANY INC. EASA.IM.A.S.02596 TCCA STC C-LSA07-322/D BOMBARDIER CL-600-2B19 Installation of Life Rafts. Aircraft Serial No. 8049 only 12.10.2007 04/01/2013 Page 214/462
EASA STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue 10016417 FIELD AVIATION COMPANY INC. EASA.IM.A.S.02750 TCCA STC SA05-73 BOMBARDIER DHC-8-311 Intallation of a Artex C406-2 or C406-N Three Frequency Emergency Locator Transmitter (ELT). 11.06.2008 10016418 FIELD AVIATION COMPANY INC. EASA.IM.A.S.02751 TCCA STC SA00-2 BOMBARDIER DHC-8-200 Ultra Electronics ANVC-Active Noise and Prior to installation of this modification the 25.08.2008 SERIES Vibration Control System and PBMS – installer must determine that the BOMBARDIER DHC-8-300 Propeller Balancing and Monitoring SystemRef. interrelationship between this modification and SERIES TCCA STC SA00-2, Issue 4, dated 24 October any other previously installed modification BOMBARDIER DHC-8-311 2004 will introduce no adverse effect upon the BOMBARDIER DHC-8-315 airworthiness of the product. 10016419 FIELD AVIATION COMPANY INC. EASA.IM.A.S.02752 TCCA LSTC C-LSA06-101/D BOMBARDIER DHC-8-311 Installation of a 320cuft baggage compartment and installation of PBE's and O2 bottle into the cabin (Ref. TCCA LSTC C-LSA06-010/D) 06.10.2008 10016430 FIELD AVIATION COMPANY Inc. EASA.IM.A.S.02769 REV. 1 TCCA STC C-LSA08-056/D DHC-8-202, DHC-8-311 Honeywell AHRS to SFIM APIRS Conversion Provisions TCCA STC C-LSA08-056/D, Issue 2 10016432 FIELD AVIATION COMPANY INC. EASA.IM.A.S.02772 TCCA STC O-LSA08-023/D BOMBARDIER DHC-8-311 VHF Comm Replacement for 8.33 kHz Spacing, ref. TCCA LST C-LSA08-023/D. 10016603 FIELD AVIATION COMPANY INC. EASA.IM.A.S.03017 TCCA STC SA01-55 BOMBARDIER DHC-8-400 SERIES BOMBARDIER DHC-8-401 BOMBARDIER DHC-8-402 Installation of Variable Position Cabin Class Divider. 10016648 FIELD AVIATION COMPANY INC. EASA.IM.A.S.03092 REV. 1 TCCA (LSTC) C-LSA08-018/D BOMBARDIER DHC-8-401, -402 G3 Water System Modification: TCCA LSTC C- LSA08-018/D, Issue 3, dated 14September 2009. 10027252 FIELD AVIATION COMPANY Inc. P- EASA.IM.A.S.02934 TCCA STC SA09-15 DHC-8-314 Icelandic Coast Guard Maritime Patrol ModificationTCCA STC Number: SA09-15, Issue 1 dated 29. April 2009 10029315 FIELD AVIATION COMPANY INC. TCCA STC SA02-86 DHC-8-102, -103, -106, -201 DHC-8-202, -301, -311, -314 DHC-8-315 10030757 FIELD AVIATION COMPANY Inc. P- EASA.IM.A.S.03226 TCCA STC SA92-93 ISSUE 4 DHC-8-102, -103, -106, -201 DHC-8-301, -311, -314, -315 Installation of a HF Antenna into the Vertical Stabilizer Leading Edgefor an Allied Signal KHF-950 HF Transceiver.TCCA STC SA02- 86, Issue 2 Installation is limited to Serial Numbers 435, 440, 441 and 407 Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The install 1. Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product;2. Prior to installation of this modification it 23.05.2012 must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. None. The installation of this modification by third persons is subject towritten permission of the approval holder and holding and disposal ofthe approved appropriate documentation. Prior to installation of this modification the UNS-1F(w) Flight Management Systems approved for En-route, Terminal andNon Precision approach operations only. External LAN System not approved for airborne operations. External Nokia Cellular Telephone System not approved for airborne use. The authorizati Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. installer must determinethat the The installation of this modification by third persons is subject towritten permission of the approval holder and holding and disposal ofthe approved appropriate documentation. Prior to installation of this modification it must be determined thatthe interr De-Icer Boot Installation None. 1. Prior to installation of this modification the installer mustdetermine that the ,,interrelationship between this modification and anyother previously installed ,,modification will introduce no adverseeffect upon the airworthiness of the product.2. The i 10031816 FIELD AVIATION COMPANY Inc. CAA STC 2004-5141 TCCA STC SH88-1 AS 332 L, AS 332 L1 Installation of 4 Place Auxiliary Seat TankThis None Prior to installation of this modification it 22.12.2010 EASA STC revises CAA STC 2004-5141 must be determined thatthe dated 14 may 2004 and adds modelAS332L1. interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness of the product. 04/01/2013 Page 215/462 15.08.2008 28.08.2008 21.09.2009 16.09.2009 18.03.2010 03.07.2009
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