# TCDS H8EU: Eurocopter France - Type: Type certificate data sheet - Status: Current - Holder: Eurocopter France - Revision: 3 - Revised: February 15, 2007 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 29 - Data sheet PDF: https://openairdocs.org/files/sha256/cf/41/cf413333e79e983f9135cee5976da3550b6f0d0e1f966baec05e1278c147064c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1FF18C0E2A32C43A8625728800759E62.0001 - Page: https://openairdocs.org/tcds/H8EU ## Models (1) As the data sheet lists them. - SA-360C Dauphin ## ADs (18, in force first) - [AD 2021-14-15](https://openairdocs.org/ad/2021-14-15): Main Rotor Head · Airbus Helicopters SA341G, SA342J and SA-360C Dauphin. Effective Aug 10, 2021 - [AD 2010-20-20](https://openairdocs.org/ad/2010-20-20): MGB planet gear carrier · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 8 more. Effective Nov 12, 2010 - [AD 2006-08-06](https://openairdocs.org/ad/2006-08-06): Main gearbox (MGB) base plate · Airbus Helicopters SA-360C Dauphin, SA-365C, SA-365C1 and 1 more. Effective Apr 28, 2006 - [AD 2002-20-03](https://openairdocs.org/ad/2002-20-03): Ferry fuel tank (tank) electrostatic ground connector · Airbus Helicopters AS-365N2, AS-365N3, AS332C and 24 more. Effective Nov 6, 2002 - [AD 99-21-14](https://openairdocs.org/ad/99-21-14): Electrical Master Box Assembly Inspection · Airbus Helicopters AS-365N2, SA-360C Dauphin, SA-365C and 5 more. Effective Nov 12, 1999 - [AD 99-21-01](https://openairdocs.org/ad/99-21-01): Electrical System · Airbus Helicopters SA-360C Dauphin, SA-365C, SA-365C1 and 1 more. Effective Oct 19, 1999 - [AD 98-24-32](https://openairdocs.org/ad/98-24-32): Tail Rotor Hub Fairing Attachment Spring · Airbus Helicopters AS-365N2, SA-360C Dauphin, SA-365C and 5 more. Effective Dec 14, 1998 - [AD 98-12-29](https://openairdocs.org/ad/98-12-29): Electric Hoists · Airbus Helicopters SA-360C Dauphin, SA-365C, SA-365C1 and 4 more. Effective Jul 15, 1998 - [AD 97-26-18](https://openairdocs.org/ad/97-26-18): Main Gear Box Bevel Pinion P/N 360A32-1021-20 · Airbus Helicopters SA-360C Dauphin. Effective Jan 5, 1998 - [AD 81-14-51 R1](https://openairdocs.org/ad/81-14-51-R1): Tail Rotor Fairing And Hub · Airbus Helicopters SA-360C Dauphin, SA-365C, SA-365C1 and 2 more. Effective Jan 15, 1988 - [AD 85-26-01](https://openairdocs.org/ad/85-26-01): Safety Belts · Airbus Helicopters SA-360C Dauphin and Safety Belts. Effective Feb 6, 1986 - [AD 82-05-04](https://openairdocs.org/ad/82-05-04): Pilot/Co-Pilot Seat Slides · Airbus Helicopters SA-360C Dauphin, SA-365C, SA-365C1 and 1 more. Effective Mar 12, 1982 - [AD 81-26-02](https://openairdocs.org/ad/81-26-02): Stabilizer Spar Tube Structure · Airbus Helicopters SA-360C Dauphin, SA-365C, SA-365C1 and 1 more. Effective Dec 21, 1981 - [AD 80-21-52](https://openairdocs.org/ad/80-21-52): Main Rotor Speed Loss · Airbus Helicopters SA-360C Dauphin. Effective May 6, 1981 - [AD 81-01-51](https://openairdocs.org/ad/81-01-51): Tail Boom · Airbus Helicopters SA-360C Dauphin, SA-365C, SA-365C1 and 1 more. Effective Feb 28, 1981 - [AD 2005-03-09](https://openairdocs.org/ad/2005-03-09) (historical): Main gearbox (MGB) planet gear · Eurocopter France AS-365N2, AS-365N3, EC 155B and 8 more. Effective Mar 1, 2005 - [AD 2002-08-16](https://openairdocs.org/ad/2002-08-16) (historical): Tie Bar · Airbus Helicopters SA-360C Dauphin, SA341G and SA342J. Effective May 8, 2002 - [AD 2001-19-51](https://openairdocs.org/ad/2001-19-51) (historical): Main Rotor Head Torsion Tie Bar · Eurocopter France SA-360C Dauphin, SA341G and SA342J. Effective Dec 10, 2001 ## Registered aircraft by registry model (OpenAirDocs) - [Aerospatiale SA-360C "DAUPHIN"](https://openairdocs.org/model/aerospatiale-sa-360c-dauphin): 0 aircraft (registry code 8680662) ## STCs approved under this data sheet (38) - [STC SH3319NM](https://openairdocs.org/stc/SH3319NM): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc - [STC SH5905SW](https://openairdocs.org/stc/SH5905SW): Installation of 110 vac inverter system - E.M.S.. RSG Products Inc - [STC SH5906SW](https://openairdocs.org/stc/SH5906SW): Installation of dual vacuum system - E.M.S.. RSG Products Inc - [STC SH5907SW](https://openairdocs.org/stc/SH5907SW): Installation of dual oxygen system - E.M.S.. RSG Products Inc - [STC SH5908SW](https://openairdocs.org/stc/SH5908SW): Installation of dual compressed air system - E.M.S.. RSG Products Inc - [STC SH5909SW](https://openairdocs.org/stc/SH5909SW): Installation of dual patient stowable litter - E.M.S.. RSG Products Inc - [STC SH5910SW](https://openairdocs.org/stc/SH5910SW): Installation of dual attendant seats and modification of co-pilot seat - E.M.S.. RSG Products Inc - [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories.. Electronics International Inc. - [STC SA00680SE (5 OF 6](https://openairdocs.org/stc/SA00680SE%20(5%20OF%206): Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.. Electronics International - [STC SR00811NY](https://openairdocs.org/stc/SR00811NY): Installation of Technisonic Industries Limited TFM-138 series transceiver models.. Technisonic Industries Limited - [STC SR01834NY](https://openairdocs.org/stc/SR01834NY): Installation of Globalstar Satellite Telephone System.. Atlantic Avionics Inc. - [STC SH2402SW-D](https://openairdocs.org/stc/SH2402SW-D): Installation of emergency lighting system.. American Eurocopter Corporation - [STC SH2441SW-D](https://openairdocs.org/stc/SH2441SW-D): Installation of soundproofing.. American Eurocopter Corporation - [STC SH2445SW-D](https://openairdocs.org/stc/SH2445SW-D): Installation of exterior markings.. American Eurocopter Corporation - [STC SH2707SW-D](https://openairdocs.org/stc/SH2707SW-D): Installation of stability augmentation/avionics equipment and cockpit modifications for certification of single and dual pilot day-night VFR/IFR (IMC) operations. Limited to installation on serial number 1006 ONLY.. American Eurocopter Corporation - [STC SH2708SW-D](https://openairdocs.org/stc/SH2708SW-D): Installation of alternate anti-collision strobe lights.. American Eurocopter Corporation - [STC SH2962SW-D](https://openairdocs.org/stc/SH2962SW-D): Installation of blade bolt balance pin adapter.. American Eurocopter Corporation - [STC SH4019SW-D](https://openairdocs.org/stc/SH4019SW-D): Installation of RCA Primus 50 Radar.. American Eurocopter Corporation - [STC SH4051SW-D](https://openairdocs.org/stc/SH4051SW-D): Modification of lower cabin flexiglass panels.. American Eurocopter Corporation - [STC SH4208SW-D](https://openairdocs.org/stc/SH4208SW-D): Relocation of aft row of seats.. American Eurocopter Corporation - [STC SH2441SW](https://openairdocs.org/stc/SH2441SW): Installation of soundproofing.. American Eurocopter Corporation - [STC SH2445SW](https://openairdocs.org/stc/SH2445SW): Installation of exterior markings.. American Eurocopter Corporation - [STC SH2707SW](https://openairdocs.org/stc/SH2707SW): Installation of stability augmentation/avionics equipment and cockpit modification for certification of single and dual pilot day-night VFR/IFR (IMC) operations.. American Eurocopter Corporation - [STC SH2708SW](https://openairdocs.org/stc/SH2708SW): Alternate anti-collision/strobe lights.. American Eurocopter Corporation - [STC SH2962SW](https://openairdocs.org/stc/SH2962SW): Blade bolt balance pin adapter.. American Eurocopter Corporation - [STC SH4019SW](https://openairdocs.org/stc/SH4019SW): Installation of RCA Primus 50 radar.. American Eurocopter Corporation - [STC SH4051SW](https://openairdocs.org/stc/SH4051SW): Modification of lower cabin plexiglass panels.. American Eurocopter Corporation - [STC SA1626NM PAGE 1](https://openairdocs.org/stc/SA1626NM%20PAGE%201): Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series). Electronics International - [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer.. Electronics International - [STC SH103NE](https://openairdocs.org/stc/SH103NE): Replacement of auxiliary fuel boost pumps with Parker-Hannifin- Airborne centrifugal boost pumps, Model1C44-1.. Parker Hannifin Corp - [STC SH1179EA](https://openairdocs.org/stc/SH1179EA): Installation of DeVore tail floodlight on upper surfaces of horizontal stabilizer.. DeVore Aviation Corporation of America, a New Mexico Corporation - [STC SH2319SW](https://openairdocs.org/stc/SH2319SW): Seat modification.. Ward Intl Aircraft Service - [STC SH2320SW](https://openairdocs.org/stc/SH2320SW): Installation of bar.. Ward Intl Aircraft Service - [STC SH2321SW](https://openairdocs.org/stc/SH2321SW): Install folding table.. Ward Intl Aircraft Service - [STC SH2322SW](https://openairdocs.org/stc/SH2322SW): Installation of coat closet.. Ward Intl Aircraft Service - [STC SH2323SW](https://openairdocs.org/stc/SH2323SW): Installation of trash container.. Ward Intl Aircraft Service - [STC SH2324SW](https://openairdocs.org/stc/SH2324SW): Inner-window assembly.. Ward Intl Aircraft Service - [STC SH3319NM (1 OF 2)](https://openairdocs.org/stc/SH3319NM%20(1%20OF%202)) (historical): Installation of Precise Flight Pulselite Control Unit in the Landing /Taxi Recognition Visual Control Light system,. Precise Flight Inc --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.