# Aerospatiale SA-365-C1 - Type: Aircraft model (FAA registry) - Registry code: 8680666 - Manufacturer (registry): AEROSPATIALE - Model: SA-365-C1 - Aircraft type: Rotorcraft - Category: Rotorcraft - Engines: 2 · Turbo-shaft - Seats: 13 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS H10EU](https://openairdocs.org/tcds/H10EU) (OpenAirDocs) - Holder: Airbus Helicopters - Registered aircraft: 0 - Page: https://openairdocs.org/model/aerospatiale-sa-365-c1 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2025-03-04](https://openairdocs.org/ad/2025-03-04): Cabin Equipment/Furnishings · Airbus Helicopters AS332L, AS332L1, AS-365N3 and 4 more. Effective Feb 19, 2025 - [AD 2023-22-14](https://openairdocs.org/ad/2023-22-14): Tail rotor gearbox · Airbus Helicopters SA-365C1, SA-365C2 and SA-365N. Effective Dec 26, 2023 - [AD 2023-11-07](https://openairdocs.org/ad/2023-11-07): Ground Proximity System · Airbus Helicopters 47, 206, 210 and 237 more. Effective Jun 22, 2023 - [AD 2022-10-09](https://openairdocs.org/ad/2022-10-09): Main Rotor Gearbox · Airbus Helicopters SA-365C1 and SA-365C2. Effective Jun 16, 2022 - [AD 2022-01-03](https://openairdocs.org/ad/2022-01-03): Fire Bottle, Portable · Airbus Helicopters AS332C, AS332C1, AS332L and 35 more. Effective Mar 7, 2022 - [AD 2022-01-01](https://openairdocs.org/ad/2022-01-01): Main Rotor System · Airbus Helicopters AS350B, AS350BA, AS350B1 and 17 more. Effective Mar 7, 2022 - [AD 2021-26-18](https://openairdocs.org/ad/2021-26-18): Tail Rotor Drive System · Airbus Helicopters AS-365N2, AS-365N3, SA-365N1 and 5 more. Effective Feb 9, 2022 - [AD 2021-22-07](https://openairdocs.org/ad/2021-22-07): Fire Bottle, Portable · Airbus A319-111, A319-112, A319-113 and 127 more. Effective Nov 18, 2021 - [AD 2020-10-02](https://openairdocs.org/ad/2020-10-02): Main Rotor System · Airbus Helicopters AS-365N2, AS-365N3, SA-365C and 5 more. Effective Jun 15, 2020 - [AD 2018-11-03](https://openairdocs.org/ad/2018-11-03): Main Rotor Head · Airbus Helicopters SA-365C, SA-365C1 and SA-365C2. Effective Jun 18, 2018 - [AD 2012-26-10](https://openairdocs.org/ad/2012-26-10): Main Rotor Gearbox · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 7 more. Effective Feb 13, 2013 - [AD 2012-05-01](https://openairdocs.org/ad/2012-05-01): Main Rotor Head · Airbus Helicopters AS-365N2, AS-365N3, SA-365C and 5 more. Effective Apr 24, 2012 - [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 2008-04-03](https://openairdocs.org/ad/2008-04-03): Main rotor hub · Airbus Helicopters AS-365N2, AS-365N3, SA-365C and 4 more. Effective Mar 6, 2008 - [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 2003-14-12](https://openairdocs.org/ad/2003-14-12): Equipment Log Card (FME) · Airbus Helicopters AS-365N2, AS-365N3, AS332C and 23 more. Effective Aug 25, 2003 - [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 2000-11-18](https://openairdocs.org/ad/2000-11-18): Bearing Attachment Joint · Airbus Helicopters AS-365N2, AS-365N3, SA-365C and 5 more. Effective Jul 11, 2000 - [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 85-15-01 R2](https://openairdocs.org/ad/85-15-01-R2): Main Rotor Mask · Airbus Helicopters SA-365C, SA-365C1, SA-365C2 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 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 86-21-01](https://openairdocs.org/ad/86-21-01): Main Rotor Head Sleeves · Airbus Helicopters SA-365C, SA-365C1, SA-365C2 and 2 more. Effective Oct 24, 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 81-10-09](https://openairdocs.org/ad/81-10-09): Tail Rotor Gearbox Mount Assembly · Airbus Helicopters SA-365C, SA-365C1 and SA-365C2. Effective Apr 30, 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 80-15-05](https://openairdocs.org/ad/80-15-05): Spherical Thrust Bearing Rear Block · Airbus Helicopters SA-365C, SA-365C1, SA-365C2 and 5 more. Effective Jul 14, 1980 Historical (superseded or no longer in force): - [AD 2021-23-13](https://openairdocs.org/ad/2021-23-13) (historical): Ground Proximity System · Airbus Helicopters K-225, K-190A, K-240 and 237 more. Effective Dec 9, 2021 - [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 99-21-24](https://openairdocs.org/ad/99-21-24) (historical): Tightening Torque Of Bolts Inspection · Eurocopter France AS-365N2, SA-365C, SA-365C1 and 4 more. Effective Nov 18, 1999 ## Information bulletins (advisory) (1) - [SAIB SW-15-07](https://openairdocs.org/saib/SW-15-07): Rotor Drive-Tail Rotor Drive Flange Shur-Lok Nut Inspection. Issued Dec 30, 2014 ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## STCs that may be installed (OpenAirDocs) (19) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [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 SR01343LA](https://openairdocs.org/stc/SR01343LA): Installation of MASS Systems fire extinguisher cartridges as replacements for W. Kidde Aerospace/L Hotellier/Dexaero fire extinguisher cartridges in fire extinguisher bottles installed in the rotorcraft models noted on the FAA Approved Model List SR01343LA dated June 28, 2002, or later FAA approved revisions. This cartridge is in accordance with MASS Systems Master Drawing List MDL-861345, Revision N/C, dated May 31, 2002, or later FAA approved revisions. AMETEK AMERON LLC d/b/a MASS Systems - [STC SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories. Electronics International Inc - [STC SA00680SE](https://openairdocs.org/stc/SA00680SE): 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 SH2987SW-D](https://openairdocs.org/stc/SH2987SW-D): Installation of external markings. American Eurocopter Corporation - [STC SH4050SW-D](https://openairdocs.org/stc/SH4050SW-D): Installation of 12-place interior with forward facing seats. American Eurocopter Corporation - [STC SH4052SW-D](https://openairdocs.org/stc/SH4052SW-D): Modification of lower cabin flexiglass panels. American Eurocopter Corporation - [STC SH4209SW-D](https://openairdocs.org/stc/SH4209SW-D): Relocation of aft row of seats. American Eurocopter Corporation - [STC SH4252SW-D](https://openairdocs.org/stc/SH4252SW-D): Installation of Blabe Bolt Balance Pin Adapter. American Eurocopter Corporation - [STC SH4253SW-D](https://openairdocs.org/stc/SH4253SW-D): Installation of Soundproofing per Drawing H360-89-3D-001 latest FAA approved revision. American Eurocopter Corporation - [STC SR01225NY](https://openairdocs.org/stc/SR01225NY): Installation of Pacific Scientific P/N 0118037-01 or -03 restraint system. Pacific Scientific - [STC SH2987SW](https://openairdocs.org/stc/SH2987SW): External markings. American Eurocopter Corporation - [STC SH4050SW](https://openairdocs.org/stc/SH4050SW): Twelve-place interior with forward facing seats. American Eurocopter Corporation - [STC SH4052SW](https://openairdocs.org/stc/SH4052SW): 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 SH198RM](https://openairdocs.org/stc/SH198RM): Installation of new auxiliary fuel tank and litter installation. Heli Med Evacuation 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.