# Aerospatiale SA-366-G1 - Type: Aircraft model (FAA registry) - Registry code: 8680820 - Manufacturer (registry): AEROSPATIALE - Model: SA-366-G1 - Aircraft type: Rotorcraft - Category: Rotorcraft - Engines: 2 · Turbo-shaft - Seats: 2 - 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-366-g1 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 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 2022-09-04](https://openairdocs.org/ad/2022-09-04): Tail Rotor Drive System · Airbus Helicopters SA-365N1, AS-365N2, AS-365N3 and 3 more. Effective May 31, 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 2021-14-16](https://openairdocs.org/ad/2021-14-16): Fuselage Main, Frame · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 2 more. Effective Aug 24, 2021 - [AD 2021-02-08](https://openairdocs.org/ad/2021-02-08): Fuselage Structure · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 4 more. Effective Apr 15, 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 2016-09-09](https://openairdocs.org/ad/2016-09-09): Fuselage Main, Frame · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 2 more. Effective Jun 10, 2016 - [AD 2015-11-06](https://openairdocs.org/ad/2015-11-06): Main Rotor Control · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 4 more. Effective Jul 13, 2015 - [AD 2013-12-04](https://openairdocs.org/ad/2013-12-04): Fuel storage · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 4 more. Effective Aug 2, 2013 - [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 2012-17-02](https://openairdocs.org/ad/2012-17-02): Cracked main rotor mast nut · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 4 more. Effective Oct 10, 2012 - [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 2010-06-07](https://openairdocs.org/ad/2010-06-07): Rotorcraft Flight Control · Airbus Helicopters AS-365N2, AS-365N3, AS332C and 14 more. Effective Apr 21, 2010 - [AD 2004-16-15 R1](https://openairdocs.org/ad/2004-16-15-R1): Main gearbox (MGB) base plate · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 4 more. Effective Aug 30, 2006 - [AD 2006-06-02](https://openairdocs.org/ad/2006-06-02): Main gearbox (MGB) · Airbus Helicopters AS-365N2, SA-365N, SA-365N1 and 1 more. Effective Apr 17, 2006 - [AD 2003-14-19](https://openairdocs.org/ad/2003-14-19): Main servocontrols · Airbus Helicopters AS-365N2, AS-365N3, AS355F and 7 more. Effective Aug 21, 2003 - [AD 2003-08-53](https://openairdocs.org/ad/2003-08-53): Tail rotor blade (blade) · Airbus Helicopters AS-365N2, AS-365N3, SA-365N1 and 1 more. Effective Jun 20, 2003 - [AD 2000-11-17](https://openairdocs.org/ad/2000-11-17): Tail Rotor Blade · Airbus Helicopters AS-365N2, SA-365N1 and SA-366G1. Effective Jul 12, 2000 - [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 2000-08-06](https://openairdocs.org/ad/2000-08-06): Electrical Modules · Airbus Helicopters SA-366G1. Effective May 24, 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 99-11-11](https://openairdocs.org/ad/99-11-11): Main Gear Box Gear Shaft For Crack Inspection · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 2 more. Effective Jun 10, 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 98-12-08](https://openairdocs.org/ad/98-12-08): Main Gearbox Strut Attachment · Airbus Helicopters AS-365N2, SA-365N, SA-365N1 and 1 more. Effective Jul 9, 1998 - [AD 98-06-35](https://openairdocs.org/ad/98-06-35): Inspect Kevlar Tie-Bar · Airbus Helicopters SA-366G1. Effective Apr 6, 1998 - [AD 98-05-01](https://openairdocs.org/ad/98-05-01): Main Rotor Head Frequency Adapter · Airbus Helicopters SA-366G1. Effective Apr 3, 1998 - [AD 98-05-17](https://openairdocs.org/ad/98-05-17): Outboard Fin Attachment Studs and Washers · Airbus Helicopters AS-365N2, SA-365N, SA-365N1 and 1 more. Effective Mar 23, 1998 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 2021-05-05](https://openairdocs.org/ad/2021-05-05) (historical): Tail Rotor · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Apr 16, 2021 - [AD 2018-19-01](https://openairdocs.org/ad/2018-19-01) (historical): Rotorcraft tail boom · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Oct 22, 2018 - [AD 2016-23-05](https://openairdocs.org/ad/2016-23-05) (historical): Tail Rotor Gearbox · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Dec 12, 2016 - [AD 2013-18-01](https://openairdocs.org/ad/2013-18-01) (historical): Main Rotor Control · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 4 more. Effective Oct 18, 2013 - [AD 2013-08-17](https://openairdocs.org/ad/2013-08-17) (historical): Fuselage Main, Frame · Airbus Helicopters AS-365N2, AS-365N3, SA-365N and 2 more. Effective Jun 5, 2013 - [AD 2007-25-08](https://openairdocs.org/ad/2007-25-08) (historical): T/R gearbox (TGB) · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective Jan 14, 2008 - [AD 2006-09-10](https://openairdocs.org/ad/2006-09-10) (historical): Pitch control rod assembly double bearing (bearing) · Airbus Helicopters AS-365N2, AS-365N3, EC 155B and 3 more. Effective May 18, 2006 - [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 2004-16-15](https://openairdocs.org/ad/2004-16-15) (historical): Main gearbox (MGB) · Eurocopter France AS-365N2, AS-365N3, EC 155B and 4 more. Effective Sep 3, 2004 - [AD 2000-10-08 R1](https://openairdocs.org/ad/2000-10-08-R1) (historical): Tail Rotor Blade · Eurocopter France AS-365N2, SA-365N1 and SA-366G1. Effective Nov 7, 2001 - [AD 2000-10-08](https://openairdocs.org/ad/2000-10-08) (historical): Tail Rotor Blades · Eurocopter France AS-365N2, SA-365N1 and SA-366G1. Effective Jun 21, 2000 - [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 - [AD 98-10-04](https://openairdocs.org/ad/98-10-04) (historical): Kevlar Tie-Bar Inspection · Eurocopter France AS-365N2, SA-365N1 and SA-366G1. Effective Jun 11, 1998 - [AD 97-15-15](https://openairdocs.org/ad/97-15-15) (historical): Main Gear Box Planetary Gear Shaft · Eurocopter France SA-365N, SA-365N1 and SA-366G1. Effective Feb 23, 1998 ## Information bulletins (advisory) (2) - [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 - [SAIB SW-05-01](https://openairdocs.org/saib/SW-05-01): . Issued Oct 7, 2004 ## 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) (11) 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 SA2693NM](https://openairdocs.org/stc/SA2693NM): Installation of Electronics International digital volt/amp gauges and accessories. Electronics International Inc - [STC SH5866SW](https://openairdocs.org/stc/SH5866SW): Installation of forward facing recognition lights. DeVore Aviation Corporation of America, a New Mexico Corporation - [STC SH5867SW](https://openairdocs.org/stc/SH5867SW): Installation of tail floodlights. DeVore Aviation Corporation of America, a New Mexico Corporation - [STC SH5400SW-D](https://openairdocs.org/stc/SH5400SW-D): Installation of equipment per AHC Drawing List 366-R-076 latest FAA approved revision, to add IFR and night conditions to eligible types of operation. Approved types of operations will be VFR, IFR, Day/Night, non-icing conditions. American Eurocopter Corporation - [STC SH5401SW-D](https://openairdocs.org/stc/SH5401SW-D): Installation of Standby Gyro. American Eurocopter Corporation - [STC SH5402SW-D](https://openairdocs.org/stc/SH5402SW-D): Installation of emergency locator transmitter. American Eurocopter Corporation - [STC SH5403SW-D](https://openairdocs.org/stc/SH5403SW-D): Addition of fire detection features to the main transmission compartment and addition of fire resistant features. American Eurocopter Corporation - [STC SH5404SW-D](https://openairdocs.org/stc/SH5404SW-D): Installation of single passenger seat. American Eurocopter Corporation - [STC SH5405SW-D](https://openairdocs.org/stc/SH5405SW-D): Installation of two passenger seat. American Eurocopter Corporation - [STC SA4302NM](https://openairdocs.org/stc/SA4302NM): Installation of Electronics Int'l digital automatic engine analyzer. Electronics International --- 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.