# TCDS H6EU: Airbus Helicopters - Type: Type certificate data sheet - Status: Current - Holder: Airbus Helicopters - Revision: 6 - Revised: January 10, 2014 - Product: Aircraft, Rotorcraft - Certification basis: Part 21, Part 27 - Registered aircraft: 29, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/a8/db/a8dbaba4320ea5cc0809a9d5e0d8eb73db0627579dff3abf40e4a816bb7062ab - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A94938A95C756B3D86257C6700615624.0001 - Page: https://openairdocs.org/tcds/H6EU ## Models (2) As the data sheet lists them. - SA341G - SA342J ## ADs (30, in force first) - [AD 2025-25-06](https://openairdocs.org/ad/2025-25-06): Main Rotor Blades · Airbus Helicopters SA341G and SA342J. Effective Feb 6, 2026 - [AD 2025-08-08](https://openairdocs.org/ad/2025-08-08): Tail Rotor Drive Shaft · Airbus Helicopters SA341G and SA342J. Effective Jun 6, 2025 - [AD 2025-05-05](https://openairdocs.org/ad/2025-05-05): Flight Control System · Airbus Helicopters SA341G and SA342J. Effective May 12, 2025 - [AD 2023-13-51](https://openairdocs.org/ad/2023-13-51): Tail Rotor Blades · Airbus Helicopters SA341G and SA342J. Effective Aug 8, 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 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 2021-08-05](https://openairdocs.org/ad/2021-08-05): Tail Rotor Blades · Airbus Helicopters SA341G and SA342J. Effective Jun 1, 2021 - [AD 2017-12-04](https://openairdocs.org/ad/2017-12-04): Main Landing Gear Strut/Axel/Truck. · Airbus Helicopters SA341G and SA342J. Effective Jun 27, 2017 - [AD 2016-07-27](https://openairdocs.org/ad/2016-07-27): Main Rotor · Airbus Helicopters SA341G and SA342J. Effective May 18, 2016 - [AD 2012-17-09](https://openairdocs.org/ad/2012-17-09): Main Rotor Head · Airbus Helicopters SA341G. Effective Oct 19, 2012 - [AD 2011-11-04](https://openairdocs.org/ad/2011-11-04): Contaminated Gas · Airbus Helicopters AS355E, AS355F, AS355F1 and 12 more. Effective Jun 17, 2011 - [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 2003-04-13](https://openairdocs.org/ad/2003-04-13): Limiting Resistor in Electric Hoist Junction Box · Airbus Helicopters SA341G and SA342J. Effective Mar 17, 2003 - [AD 2000-10-05](https://openairdocs.org/ad/2000-10-05): Flotation Gear Nitrogen Cylinders · Airbus Helicopters SA330F, SA330G, SA330J and 6 more. Effective Jun 29, 2000 - [AD 99-11-03](https://openairdocs.org/ad/99-11-03): Main Rotor Head Pitch Change Rod · Airbus Helicopters SA341G and SA342J. Effective Jun 2, 1999 - [AD 98-06-36](https://openairdocs.org/ad/98-06-36): Tail Gearbox Support Tripod Inspection · Airbus Helicopters SA341G and SA342J. Effective Apr 6, 1998 - [AD 77-22-04](https://openairdocs.org/ad/77-22-04): Landing Gear · Airbus Helicopters SA341G. Effective Nov 28, 1977 - [AD 76-07-10](https://openairdocs.org/ad/76-07-10): Main Gear Box Attachment · Airbus Helicopters SA341G. Effective Apr 22, 1976 - [AD 76-02-02](https://openairdocs.org/ad/76-02-02): Tail Rotor Drive System · Airbus Helicopters SA341G. Effective Jan 30, 1976 - [AD 76-02-03](https://openairdocs.org/ad/76-02-03): Hydraulic Unit Drive · Airbus Helicopters SA341G. Effective Jan 30, 1976 - [AD 75-27-04](https://openairdocs.org/ad/75-27-04): Fuel System Modification · Airbus Helicopters SA341G. Effective Jan 19, 1976 - [AD 75-22-07](https://openairdocs.org/ad/75-22-07): Main Gear Boxes · Airbus Helicopters SA341G. Effective Nov 3, 1975 - [AD 75-17-25](https://openairdocs.org/ad/75-17-25): Main Rotor Head · Airbus Helicopters SA341G. Effective Aug 20, 1975 - [AD 75-17-26](https://openairdocs.org/ad/75-17-26): Over-Torquing of Engine · Airbus Helicopters SA341G. Effective Aug 20, 1975 - [AD 75-17-20](https://openairdocs.org/ad/75-17-20): Main Rotor Blade · Airbus Helicopters SA341G. Effective Aug 19, 1975 - [AD 2022-19-08](https://openairdocs.org/ad/2022-19-08) (historical): Tail Rotor Blades · Airbus Helicopters SA341G and SA342J. Effective Oct 3, 2022 - [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 2016-20-04](https://openairdocs.org/ad/2016-20-04) (historical): Main Landing Gear Strut/Axel/Truck · Airbus Helicopters SA341G and SA342J. Effective Oct 18, 2016 - [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 SA341G GAZELLE](https://openairdocs.org/model/aerospatiale-sa341g-gazelle): 20 aircraft (registry code 8680610) - [Aerospatiale SA342J](https://openairdocs.org/model/aerospatiale-sa342j): 4 aircraft (registry code 8680828) - [S N I A S SA341G](https://openairdocs.org/model/s-n-i-a-s-sa341g): 2 aircraft (registry code 868016A) - [Eurocopter France GAZELLE SA342J](https://openairdocs.org/model/eurocopter-france-gazelle-sa342j): 1 aircraft (registry code 8680974) - [Eurocopter France SA 341G](https://openairdocs.org/model/eurocopter-france-sa-341g): 1 aircraft (registry code 868097L) - [Eurocopter France SA342J](https://openairdocs.org/model/eurocopter-france-sa342j): 1 aircraft (registry code 868097K) - [Sud GAZELLE SA 342J](https://openairdocs.org/model/sud-gazelle-sa-342j): 0 aircraft (registry code 8680822) ## STCs approved under this data sheet (60, first 50) - [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 SR02704SE](https://openairdocs.org/stc/SR02704SE): Installation and maintenance of the Sunspot 36 and 46 series lights. AeroLED's Holdings LLC - [STC SR00359BO](https://openairdocs.org/stc/SR00359BO): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [STC SR02487AK](https://openairdocs.org/stc/SR02487AK): Installation of L-3 Communications Avionics Systems ESI-500 Standby Instrument System. ADS-B Technologies, LLC - [STC SR02470AK](https://openairdocs.org/stc/SR02470AK): Installation of the L-3 Communications NGT -1000/2000/2500 ADS-B System. ADS-B Technologies, LLC - [STC SR02471AK](https://openairdocs.org/stc/SR02471AK): Installation of the L-3 Communications NGT -9000/9000R ADS-B System. ADS-B Technologies, LLC - [STC SR02394AK](https://openairdocs.org/stc/SR02394AK): Replacement of existing landing and/or hover light bulbs with Light Emitting Diode (LED) lighting system. Seaplanes North LLC - [STC SH529AL](https://openairdocs.org/stc/SH529AL): Installation of Airglas L2700SA341 and L2700SA341HS skis.. Airglas Inc. - [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 SH1621SW-D](https://openairdocs.org/stc/SH1621SW-D): Installation of Eastern Rotorcraft Cargo Hook.. American Eurocopter Corporation - [STC SH1654SW-D](https://openairdocs.org/stc/SH1654SW-D): Installation of environmental control unit.. American Eurocopter Corporation - [STC SH1770SW-D](https://openairdocs.org/stc/SH1770SW-D): Installation of modified cockpit instrument panel.. American Eurocopter Corporation - [STC SH1903SW-D](https://openairdocs.org/stc/SH1903SW-D): Installation of single/dual stowable litter kit.. American Eurocopter Corporation - [STC SH1956SW-D](https://openairdocs.org/stc/SH1956SW-D): Installation of 341-78-3D-36 hourmeter kit.. American Eurocopter Corporation - [STC SH1975SW-D](https://openairdocs.org/stc/SH1975SW-D): Modification SFENA SAS System with integrated attitude and coupled (HELCIS). Limited to serial number 1003.. American Eurocopter Corporation - [STC SH2215SW-D](https://openairdocs.org/stc/SH2215SW-D): Installation of abrasion resistant tape on main rotor blade leading edge.. American Eurocopter Corporation - [STC SH2272SW-D](https://openairdocs.org/stc/SH2272SW-D): Installation of strobe lights.. American Eurocopter Corporation - [STC SH2291SW-D](https://openairdocs.org/stc/SH2291SW-D): Installation of Motorola StereoModel TM 204S, or TM416S.. American Eurocopter Corporation - [STC SH2292SW-D](https://openairdocs.org/stc/SH2292SW-D): Installation of Flitephone III system.. American Eurocopter Corporation - [STC SH2306SW-D](https://openairdocs.org/stc/SH2306SW-D): Relocation of emergency float inflation bottles and quick removal provisions for emergency floats.. American Eurocopter Corporation - [STC SH2337SW-D](https://openairdocs.org/stc/SH2337SW-D): Replace stabilizer mounting bolts with Adjusto-Fit Bolts P/N ABC 6443. Limited to installation on SA1250 ONLY.. American Eurocopter Corporation - [STC SH2347SW-D](https://openairdocs.org/stc/SH2347SW-D): Installation of a nightsun searchlight. Aircraft must be placarded: VNE - 130 Kts with SX-16C NightSun Lamp installed, and other placard on drawing H341-82-4D-012.. American Eurocopter Corporation - [STC SH2371SW-D](https://openairdocs.org/stc/SH2371SW-D): Installation of main rotor head balance provisions.. American Eurocopter Corporation - [STC SH2379SW-D](https://openairdocs.org/stc/SH2379SW-D): Extend cabin section 200mm just forward of the rear bulkhead. STC SH1858SW tail rotor drive shaft cover or other FAA approved equivalent must be installed.. American Eurocopter Corporation - [STC SH2400SW-D](https://openairdocs.org/stc/SH2400SW-D): Installation of STC SH1975SW configurations -5 and subsequent, IFR Category II certification.. American Eurocopter Corporation - [STC SH2453SW-D](https://openairdocs.org/stc/SH2453SW-D): Installation of cabin floor extension. Applicable only when STC SH2379SW (stretched version) is installed.. American Eurocopter Corporation - [STC SH2472SW-D](https://openairdocs.org/stc/SH2472SW-D): Installation of exterior markings.. American Eurocopter Corporation - [STC SH2497SW-D](https://openairdocs.org/stc/SH2497SW-D): Structural provisions and installation of ballast.. American Eurocopter Corporation - [STC SH2664SW-D](https://openairdocs.org/stc/SH2664SW-D): Installation of right hand maintenance step.. American Eurocopter Corporation - [STC SH2867SW-D](https://openairdocs.org/stc/SH2867SW-D): Installation of widened instrument panel. Limited to installation on SA341G serial number 1491 ONLY.. American Eurocopter Corporation - [STC SH2931SW-D](https://openairdocs.org/stc/SH2931SW-D): Installation of Toe Weights in the skid gear.. American Eurocopter Corporation - [STC SR01409NY](https://openairdocs.org/stc/SR01409NY): Installation of a Safe Flight Power Line Detector System.. Safe Flight Instrument Corp - [STC SR01115NY-D](https://openairdocs.org/stc/SR01115NY-D): Installation of a Safe Flight Instrument Corporation collective and pedal shaker system. Approved for serial number 1584 ONLY.. Keystone Helicopter Corp - [STC SH1956SW](https://openairdocs.org/stc/SH1956SW): Install 341-78-3D-036 hour meter kit.. American Eurocopter Corporation - [STC SH1975SW](https://openairdocs.org/stc/SH1975SW): Modification SFENA SAS system with integrated attitude and ocupled (HELCIS).. American Eurocopter Corporation - [STC SH2215SW](https://openairdocs.org/stc/SH2215SW): Installation of abrasion resistant tape on main rotor blade leading edge.. American Eurocopter Corporation - [STC SH2272SW](https://openairdocs.org/stc/SH2272SW): Installation of strobe lights.. American Eurocopter Corporation - [STC SH2291SW](https://openairdocs.org/stc/SH2291SW): Installation of Motorola stereo model TM204S or TM416S.. American Eurocopter Corporation - [STC SH2292SW](https://openairdocs.org/stc/SH2292SW): Flitephone III system.. American Eurocopter Corporation - [STC SH2337SW](https://openairdocs.org/stc/SH2337SW): Replace stabilizer mounting bolts with Adjusto-fit bolts P/N ABC 6443.. American Eurocopter Corporation - [STC SH2347SW](https://openairdocs.org/stc/SH2347SW): Install Nightsun searchlight.. American Eurocopter Corporation - [STC SH2371SW](https://openairdocs.org/stc/SH2371SW): Installation of main rotor head balance provisions.. American Eurocopter Corporation - [STC SH2379SW](https://openairdocs.org/stc/SH2379SW): Extend cabin section 200mm just forward of rear bulkhead.. American Eurocopter Corporation - [STC SH2400SW](https://openairdocs.org/stc/SH2400SW): Installation of STC SH1975SW configurations -5 and subsequent, IFR Category II certification.. American Eurocopter Corporation - [STC SH2453SW](https://openairdocs.org/stc/SH2453SW): Installation of cabin floor extension.. American Eurocopter Corporation - [STC SH2472SW](https://openairdocs.org/stc/SH2472SW): Installation of exterior markings.. American Eurocopter Corporation - [STC SH2497SW](https://openairdocs.org/stc/SH2497SW): Structural provisions and installation of ballast.. American Eurocopter Corporation - [STC SH2664SW](https://openairdocs.org/stc/SH2664SW): Install right hand maintenance step.. American Eurocopter Corporation - [STC SH2867SW](https://openairdocs.org/stc/SH2867SW): Installation of widened instrument panel.. American Eurocopter Corporation All 60: https://openairdocs.org/tcds/H6EU/stcs.md --- 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.