# N341AS: 1972 S N I A S SA341G - Status: Valid registration - Airframe: [S N I A S SA341G](https://openairdocs.org/model/s-n-i-a-s-sa341g) (registry code 868016A, 5 seats) - Engine: [Turbomeca ASTAZOU-111A](https://openairdocs.org/engine/turbomeca-astazou-111a) (registry code 60007) - Data sheets: [TCDS H6EU](https://openairdocs.org/tcds/H6EU) (Airbus Helicopters) (OpenAirDocs) - Serial number: 1042 - Year built: 1972 - Type: Rotorcraft - Engine type: Turbo-shaft - Airworthiness: Standard, normal - Airworthiness date: September 2, 2013 - Certificate issued: January 23, 2026 - Expires: January 31, 2033 - Mode S code: A3C116 - Registered owner: [International Air Services Inc Owner Trustee](https://openairdocs.org/faa-owner/INTERNATIONAL%20AIR%20SERVICES%20INC%20OWNER%20TRUSTEE) - Location: [Carson City, NV](https://openairdocs.org/faa-place/NV/Carson%20City) - Owner type: Corporation - Owner's area on the map: 39.2227° N, 119.7016° W: Placed by OpenAirDocs at the center of ZIP code 89706, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=341AS - Page: https://openairdocs.org/aircraft/N341AS From the FAA registry file of October 22, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 25 in force ### Matched by airframe (S N I A S SA341G) - [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 76-02-03](https://openairdocs.org/ad/76-02-03): Hydraulic Unit Drive · Airbus Helicopters SA341G. Effective Jan 30, 1976 - [AD 76-02-02](https://openairdocs.org/ad/76-02-02): Tail Rotor Drive System · 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 75-17-26](https://openairdocs.org/ad/75-17-26): Over-Torquing of Engine · Airbus Helicopters SA341G. Effective Aug 20, 1975 - [AD 75-17-25](https://openairdocs.org/ad/75-17-25): Main Rotor Head · Airbus Helicopters SA341G. Effective Aug 20, 1975 - [AD 75-17-20](https://openairdocs.org/ad/75-17-20): Main Rotor Blade · Airbus Helicopters SA341G. Effective Aug 19, 1975 ### Matched by engine (Turbomeca ASTAZOU-111A) None in force. ### Historical (superseded or no longer in force) - [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 ## Information bulletins (advisory) (1 in force) - [SAIB SW-04-81](https://openairdocs.org/saib/SW-04-81): . Issued Aug 27, 2004 ## NTSB investigations None matched to N341AS. ## FAA accident and incident reports None matched to N341AS. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## STCs that may be installed (OpenAirDocs) (59, first 50) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (S N I A S SA341G) - [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 59: https://openairdocs.org/aircraft/N341AS/stcs.md ## Earlier aircraft with N341AS The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N341AS before. - [Cancelled 1991-04-30](https://openairdocs.org/deregistered/N341AS-1991-04-30): Stranz Albert BARRACUDA, S/N 341. Triennial form not returned. Owner: [Stranz Albert](https://openairdocs.org/faa-owner/STRANZ%20ALBERT), [Tucson, AZ](https://openairdocs.org/faa-place/AZ/Tucson) ## Related - Other S N I A S SA341G aircraft: https://openairdocs.org/model/s-n-i-a-s-sa341g/aircraft.md - The Turbomeca ASTAZOU-111A engine: https://openairdocs.org/engine/turbomeca-astazou-111a.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.