# N1079U: 1980 Bell 212

- Status: Valid registration
- Airframe: [Bell 212](https://openairdocs.org/model/bell-212) (registry code 1181420, 15 seats)
- Engine: [Pratt & Whitney PT6 series](https://openairdocs.org/engine/pratt-whitney-pt6-series) (registry code 52033)
- Data sheets: [TCDS H4SW](https://openairdocs.org/tcds/H4SW) (Bell Textron Inc.) (OpenAirDocs)
- Serial number: 31122
- Year built: 1980
- Type: Rotorcraft
- Engine type: Turbo-shaft
- Airworthiness: Multiple
- Airworthiness date: May 17, 1995
- Mode S code: A0225B
- Registered owner: [Turbines Ltd](https://openairdocs.org/faa-owner/TURBINES%20LTD)
- Location: [West Point, NE](https://openairdocs.org/faa-place/NE/West%20Point)
- Owner type: Corporation
- Owner's area on the map: 41.8336° N, 96.7243° W: Placed by OpenAirDocs at the center of ZIP code 68788, within about 8 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1079U
- Page: https://openairdocs.org/aircraft/N1079U

From the FAA registry file of October 24, 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. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6 model are included.

## ADs that may apply (OpenAirDocs): 99 in force

### Matched by airframe (Bell 212)

- [AD 2025-07-01](https://openairdocs.org/ad/2025-07-01): Air Data Computer · Synthetic Vision Electronic Flight Information System (Arrow STC SR09595RC or ST01523WI). Effective May 15, 2025
- [AD 2024-20-07](https://openairdocs.org/ad/2024-20-07): Emergency Equipment; Emergency Flotation Section · Apical Emergency Float Kit, P/N 20498 (STC SR00780LA or 12 others). Effective Dec 5, 2024
- [AD 2024-16-19](https://openairdocs.org/ad/2024-16-19): Rotorcraft Tail Boom · Bell Textron 212, 412CF, 412 and 1 more. Effective Nov 8, 2024
- [AD 2024-19-17](https://openairdocs.org/ad/2024-19-17): Rotorcraft flight control · Airwolf Aerospace, LLC Tension-Torsion Strap Assemblies, P/N… (STC SR03408CH). Effective Oct 11, 2024
- [AD 2024-16-01](https://openairdocs.org/ad/2024-16-01): Fuselage structure · Bell Textron 205A, 205A-1, 205B and 4 more. Effective Sep 4, 2024
- [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 2022-20-14](https://openairdocs.org/ad/2022-20-14): Main Rotor Gearbox · Bell Textron 204B, 205A, 205A-1 and 20 more. Effective Dec 27, 2022
- [AD 2022-22-12](https://openairdocs.org/ad/2022-22-12): Nose/Tail Landing Gear Structure/Axle · Replacement crosstubes P/N D212-664 (Dart Aerospace STC SR01298NY). Effective Nov 22, 2022
- [AD 2022-11-19](https://openairdocs.org/ad/2022-11-19): Aircraft Fuel System, Engine Oil System (Airframe) · Bell Textron 212, 412, 412CF and 1 more. Effective Jul 6, 2022
- [AD 2022-07-02](https://openairdocs.org/ad/2022-07-02): Rotorcraft Tail Boom · Bell Textron 205A, 205A-1, 205B and 5 more. Effective May 9, 2022
- [AD 2022-05-10](https://openairdocs.org/ad/2022-05-10): Cabin Equipment/Furnishings · Airbus Helicopters AS332L, AS332L1, AS332L2 and 57 more. Effective Apr 20, 2022
- [AD 2022-06-03](https://openairdocs.org/ad/2022-06-03): Main Rotor System · Bell Textron 204B, 205A, 205A-1 and 3 more. Effective Mar 16, 2022
- [AD 2020-19-08](https://openairdocs.org/ad/2020-19-08): Main Rotor · Bell Textron 204B, 205A-1 and 212. Effective Oct 21, 2020
- [AD 2020-16-10](https://openairdocs.org/ad/2020-16-10): Cabin Equipment/Furnishings · Bell Textron 204B, 205A, 205A-1 and 7 more. Effective Sep 3, 2020
- [AD 2020-12-10](https://openairdocs.org/ad/2020-12-10): Tail Rotor Blades · Bell Textron 205A, 205A-1, 205B and 4 more. Effective Jul 16, 2020
- [AD 2019-09-02](https://openairdocs.org/ad/2019-09-02): 7900 Engine Oil System and 2800 Aircraft Fuel System · Bell Helicopter Textron 212, 412, 412CF and 1 more. Effective Jun 4, 2019
- [AD 2018-16-14](https://openairdocs.org/ad/2018-16-14): Emergency Flotation Section · Bell Helicopter Textron 212, 412 and 412EP. Effective Oct 4, 2018
- [AD 2015-15-04](https://openairdocs.org/ad/2015-15-04): Main Rotor Blade Grip · Bell Helicopter Textron 204B, 205A, 205A-1 and 1 more. Effective Aug 7, 2015
- [AD 2014-12-04](https://openairdocs.org/ad/2014-12-04): Main Rotor Head · Bell Helicopter Textron 204B, 205A, 205A-1 and 3 more. Effective Jul 24, 2014
- [AD 2013-15-02](https://openairdocs.org/ad/2013-15-02): Tail Rotor Blades · Bell Helicopter Textron 205A, 205A-1, 205B and 5 more. Effective Aug 14, 2013
- [AD 2013-06-51](https://openairdocs.org/ad/2013-06-51): Equipment/Furnishings · Agusta A109, A109A, A109A II and 43 more. Effective Jul 15, 2013
- [AD 2013-03-16](https://openairdocs.org/ad/2013-03-16): Main Rotor Head · Bell Helicopter Textron 204B, 205A, 205A-1 and 3 more. Effective Feb 27, 2013
- [AD 2012-17-08](https://openairdocs.org/ad/2012-17-08): Main Rotor Head · Bell Helicopter Textron 204B, 205A, 205A-1 and 2 more. Effective Feb 27, 2013
- [AD 2012-22-06](https://openairdocs.org/ad/2012-22-06): High Landing Gear Forward Crosstube Assembly · Aeronautical Accessories AB412, AB412 EP, 205A and 7 more. Effective Dec 14, 2012
- [AD 2011-25-01](https://openairdocs.org/ad/2011-25-01): Liferafts · Agusta AB412, AB412 EP, 206A and 23 more. Effective Jan 17, 2012
- [AD 2011-23-02](https://openairdocs.org/ad/2011-23-02): Main rotor blade (blade) assemblies · Bell Helicopter Textron 205A-1, 205B, 210 and 1 more. Effective Nov 21, 2011
- [AD 2010-26-52](https://openairdocs.org/ad/2010-26-52): Tail Rotor Blade · Bell Helicopter Textron 204B, 205A, 205A-1 and 6 more. Effective Nov 15, 2011
- [AD 2010-10-16](https://openairdocs.org/ad/2010-10-16): Crosstube · Agusta AB412, AB412 EP, 205A and 6 more. Effective Jun 8, 2010
- [AD 2007-22-02](https://openairdocs.org/ad/2007-22-02): Tail rotor blade (blade) forward tip weight retention block (tip block) and the aft tip closure (tip closure) · Bell Helicopter Textron 205A, 205A-1, 205B and 4 more. Effective Nov 30, 2007
- [AD 2005-20-38](https://openairdocs.org/ad/2005-20-38): Reservoir assembly adapter (adapter) · Bell Helicopter Textron 212, 412 and 412EP with STC SH2820SO. Effective Oct 28, 2005
- [AD 2002-22-14](https://openairdocs.org/ad/2002-22-14): Main rotor tension-torsion (TT) straps · Bell Helicopter Textron 204B, 205A, 205A-1 and 4 more. Effective Dec 13, 2002
- [AD 2002-19-05](https://openairdocs.org/ad/2002-19-05): Tail boom · Bell Helicopter Textron 212. Effective Oct 30, 2002
- [AD 2001-13-01](https://openairdocs.org/ad/2001-13-01): Tail Rotor Counterweight Bellcrank (bellcrank) Retention Nut (retention nut) · Bell Helicopter Textron 205A-1, 205B, 212 and 3 more. Effective Aug 1, 2001
- [AD 2001-08-04](https://openairdocs.org/ad/2001-08-04): Main Rotor Actuator · Bell Helicopter Textron 205A-1, 205B, 212 and 3 more. Effective May 3, 2001
- [AD 2000-15-52](https://openairdocs.org/ad/2000-15-52): Mast and main rotor trunnions · Bell Helicopter Textron 204B, 205A, 205A-1 and 2 more. Effective Dec 28, 2000
- [AD 98-11-15](https://openairdocs.org/ad/98-11-15): Tail Rotor Yoke Assembly · Bell Helicopter Textron 212. Effective Feb 10, 1999
- [AD 94-18-09](https://openairdocs.org/ad/94-18-09): Main Transmission Lower Planetary Spider · Bell Helicopter Textron 205A, 205A-1, 205B and 2 more. Effective Oct 14, 1994
- [AD 93-17-12](https://openairdocs.org/ad/93-17-12): Main Rotor Transmission Lower Planetary Spider · Bell Helicopter Textron 204B, 205A, 205A-1 and 3 more. Effective Jul 29, 1994
- [AD 92-23-01](https://openairdocs.org/ad/92-23-01): Main Rotor Pillow Blocks · Bell Helicopter Textron 204B, 205A, 205A-1 and 10 more. Effective Apr 23, 1993
- [AD 92-13-10](https://openairdocs.org/ad/92-13-10): Tail Rotor Driveshaft Hanger Bearing · Bell Helicopter Textron 204B, 205A, 205A-1 and 3 more. Effective Feb 23, 1993
- [AD 92-09-05](https://openairdocs.org/ad/92-09-05): Torque Adapter · Bell Helicopter Textron 212 and 412. Effective Jun 2, 1992
- [AD 92-07-08](https://openairdocs.org/ad/92-07-08): Swashplate Support Assembly · Bell Helicopter Textron 204B, 205A, 205A-1 and 2 more. Effective Mar 25, 1992
- [AD 90-26-11](https://openairdocs.org/ad/90-26-11): Drag Brace Assemblies · Bell Helicopter Textron 212. Effective Jan 18, 1991
- [AD 90-03-09](https://openairdocs.org/ad/90-03-09): T/R Hub Assembly  (See 90-03-09) · Bell Helicopter Textron 205A, 205A-1, 212 and 1 more. Effective Feb 13, 1990
- [AD 89-08-05](https://openairdocs.org/ad/89-08-05): Transmission Internal Sump Oil Filter · Bell Helicopter Textron 204B, 205A, 205A-1 and 2 more. Effective Jan 3, 1990
- [AD 81-10-07](https://openairdocs.org/ad/81-10-07): Swashplate Support · Bell Helicopter Textron 212. Effective May 14, 1981
- [AD 80-21-05](https://openairdocs.org/ad/80-21-05): Landing Gear Cross Tubes · Bell Helicopter Textron 205A-1 and 212. Effective Oct 15, 1980
- [AD 79-05-08](https://openairdocs.org/ad/79-05-08): Emergency Flotation (Ditching) Equipment · Bell Helicopter Textron 212. Effective Apr 16, 1979
- [AD 78-17-03](https://openairdocs.org/ad/78-17-03): Spiral Bevel Gear · Bell Helicopter Textron 212. Effective Nov 22, 1978
- [AD 78-20-07](https://openairdocs.org/ad/78-20-07): Shoulder Radius Fitting · Bell Helicopter Textron 204B, 205A-1 and 212. Effective Oct 25, 1978

### Matched by engine (Pratt & Whitney PT6 series)

- [AD 2024-04-51](https://openairdocs.org/ad/2024-04-51): Turbine Section · Pratt & Whitney Canada PT6A-64, PT6A-66, PT6A-66A and 17 more. Effective Mar 28, 2024
- [AD 2023-03-02](https://openairdocs.org/ad/2023-03-02): Turbine Engine Compressor Section · Pratt & Whitney Canada PT6E-67XP. Effective Mar 21, 2023
- [AD 2022-08-13](https://openairdocs.org/ad/2022-08-13): Turbine Section · Pratt & Whitney Canada PT6A-34, PT6A-34B, PT6A-34AG and 2 more. Effective May 27, 2022
- [AD 2020-18-05](https://openairdocs.org/ad/2020-18-05): Fuel Control/Turbine Engines · Pratt & Whitney Canada PT6B-37A. Effective Oct 7, 2020
- [AD 2019-22-03](https://openairdocs.org/ad/2019-22-03): Turbine Engine Reduction Gear · Pratt & Whitney Canada PT6B-37A. Effective Dec 24, 2019
- [AD 2016-05-13](https://openairdocs.org/ad/2016-05-13): Corrosion and perforation of the two-ply Cu-Be bellows in Woodward FCUs. · Pratt & Whitney Canada PT6A-60AG, PT6A-65AG, PT6A-67AF and 1 more. Effective Apr 22, 2016
- [AD 2014-17-08 R1](https://openairdocs.org/ad/2014-17-08-R1): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Jun 5, 2015
- [AD 2014-11-05](https://openairdocs.org/ad/2014-11-05): Reinforcement liner to the power turbine (PT) containment   
  ring and, for certain PT containment rings, adding scallops · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 18 more. Effective Aug 5, 2014
- [AD 2013-03-14](https://openairdocs.org/ad/2013-03-14): Power turbine (PT) baffle · Pratt & Whitney Canada PT6C-67C. Effective Mar 26, 2013
- [AD 2012-09-10](https://openairdocs.org/ad/2012-09-10): First stage sun gears · Pratt & Whitney Canada PT6A-110, PT6A-112, PT6A-114 and 12 more. Effective May 23, 2012
- [AD 2011-25-12](https://openairdocs.org/ad/2011-25-12): Sun gear · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 4 more. Effective Dec 28, 2011
- [AD 2011-20-51](https://openairdocs.org/ad/2011-20-51): Gears · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 4 more. Effective Nov 1, 2011
- [AD 2004-25-18](https://openairdocs.org/ad/2004-25-18): Propeller governor assemblies · Pratt & Whitney Canada PT6A-60A and PT6A-65B. Effective Jan 18, 2005
- [AD 2004-20-04](https://openairdocs.org/ad/2004-20-04): Compressor rear hubs · Pratt & Whitney Canada PT6B-36A and PT6B-36B. Effective Oct 18, 2004
- [AD 2002-23-13](https://openairdocs.org/ad/2002-23-13): Turbine Exhaust Ducts · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 20 more. Effective Dec 31, 2002
- [AD 2001-20-01](https://openairdocs.org/ad/2001-20-01): Compressor Bleed Valve Assembly · Pratt & Whitney Canada PT6A-114A and PT6A-25C. Effective Nov 5, 2001
- [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997
- [AD 95-13-08](https://openairdocs.org/ad/95-13-08): Compressor Turbine Disk · Pratt & Whitney Canada PT6A-67D. Effective Jul 12, 1995
- [AD 93-23-06](https://openairdocs.org/ad/93-23-06): Airframe Chip Detector Flag System · Pratt & Whitney Canada PT6A-50. Effective Jan 26, 1994
- [AD 92-15-11](https://openairdocs.org/ad/92-15-11): Compressor Delivery Air Line (P3) Filter Assembly · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-21 and 7 more. Effective Aug 17, 1992
- [AD 90-12-05](https://openairdocs.org/ad/90-12-05): Engine Overhaul · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 3 more. Effective May 30, 1990
- [AD 88-03-01](https://openairdocs.org/ad/88-03-01): Compressor Stator Assembly · Pratt & Whitney Canada PT6B-36A. Effective Nov 29, 1988
- [AD 86-10-05](https://openairdocs.org/ad/86-10-05): First Stage Compressor Hub · Pratt & Whitney Canada PT6A-42. Effective Jun 5, 1986
- [AD 80-08-12](https://openairdocs.org/ad/80-08-12): Fuel Pump Drive Coupling Splines · Pratt & Whitney Canada PT6A-11, PT6A-112, PT6A-135 and 24 more. Effective Apr 18, 1980
- [AD 80-04-02](https://openairdocs.org/ad/80-04-02): Push-Pull Control Terminal · Pratt & Whitney Canada PT6A-20, PT6A-6A, PT6A-6B and 1 more. Effective Feb 8, 1980
- [AD 79-11-03](https://openairdocs.org/ad/79-11-03): Automatic Fuel Control · Pratt & Whitney Canada PT6T-3 and PT6T-6. Effective May 31, 1979
- [AD 78-17-07](https://openairdocs.org/ad/78-17-07): Fuel Control Unit · Pratt & Whitney Canada PT6A-38, PT6A-41 and PT6A-45A. Effective Aug 31, 1978
- [AD 78-17-05](https://openairdocs.org/ad/78-17-05): Automatic Fuel Control Unit · Pratt & Whitney Canada PT6T-3, PT6T-3A and PT6T-6. Effective Aug 31, 1978
- [AD 78-12-04](https://openairdocs.org/ad/78-12-04): No. 2 Bearing Pressure Oil Transfer Tube Assembly · Pratt & Whitney Canada PT6A-38, PT6A-41 and PT6A-45A. Effective Jun 19, 1978
- [AD 75-06-01](https://openairdocs.org/ad/75-06-01): Gearbox Deterioration · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-20B and 11 more. Effective Apr 1, 1977
- [AD 76-02-08](https://openairdocs.org/ad/76-02-08): Fuel Pump · Pratt & Whitney Canada PT6T-3, PT6T-3A and PT6T-6. Effective Feb 5, 1976
- [AD 75-11-04](https://openairdocs.org/ad/75-11-04): Reduction Gearbox Engine Distress · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-20B and 8 more. Effective May 20, 1975
- [AD 70-16-01](https://openairdocs.org/ad/70-16-01): Turbo Propeller Governors · Pratt & Whitney Canada PT6A-11, PT6A-11AG, PT6A-15AG and 5 more. Effective Aug 4, 1970
- [AD 69-23-06](https://openairdocs.org/ad/69-23-06): Fuel Pumps · Pratt & Whitney Canada PT6A-20, PT6A-27, PT6A-28 and 4 more. Effective Nov 15, 1969
- [AD 68-05-03](https://openairdocs.org/ad/68-05-03): Reverse Mode · Pratt & Whitney Canada PT6A-20 and PT6A-6B. Effective Feb 28, 1968

### Historical (superseded or no longer in force)

- [AD 2022-02-02](https://openairdocs.org/ad/2022-02-02) (historical): Main Rotor System · Bell Textron 204B, 205A, 205A-1 and 3 more. Effective Feb 16, 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 2021-15-51](https://openairdocs.org/ad/2021-15-51) (historical): Main rotor system · Bell Textron 204B, 205A, 205A-1 and 2 more. Effective Aug 24, 2021
- [AD 2018-17-01](https://openairdocs.org/ad/2018-17-01) (historical): Engine Oil System and Aircraft Fuel System · Bell Helicopter Textron 212, 412, 412CF and 1 more. Effective Sep 5, 2018
- [AD 2017-15-02](https://openairdocs.org/ad/2017-15-02) (historical): Engine Oil System and Aircraft Fuel System · Bell Helicopter Textron 212 and 412. Effective Aug 4, 2017
- [AD 2011-12-08](https://openairdocs.org/ad/2011-12-08) (historical): Tail rotor (T/R) blades · Bell Helicopter Textron 205A, 205A-1, 205B and 4 more. Effective Jul 5, 2011
- [AD 2011-08-01](https://openairdocs.org/ad/2011-08-01) (historical): Main rotor hub · Bell Helicopter Textron 212. Effective Apr 21, 2011
- [AD 2010-25-51](https://openairdocs.org/ad/2010-25-51) (historical): Main Rotor Hub · Bell Helicopter Textron 212
- [AD 2010-24-52](https://openairdocs.org/ad/2010-24-52) (historical): Cracked fitting · Bell Helicopter Textron 212
- [AD 2010-24-51](https://openairdocs.org/ad/2010-24-51) (historical): Cracked fitting · Bell Helicopter Textron 212
- [AD 2010-03-03](https://openairdocs.org/ad/2010-03-03) (historical): Main rotor blade · Bell Helicopter Textron 205B and 212. Effective Feb 19, 2010
- [AD 2008-10-03](https://openairdocs.org/ad/2008-10-03) (historical): Tail rotor blade assembly · Bell Helicopter Textron 204B, 205A, 205A-1 and 6 more. Effective May 21, 2008
- [AD 2007-19-53](https://openairdocs.org/ad/2007-19-53) (historical): Tail rotor blade (blade) · Bell Helicopter Textron 204B, 205A, 205A-1 and 6 more. Effective Dec 5, 2007
- [AD 2003-01-04](https://openairdocs.org/ad/2003-01-04) (historical): Main rotor grip · New rotor blades (Hillsboro STC SH5132NM). Effective Jan 30, 2003
- [AD 2002-09-04](https://openairdocs.org/ad/2002-09-04) (historical): Tip Block and Tip Closure · Bell Helicopter Textron 205A, 205A-1, 205B and 4 more. Effective Jun 7, 2002
- [AD 2000-25-03](https://openairdocs.org/ad/2000-25-03) (historical): Main Rotor Actuator Locking Washer · Bell Helicopter Textron 205A-1, 205B, 212 and 2 more. Effective Dec 28, 2000
- [AD 2000-08-52](https://openairdocs.org/ad/2000-08-52) (historical): Main Rotor System · Bell Helicopter Textron 204B, 205A, 205A-1 and 2 more
- [AD 98-24-15](https://openairdocs.org/ad/98-24-15) (historical): Main Rotor Mast and Trunnion · Bell Helicopter Textron 204B, 205A, 205A-1 and 2 more. Effective Dec 8, 1998
- [AD 93-05-01](https://openairdocs.org/ad/93-05-01) (historical): Main Rotor Yoke Assembly · Bell Helicopter Textron 212. Effective Apr 19, 1993
- [AD 81-19-01](https://openairdocs.org/ad/81-19-01) (historical): Main Rotor Yoke · Bell Helicopter Textron 212. Effective Sep 30, 1981
- [AD 80-17-09](https://openairdocs.org/ad/80-17-09) (historical): Main Rotor Straps · Bell Helicopter Textron 204B, 205A-1, 212 and 16 more. Effective Sep 15, 1980
- [AD 79-20-05](https://openairdocs.org/ad/79-20-05) (historical): Main Rotor Hub Assembly · Bell Helicopter Textron 204B, 205A-1 and 212. Effective Jan 18, 1980
- [AD 75-26-05](https://openairdocs.org/ad/75-26-05) (historical): Main Rotor Blades · Bell Helicopter Textron 204B, 205A-1 and 212. Effective Jan 19, 1976
- [AD 74-08-03](https://openairdocs.org/ad/74-08-03) (historical): Tail Fin Forward Spar Cap Angle · Bell Helicopter Textron 212. Effective May 6, 1974
- [AD 2015-20-04](https://openairdocs.org/ad/2015-20-04) (historical): Reduction gearbox (RGB) assembly · Pratt & Whitney Canada PT6B-37A. Effective Nov 18, 2015
- [AD 2014-17-08](https://openairdocs.org/ad/2014-17-08) (historical): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Oct 8, 2014
- [AD 88-24-02](https://openairdocs.org/ad/88-24-02) (historical): Airframe Chip Detector Flag System · Pratt & Whitney Canada PT6A-50

All 126: https://openairdocs.org/aircraft/N1079U/ads.md

## Information bulletins (advisory) (10 in force)

- [SAIB SW-12-38](https://openairdocs.org/saib/SW-12-38): Emergency Push Out  Window Retention. Issued Jul 30, 2012
- [SAIB SW-08-42](https://openairdocs.org/saib/SW-08-42): Emergency Float with Liferaft Kits (kits). Issued Aug 27, 2008
- [SAIB SW-05-79](https://openairdocs.org/saib/SW-05-79): . Issued Aug 8, 2005
- [SAIB SW-05-47](https://openairdocs.org/saib/SW-05-47): . Issued Apr 5, 2005
- [SAIB SW-05-10R1](https://openairdocs.org/saib/SW-05-10R1): . Issued Nov 30, 2004
- [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015
- [SAIB NE-12-04](https://openairdocs.org/saib/NE-12-04): Turbine/ Turboprop Engine: Reduction Gearbox. Issued Nov 1, 2011
- [SAIB NE-10-47](https://openairdocs.org/saib/NE-10-47): Turbine Engine Compressor Section. Issued Aug 30, 2010
- [SAIB NE-06-34](https://openairdocs.org/saib/NE-06-34): . Issued Mar 21, 2006
- [SAIB CE-03-24](https://openairdocs.org/saib/CE-03-24): . Issued Feb 19, 2003
- [SAIB SW-05-10](https://openairdocs.org/saib/SW-05-10) (historical): . Issued Nov 5, 2004

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ANC03GA023](https://openairdocs.org/ntsb/ANC03GA023), Jan 17, 2003: Bell 212 (N1079U), McMurdo Station, AY, substantial damage. Probable cause: The pilot's continued operation of the helicopter with an unstable external load, which resulted in damage to the cargo hook assembly, adjacent throttle controls, and subsequent loss of engine power,…

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20030116000359A](https://openairdocs.org/incident/20030116000359A), Jan 16, 2003: Bell 212 (N1079U), Lakefryxell, AY, Substantial damage. (-23) Witnesses reported that the helicopter was hovering (approx 100' AGL) during an external load operation when "white smoke" was seen emanating from the…

## Service difficulty reports (59, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR HEEA079750](https://openairdocs.org/sdr/HEEA079750), May 31, 2002: CONTROL HEAD. MALFUNCTIONED. CONTROL HEAD WILL NOT RECEIVE ON 120.5 MHZ. FOUND BAD CR3 DIODE. BENCH CHECK GOOD.
- [SDR HEEA076256](https://openairdocs.org/sdr/HEEA076256), Oct 9, 2001: ENGINE. CORRODED. CORROSION AT 12 OCLOCK. SENT TO PRATT AND WHITNEY FOR INSPECTION AND REPAIR.
- [SDR HEEA062805](https://openairdocs.org/sdr/HEEA062805), Jul 12, 1999: GPS RECEIVER. FAILED. GPS RECEIVER FAILED ON SHORT FINAL.
- [SDR HEEA061685](https://openairdocs.org/sdr/HEEA061685), Apr 5, 1999: COMPENSATOR. MALFUNCTIONED. TRIM COMPENSATOR TURNED TO 100 DEGREES AND WILL NOT DROP TEMPS. WITHIN RANGE.
- [SDR HEEA060723](https://openairdocs.org/sdr/HEEA060723), Feb 22, 1999: GYRO. INOPERATIVE. RATE GYRO TURN NEEDLE INOPERATIVE.
- [SDR HEEA060124](https://openairdocs.org/sdr/HEEA060124), Jan 21, 1999: PUMP. MALFUNCTIONED. LOW FUEL PRESSURE.
- [SDR HEEA0016488](https://openairdocs.org/sdr/HEEA0016488), Oct 27, 1998: INVERTER. INOPERATIVE. INVERTER INOPERATIVE.
- [SDR HEEA0016415](https://openairdocs.org/sdr/HEEA0016415), Oct 23, 1998: TRIM COMPENSATOR. INACCURATE. TRIM COMPENSATOR ADJUSTED TO 100. WILL NOT LOWER TEMP INDICATION TO WITHIN RANGE.
- [SDR HEEA0016410](https://openairdocs.org/sdr/HEEA0016410), Oct 23, 1998: GENERATOR. FAILED. STARTER/GENERATOR WILL NOT COME ON-LINE.
- [SDR HEEA0016397](https://openairdocs.org/sdr/HEEA0016397), Oct 23, 1998: INVERTER. MALFUNCTIONED. INVERTER HAS LOW VOLTAGE OUTPUT.
- [SDR 99ZZZX681](https://openairdocs.org/sdr/99ZZZX681), Jul 30, 1998: FUEL CONTROL. MALFUNCTIONED. WHILE IN CRUISE FLIGHT, NR 1 ENGINE TORQUE WENT LOW WHICH RESULTED IN A 20 PERCENT TORQUE SPLIT BETWEEN NR 1 AND NR 2 ENGINES. PILOT RETURNED TO BASE AND LANDED
- [SDR HEEA0015375](https://openairdocs.org/sdr/HEEA0015375), Jul 29, 1998: COMPENSATOR. MALFUNCTIONED. TRIM COMPENSATOR WILL NOT BRING TEMPERATURE ANY LOWER THAN 75 CHANGE.
- [SDR HEEA0015137](https://openairdocs.org/sdr/HEEA0015137), Jul 1, 1998: INDICATOR. INOPERATIVE. ALTIMETER INDICATOR INDICATED 150 FEET AT 1,000 AND 2,000 FEET. INOPERATIVE.
- [SDR HEEA0014846](https://openairdocs.org/sdr/HEEA0014846), Jun 22, 1998: INDICATOR. MALFUNCTIONED. COURSE DIGITIZER OUT OF ALIGNMENT.
- [SDR HEEA0014589](https://openairdocs.org/sdr/HEEA0014589), Jun 4, 1998: ALTIMETER. FAILED. ALTIMETER FAILED FRICTION ERROR TEST.
- [SDR HEEA0014578](https://openairdocs.org/sdr/HEEA0014578), Jun 4, 1998: DUAL AMMETER. STICKS. DUAL AMMETER NR 2 NEEDLE IS STICKING.
- [SDR HEEA0014502](https://openairdocs.org/sdr/HEEA0014502), Jun 4, 1998: TRANSMITTER. FAILED. TORQUEMETER READS LOW, OUT OF TOLERANCE.
- [SDR HEEA0013700](https://openairdocs.org/sdr/HEEA0013700), Apr 2, 1998: BEACON. WEAK. BEACON IS WEAK.
- [SDR HEEA0013681](https://openairdocs.org/sdr/HEEA0013681), Apr 2, 1998: INDICATOR. STUCK. INDICATOR NEEDLE STUCK AT ZERO.
- [SDR HEEA0013596](https://openairdocs.org/sdr/HEEA0013596), Mar 26, 1998: INDICATOR. FAILED. NR 2 NEEDLE READING HIGH.
- [SDR HEEA0013325](https://openairdocs.org/sdr/HEEA0013325), Mar 5, 1998: EPIRB. DEFECTIVE. EPIRB CASE IS SWOLLEN. CORROSION IN ANTENNA MOUNT.
- [SDR HEEA0012485](https://openairdocs.org/sdr/HEEA0012485), Jan 6, 1998: EPIRB. DEFECTIVE. EPIRB ANTENNA BROKEN AND BODY CRACKS IN BOTTOM.
- [SDR HEEA0011722](https://openairdocs.org/sdr/HEEA0011722), Oct 22, 1997: BEARING. WORN. M/R DAMPER BEARINGS WORN.
- [SDR HEEA0011452](https://openairdocs.org/sdr/HEEA0011452), Oct 10, 1997: TACH GENERATOR. SHAFT WORN. ROTOR TACH GEN SHAFT WORN.
- [SDR HEEA0011365](https://openairdocs.org/sdr/HEEA0011365), Oct 9, 1997: INDICATOR. FAILED. NR1 NEEDLE DOES NOT INDICATE.
- [SDR HEEA0011264](https://openairdocs.org/sdr/HEEA0011264), Oct 8, 1997: LINER ASSY. BURNT. COMBUSTION LINER ASSY BURNT LOUVERS.
- [SDR HEEA0011247](https://openairdocs.org/sdr/HEEA0011247), Oct 7, 1997: CVR. WONT TEST. CVR WILL NOT TEST.
- [SDR HEEA0011116](https://openairdocs.org/sdr/HEEA0011116), Sep 30, 1997: VANE RING ASSY. CRACKED. VANE RING ASSY CRACKED BEYOND LIMITS.
- [SDR HEEA0011102](https://openairdocs.org/sdr/HEEA0011102), Sep 30, 1997: HARNESS. FAILED. HARNESS BURNT PROBE TIP.
- [SDR HEEA0010356](https://openairdocs.org/sdr/HEEA0010356), Jun 26, 1997: CVR. MALFUNCTION. CVR HAS EXCESSIVE NOISE ON TAPE.
- [SDR HEEA0010082](https://openairdocs.org/sdr/HEEA0010082), Jun 11, 1997: RADAR ALTIMETER. DEFECTIVE. DH BUG WILL NOT GO PAST 1800 FEET AND FLAG WILL NOT PULL. ALSO NEEDLE IS OFF 20 FEET.
- [SDR HAIHEEA9598](https://openairdocs.org/sdr/HAIHEEA9598), Apr 24, 1997: INDICATOR. PRECESSES. PRECESSES 5 PERCENT RIGHT AND 5 PERCENT NOSE UP IN 10 MINUTES OF FLIGHT.
- [SDR HAIHEEA9300](https://openairdocs.org/sdr/HAIHEEA9300), Apr 1, 1997: INDICATOR. READS HIGH. PRESSURE SIDE READS HIGH. TEMP SIDE HAS EXCESSIVE FRICTION ERROR.
- [SDR HEEA979205](https://openairdocs.org/sdr/HEEA979205), Mar 12, 1997: ENCODER. STICKS. INCONSISTENT OUTPUT AND NEEDLE INTERMITTENTLY STICKS. TIME SINCE REPAIR 1008:55.
- [SDR HEEA978993](https://openairdocs.org/sdr/HEEA978993), Feb 10, 1997: FUEL PROBE. FAILED. FUEL PROBE READS HIGH OUT OF TOLERANCE.
- [SDR HEEA968637](https://openairdocs.org/sdr/HEEA968637), Dec 10, 1996: DAMPER ASSY. LEAKING. DAMPER LEAKING OIL.
- [SDR HEEA968452](https://openairdocs.org/sdr/HEEA968452), Nov 6, 1996: INDICATOR. DEFECTIVE. HSI INDICATOR COURSE SELECT KNOB HARD TO TURN. TIME SINCE REPAIR 237:35.
- [SDR HEEA968071](https://openairdocs.org/sdr/HEEA968071), Oct 3, 1996: SHAFT. CORRODED. SHAFT IS CORRODED.( FOUND EXCESSIVE CORROSION IN SPLINES "N" (REF. BHT 412 CR&0 SEC. 65-00-00 PAGE 133 FIG. 65-40) BEYOND LIMITS. REPLACED WTH SERVICEABLE SHAFT
- [SDR HEEA968027](https://openairdocs.org/sdr/HEEA968027), Oct 3, 1996: INDICATOR. INTERMITTENT. #1 NEEDLE HAS INTERMITTENT OPERATION.
- [SDR HEEA967770](https://openairdocs.org/sdr/HEEA967770), Sep 3, 1996: INDICATOR. FAILED. TORQUEMETER #1 NEEDLE HAS NO INDICATION.
- [SDR HEEA967257](https://openairdocs.org/sdr/HEEA967257), May 22, 1996: TRANSCEIVER. MIS WIRED. HUM ON LINE AND AUDIO CUTS OUT WHEN POWER SUPPLY IS DECREASED BELOW +280. FOUND THE INPUT AND OUTPUT OF U2 WAS WIRED WRONG. REWIRED U2 CORRECTLY AND UNIT MEETS 
- [SDR HEEA966998](https://openairdocs.org/sdr/HEEA966998), Apr 15, 1996: DAMPER ASSY. DEFECTIVE. FLUID CONTAMINATION AND GLASS IS UNREADABLE.
- [SDR HEEA966997](https://openairdocs.org/sdr/HEEA966997), Apr 15, 1996: DAMPER ASSY. DEFECTIVE. FLUID CONTAMINATION AND GLASS IS UNREADABLE.
- [SDR HEEA966920](https://openairdocs.org/sdr/HEEA966920), Apr 4, 1996: INDICATOR. DEFECTIVE. UNIT HAD BROKEN "MAP" SWITCH, REPLACED SWITCH WITH SPARE. REPAIRED.TROUBLESHOT UNIT FURTHER AND FOUND VIDEO BOARD TO BE INTERMITTENT AND LOGIC #2BOARD BAD. CAUS
- [SDR HEEA966636](https://openairdocs.org/sdr/HEEA966636), Feb 5, 1996: CONTROL UNIT. DEFECTIVE. CONTROL UNIT DEFECTIVE. GENERATOR WOULD NOT COME ON LINE.
- [SDR HEEA966634](https://openairdocs.org/sdr/HEEA966634), Feb 5, 1996: CONTROL UNIT. DEFECTIVE. #2 GENERATOR KICKS OFF LINE WHEN ANY INVERTER IS TURNED ON.
- [SDR HEEA956256](https://openairdocs.org/sdr/HEEA956256), Dec 13, 1995: GEAR ASSY. WORN. WORN SEAL RIDE AREA.
- [SDR HEEA956123](https://openairdocs.org/sdr/HEEA956123), Nov 22, 1995: TRANSCEIVER. DEFECTIVE. TRANSMIT BREAKS UP.
- [SDR HEEA955976](https://openairdocs.org/sdr/HEEA955976), Nov 8, 1995: INDICATOR. WONT TEST. WILL NOT TEST. INOPERATIVE.
- [SDR HEEA955846](https://openairdocs.org/sdr/HEEA955846), Oct 5, 1995: CONTROL UNIT. DEFECTIVE. INSPECT FOR CORROSION. INSPECTED CONTROL UNIT, BUT FOUND NO CORROSION. HOWEVER, FOUND THUMBWHEEL TO BE INTERMITTENTLY DIALING UP WRONG FREQUENCIES. REPLACED 1 E

All 59: https://openairdocs.org/aircraft/N1079U/reports.md

## STCs that may be installed (OpenAirDocs) (414, 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 (Bell 212)

- [STC SR12508IB](https://openairdocs.org/stc/SR12508IB): Installation of Personnel Carrying Devices (PCDs) for Human External Cargo (HEC). Ascent Aerospace Ltd
- [STC SR12427IB](https://openairdocs.org/stc/SR12427IB): Installation of an AEM MTP136D Panel Mount FM Transceiver. Anodyne Electronics Manufacturing Corporation
- [STC SR02736NY](https://openairdocs.org/stc/SR02736NY): Installation of Utility Basket on the right hand side. Alpine Aerotech Ltd
- [STC SR02270SE](https://openairdocs.org/stc/SR02270SE): Fabrication and installation of Geneva Aviation Audio System. AEM USA Inc
- [STC SR02444SE](https://openairdocs.org/stc/SR02444SE): Installation of P178 Failsafe Audio Mixer. AEM USA Inc
- [STC SR12332SE](https://openairdocs.org/stc/SR12332SE): Installation of Mechanical Specialties, LLC Human External Cargo (HEC) and non-HEC Hook System. Mechanical Specialties, LLC
- [STC SH3261SO](https://openairdocs.org/stc/SH3261SO): Installation of replacement skid tubes. Bell Helicopter Textron Inc
- [STC SR04465NY](https://openairdocs.org/stc/SR04465NY): Installation of the iPad Mount. Avio Design Group Inc
- [STC SR09922AC](https://openairdocs.org/stc/SR09922AC): Installation of a Foresight MX Condition Monitoring System. GPMS International Inc
- [STC SR12068IB](https://openairdocs.org/stc/SR12068IB): Installation of the AFI4700 Electronic Flight Instrument. Alpine Aerotech LP
- [STC SR12072IB](https://openairdocs.org/stc/SR12072IB): Manufacturing and Installation of Cargo Hold Nets; Maintenance must be in accordance with ICARUS Aero Inc. Instructions for Continued Airworthiness as shown on the attached FAA AML No. SR12072IB. Icarus Aero Inc
- [STC SR11922AC](https://openairdocs.org/stc/SR11922AC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc
- [STC SH8610SW](https://openairdocs.org/stc/SH8610SW): Fabrication of Isolair Eliminator II Model 4600-212/412 Fire Fighting System. Isolair Inc
- [STC SR02590AK](https://openairdocs.org/stc/SR02590AK): Installation of Bell Lightweight Tailboom Modification. StandardAero Atlantic USA Inc
- [STC SR00855DE](https://openairdocs.org/stc/SR00855DE): Installation of Tracking Patient Loading System. Air Methods LLC
- [STC SR04132CH](https://openairdocs.org/stc/SR04132CH): Installation of Heli-Preheat Kit, p/n TA3132-1 for 115 volt application in accordance with Heli-Preheat Kit drawing TA3132-1 Revision G, dated December 11, 2023 or later FAA approved revisions and Preheat Kit Installation Instruction TNH3132 Revision C, dated November 7, 2023 or later FAA approved revisions. HARTZELL PROPELLER LLC
- [STC SH1253SO](https://openairdocs.org/stc/SH1253SO): Installation of a wire strike protection system. Magellan Aerospace
- [STC SR01779LA](https://openairdocs.org/stc/SR01779LA): Installation of the Emergency Float Kits. Dart Aerospace ULC
- [STC SR00169IB](https://openairdocs.org/stc/SR00169IB): Installation of the Garmin G500H TXi Flight Display System. Eagle Copters Maintenance Ltd
- [STC SR09343RC](https://openairdocs.org/stc/SR09343RC): Installation of Aero Seats and Systems, Inc., Life Raft Deployment System (LRDS). Bell Textron Inc
- [STC SR00145IB](https://openairdocs.org/stc/SR00145IB): Installation of LH and RH Vertical Reference Door(s). Transwest Helicopters Ltd
- [STC SR00142IB](https://openairdocs.org/stc/SR00142IB): Installation of the Integrated Health and Usage Monitoring System (HUMS). RMCI Canada Inc
- [STC SR00141IB](https://openairdocs.org/stc/SR00141IB): Installation of the Aft Pedestal Stowage Compartment. Alpine Aerotech LP
- [STC SH4056NM](https://openairdocs.org/stc/SH4056NM): Installation of pneumatic door actuators. Dart Aerospace USA Inc
- [STC SR00131IB](https://openairdocs.org/stc/SR00131IB): Installation of an Artex Emergency Locator Transmitter (ELT) 4000 HM System. Eagle Copters Maintenance Ltd
- [STC SR01865SE](https://openairdocs.org/stc/SR01865SE): Fabrication and installation of FastFin System. BLR Aerospace LLC
- [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 SR00871LA](https://openairdocs.org/stc/SR00871LA): Installation of the Modular Seating System. LifePort LLC
- [STC SR00094IB](https://openairdocs.org/stc/SR00094IB): Installation of Extended Port Seat Rail. Ascent Aerospace Ltd
- [STC SR00080IB](https://openairdocs.org/stc/SR00080IB): Installation of the Garmin GRA 55 Radar Altimeter. Alpine Aerotech LP
- [STC SR00077IB](https://openairdocs.org/stc/SR00077IB): Installation of the Two Place Seat Assembly. Ascent Aerospace Ltd
- [STC SR00075IB](https://openairdocs.org/stc/SR00075IB): Installation of Cabin Furnishings. Ascent Aerospace Ltd
- [STC SH400NW](https://openairdocs.org/stc/SH400NW): Installation of left hand bubble door with or without duplicate engine instruments. WSH, LLC
- [STC SR03832NY](https://openairdocs.org/stc/SR03832NY): Installation of Full Vertical Reference Door P/N D412-761 for Left Hand Vertical Reference Operations. Dart Aerospace Limited
- [STC SR04782NY](https://openairdocs.org/stc/SR04782NY): Installation of PCDs and HEC System. Ascent Aerospace Ltd
- [STC SR00058IB](https://openairdocs.org/stc/SR00058IB): Installation of J301A Audio Controller. Alpine Aerotech LP
- [STC SR00047IB](https://openairdocs.org/stc/SR00047IB): Installation of VIH Aerospace (VIHA) Pulse Light. VIH Aerospace Inc
- [STC SR00035IB](https://openairdocs.org/stc/SR00035IB): Installation of the Garmin GTS 8xx Traffic System. Alpine Aerotech LP
- [STC SR04615NY](https://openairdocs.org/stc/SR04615NY): Installation of the Human External Cargo (HEC) Suspension Line Kit. Boost Human External Cargo Systems Inc
- [STC SR04616NY](https://openairdocs.org/stc/SR04616NY): Installation of the Dual HEC Hook System Provisions is to be performed. Boost Human External Cargo Systems Inc
- [STC SR01124LA](https://openairdocs.org/stc/SR01124LA): Installation of Pratt & Whitney PT6T-3DE, or -3DF Twin-Pac in place of PT6T-3 or PT6T-3B Twin-Pac. ASCENT POWER INC
- [STC SR00713SE](https://openairdocs.org/stc/SR00713SE): Installation of Onboard Systems International Cargo Hook Kit. Onboard Systems International
- [STC SR01634SE](https://openairdocs.org/stc/SR01634SE): Installation of a Supplemental Lighting System. Aviation Specialties Unlimited Inc
- [STC SR01903NY](https://openairdocs.org/stc/SR01903NY): Installation of a modified co-pilot seat. Transwest Helicopters Ltd
- [STC SR04663NY](https://openairdocs.org/stc/SR04663NY): Installation of the Center Pedestal Riser. Alpine Aerotech LP
- [STC SH5707NM](https://openairdocs.org/stc/SH5707NM): Fabrication of Onboard Systems Model 200-088-03 or 200-088-04 (without Load Weight) or 200-089-03, -04, -05 or -06 (with Load Weight) cargo hook suspension systems. Onboard Systems International
- [STC SH5737NM](https://openairdocs.org/stc/SH5737NM): Replacement of Bell magnesium cargo hook bumper and ring Part Nos. 204-072-901-1 or -3, and 204-072-905-3, respectively, with Onboard bumper ring kit No. 210-092-00. Fabrication of Onboard Systems Model 210-092-00 bumper ring kit. Onboard Systems International
- [STC SH5758NM](https://openairdocs.org/stc/SH5758NM): Fabrication of the Onboard Model 200-095-00 Multi-Channel Electrical Slip-Ring Kit. Onboard Systems International
- [STC SR00277SE](https://openairdocs.org/stc/SR00277SE): Fabrication of Onboard Systems Model 528-002-00 or 528-002-01 cargo hook. Onboard Systems International LLC
- [STC SR00699SE](https://openairdocs.org/stc/SR00699SE): Fabrication of Onboard Systems Model 200-246-00 cargo hook kit. Onboard Systems International

All 414: https://openairdocs.org/aircraft/N1079U/stcs.md

## Earlier aircraft with N1079U

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N1079U before.

- [Cancelled 1973-06-04](https://openairdocs.org/deregistered/N1079U-1973-06-04): Piper PA-34-200, S/N 34-7250082. Exported to Canada. Owner: [Wiggins Airways Inc](https://openairdocs.org/faa-owner/WIGGINS%20AIRWAYS%20INC), [Alton, NH](https://openairdocs.org/faa-place/NH/Alton)

## Related

- Other Bell 212 aircraft: https://openairdocs.org/model/bell-212/aircraft.md
- The Pratt & Whitney PT6 series engine: https://openairdocs.org/engine/pratt-whitney-pt6-series.md

---
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