- Registered owner
- Bighorn Airways Inc
- Location
- Sheridan, WY
- Owner type
- Corporation
- Serial number
- 165
- Year built
- 1979
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Restricted, forest, other
- Airworthiness date
- May 3, 1996
- Certificate issued
- April 20, 1989
- Expires
- June 30, 2027
- Mode S code
- A01ED6
Construcciones Aeronauticas C-212-CCTCDS A43EUAirframe · Construcciones Aeronauticas C-212-CCEngine modelAiResearch TPE331 series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every AiResearch TPE331 model are included below.
On this page
Airworthiness directives that may apply · 85
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 1 |
|---|---|
| 1974 | 2 |
| 1975 | 2 |
| 1976 | 1 |
| 1979 | 2 |
| 1980 | 2 |
| 1983 | 1 |
| 1984 | 4 |
| 1986 | 1 |
| 1987 | 8 |
| 1988 | 2 |
| 1989 | 7 |
| 1991 | 1 |
| 1992 | 1 |
| 1993 | 4 |
| 1994 | 1 |
| 1995 | 2 |
| 1996 | 3 |
| 1997 | 3 |
| 1998 | 7 |
| 1999 | 2 |
| 2001 | 1 |
| 2002 | 2 |
| 2003 | 1 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 4 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 3 |
| 2011 | 1 |
| 2012 | 1 |
| 2014 | 1 |
| 2015 | 3 |
| 2016 | 2 |
| 2017 | 2 |
| 2018 | 5 |
| 2020 | 1 |
| 2021 | 1 |
| 2022 | 1 |
Airframe · Construcciones Aeronauticas C-212-CC
AD 2022-17-06FuselageAD 2020-03-18Flight ControlsAD 2018-19-02Flight controlsInformation bulletins that may apply · 4
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N107BHMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Construcciones Aeronauticas C-212-CC aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR BIGA20190821001Line · leakingINITIAL REPORTS WERE OF AN SMOKE IN THE COCKPIT, NOTICED HYDRAULIC FLUID ON THE WINDOWS INTERNALLY AND EXTERNALLY AND HYDRAULIC FLUID FROM THE RADOME TO THE RAMP DOOR DRIPPING OFF THE BELLY. HYDRAULIC FLUID SEEMED TO BE CONCENTRATED ON THE RIGHT (CO-PILOT) SDR BIGA20190721001Engine · malfunctionedRIGHT ENGINE SURGED, UP TO 100% AND COULD NOT BE REDUCED. CHIP DETECTOR LIGHT CAME ONE AND OIL PRESSURE WENT TO ZERO. PILOT FOLLOWED EMERGENCY PROCEDURES SHUT DOWN ENGINE AND RETURNED TO THE NEARBY AIRPORT. AFTER LANDING THE ENGINE PROPELLER COULD NOT BE ROSDR BIGA20170821001Line · crackedTHE PILOT REPORTED AN OIL LEAK AND FLUCTUATING OIL PRESSURE ON THE RIGHT ENGINE. MAINTENANCE FOUND THE ENGINE 4 QTS LOW ON OIL, CLEANED ENGINE AND COWLINGS, AND SERVICED ENGINE OIL. THE ENGINE WAS MOTORED AND A THE OIL LEAK WAS LOCATED ON THE .125 INCH STAINSDR BIGA20161206001Mount · crackedA VIBRATION WAS NOTED ON THE RIGHT PROPELLER DURING ENGINE RUN UP DURING MAINTENANCE, PROP DYNAMIC BALANCE WAS FOUND OUT OF LIMITS (2.5 IPS). THE PROPELLER WAS FOUND TO HAVE 3 BLADES SLIP IN THE CLAMPS CAUSING 2 BLADES TO BE OVER 1.5 DEGREES OFF FROM THE RESTSDR BIGA20160531001Tube · misalignedTHE PILOT NOTED A LT ENG OIL PRESS FLUCTUATION, THEN DURING CLIMB TO 2000 FT, THEN THE LOW OIL PRESS LIGHT CAME ON & TORQUE FLUCTUATION OCCURRED. THE PILOT PERFORMED AN INFLIGHT SHUTDOWN & RETURNED. LANDED WITHOUT INCIDENT. PERSONNEL FOUND THE OIL TUBE, PN SDR BIGA20150211001Fuel Control · failedTHE FUEL CONTROL UNIT , FCU, WAS SENT OUT FOR BENCH CHECK & REPAIR DUE TO A SUSPECTED FUEL FLOW PROBLEM. THE FCU WAS BENCH CHECKED & THE PROBLEM COULD IT WAS SLIGHTLY OUT OF RIG THAT MAY HAVE BEEN CAUSING A GOVERNOR INTERFERENCE PROBLEM. IT ALSO HAD THE DRIVSDR BIG2008F00000Pitch Control · malfunctionedON THE LT ENG WITH THE SPEED LEVERS EET AT 100 PERCENT AND YOU TRY TO BRING THE POWER LEVER BACK TO CRUISE, AT ABOUT 70 PERCENT TO 80 PERCENT TORQUE THE RPM DROPS TO 93 PERCENT. TORQUE TEMP AND FUEL FLOW WILL INCREASE TO A HIGHER SETTING ON ITS OWN MAKING CON
STCs that may be installed · 86
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Construcciones Aeronauticas C-212-CC
Earlier aircraft with this N-number · 1
This aircraft carried N107BH before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.