Bell 206 Safety Record
Complete NTSB accident and incident history. 1329 events recorded from 1982 to 2026.
| Date | Location | Reg# | Severity | Damage | Probable Cause |
|---|---|---|---|---|---|
| Apr 15, 1994 | ENGLEWOOD, CO | N937S | Incident | substantial |
THE PILOT'S FAILURE TO MAINTAIN ROTOR RPM, HIS DELAYED FLARE, AND IMPROPER TOUCHDOWN. A FACTOR WAS A FAILURE OF THE FUEL CONTROL/GOVERNOR TO THE HIGH …THE PILOT'S FAILURE TO MAINTAIN ROTOR RPM, HIS DELAYED FLARE, AND IMPROPER TOUCHDOWN. A FACTOR WAS A FAILURE OF THE FUEL CONTROL/GOVERNOR TO THE HIGH SIDE WHICH REQUIRED THE PILOT TO PERFORM A FULL AUTOROTATION. |
| Mar 27, 1994 | BELEN, NM | N2779B | Incident | substantial | THE HARD LANDING DUE TO A DELAYED FLARE AND IMPROPER TOUCHDOWN. A FACTOR WAS THE LOSS OF ENGINE POWER. |
| Feb 27, 1994 | AGUA DULCE, CA | N50PE | Incident | substantial | THE CFI'S SELECTION OF UNSUITABLE TERRAIN TO DEMONSTRATE A SIMULATED AUTOROTATION. THE SOFT TERRAIN WAS A FACTOR IN THIS ACCIDENT. |
| Jan 20, 1994 | CASCADE, CO | N3211K | Incident | substantial | THE PILOT'S IMPROPER IN-FLIGHT PLANNING WHICH RESULTED IN THE AIRCRAFT'S YAW PERFORMANCE BEING EXCEEDED. A FACTOR WAS THE HIGH DENSITY ALTITUDE. |
| Dec 24, 1993 | LAS VEGAS, NV | N162BC | Incident | substantial | the pilot's failure to properly position the helicopter away from the dolly edge during the initial touchdown. |
| Dec 11, 1993 | FLAGSTAFF, AZ | N2773R | Incident | substantial |
The pilot's improper initiation of an emergency autorotation into unsuitable terrain and subsequent hard landing and rollover. A false annunciator in…The pilot's improper initiation of an emergency autorotation into unsuitable terrain and subsequent hard landing and rollover. A false annunciator indication, a failure of the N1 tach generator, the pilot's continued flight with a known aircraft defect, and the pilot's improper identification of the failed N1 gauge were factors in this accident. |
| Oct 29, 1993 | NEW YORK, NY | N16696 | Incident | — |
Inadequate maintenance which resulted in the improper alignment of the 'O' ring on the spur adapter gear drive which caused lack of lubrication and we…Inadequate maintenance which resulted in the improper alignment of the 'O' ring on the spur adapter gear drive which caused lack of lubrication and wear of the gear drive and the disengagement of the compressor and turbine. |
| Oct 29, 1993 | GULF OF MEXICO, | N5370V | Incident | substantial | THE PILOT IN COMMAND'S INADEQUATE PREFLIGHT INSPECTION IN THAT HE FAILED TO REMOVE A TIE DOWN ROPE. A FACTOR WAS THE PILOT'S SELF-INDUCED PRESSURE. |
| Sep 30, 1993 | HURST, TX | N2064J | Incident | substantial |
THE EXCESSIVE FLARE AND THE CONTROL INTERFERENCE BY THE PILOT UNDERGOING INSTRUCTION AND INADEQUATE SUPERVISION BY THE CFI. FACTORS WERE THE PILOT'S F…THE EXCESSIVE FLARE AND THE CONTROL INTERFERENCE BY THE PILOT UNDERGOING INSTRUCTION AND INADEQUATE SUPERVISION BY THE CFI. FACTORS WERE THE PILOT'S FAILURE TO UNDERSTAND THE INSTRUCTOR'S DIRECTIONS DUE TO HIS LIMITED KNOWLEDGE OF THE ENGLISH LANGUAGE. |
| Sep 29, 1993 | WHT SANDS MR, NM | N39049 | Incident | substantial | THE PILOT'S FAILURE TO LAND AN ADEQUATE DISTANCE AWAY FROM THE UNSECURED PARACHUTE. |
| Aug 04, 1993 | PEARLAND, TX | N16814 | Incident | substantial |
PILOT'S FAILURE TO MAINTAIN PROPER ROTOR RPM, THE DELAYED FLARE, AND IMPROPER TOUCHDOWN. FACTORS WERE TOTAL FAILURE OF THE POWER TURBINE DUE TO OIL ST…PILOT'S FAILURE TO MAINTAIN PROPER ROTOR RPM, THE DELAYED FLARE, AND IMPROPER TOUCHDOWN. FACTORS WERE TOTAL FAILURE OF THE POWER TURBINE DUE TO OIL STARVATION TO THE #8 BEARING ASSEMBLY. |
| Jun 17, 1993 | STONEYFORD, CA | N38EA | Incident | substantial |
the pilot's inadequate compensation for the existing wind conditions during a hover operation. A factor in the accident was the high density altitude…the pilot's inadequate compensation for the existing wind conditions during a hover operation. A factor in the accident was the high density altitude and the gusting, variable wind conditions. |
| Jan 24, 1993 | BRIGHAM CITY, UT | N39088 | Incident | substantial |
THE LOCATION OF UNMARKED ELECTRICAL TRANSMISSION WIRES OVER A DESIGNATED AIRPORT TAXIWAY. FACTORS RELATING TO THE ACCIDENT WERE THE PILOT'S LACK OF E…THE LOCATION OF UNMARKED ELECTRICAL TRANSMISSION WIRES OVER A DESIGNATED AIRPORT TAXIWAY. FACTORS RELATING TO THE ACCIDENT WERE THE PILOT'S LACK OF EXPECTANCY TO ENCOUNTER WIRES ABOVE AN ARPT TAXIWAY, AND HIS DIVERTED ATTENTION DUE TO THE CLOSE PROXIMITY OF THE TAXIWAY TO BUILDINGS AND THE LOOSE DRY SNOW ON THE AIRPORT. |
| Nov 10, 1992 | ELF POINT CAMP, AK | N21424 | Incident | substantial | THE PILOT MISJUDGED CLEARANCE AND DRAGGED AN EXTERNAL LOAD LONGLINE CABLE WHILE LANDING. |
| Aug 25, 1992 | FAIRBANKS, AK | N83139 | Incident | substantial |
POOR MAINTENANCE AND INSPECTION PROCEDURES BY THE CONTRACT MAINTENANCE PERSONNEL, AS WELL AS IMPROPER MAINTENANCE AND INSTALLATION OF THE FUEL LINE BY…POOR MAINTENANCE AND INSPECTION PROCEDURES BY THE CONTRACT MAINTENANCE PERSONNEL, AS WELL AS IMPROPER MAINTENANCE AND INSTALLATION OF THE FUEL LINE BY THE CONTRACT MAINTENANCE PERSONNEL. FACTORS RELATING TO THE ACCIDENT WERE THE TURBOSHAFT ENGINE VIBRATIONS AND THE CRACKED FUEL LINE(S). |
| Jun 21, 1992 | PONCA CITY, OK | N66LR | Incident | substantial | THE PILOT'S FAILURE TO MAINTAIN MAIN ROTOR RPM. A FACTOR WAS THE CONTAMINATED FUEL. |
| Apr 01, 1992 | KAAAWA, HI | N3200N | Incident | substantial | AN ENGINE FLAME OUT DUE TO THE PILOT'S INTENTIONAL FLIGHT THROUGH AN IRRIGATION SPRINKLER SYSTEM WATER STREAM IN ORDER TO WASH THE HELICOPTER. |
| Mar 05, 1992 | SABINE PASS #18, | N41791 | Incident | — | THE PILOT'S CARDIOVASCULAR DISEASE. |
| Mar 03, 1992 | FALFURRIAS, TX | N3201R | Incident | substantial |
THE PILOT'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL DUE TO HIS ABILITY TO MAINTAIN AN ADEQUATE VISUAL LOOKOUT BEING RESTRICTED. FACTORS WERE THE OBSE…THE PILOT'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL DUE TO HIS ABILITY TO MAINTAIN AN ADEQUATE VISUAL LOOKOUT BEING RESTRICTED. FACTORS WERE THE OBSERVER'S DELAY IN INFORMING THE PILOT OF THE REARWARD DRIFT AND THE DARK NIGHT CONDITIONS. |
| Mar 02, 1992 | GLENBROOK, NV | N59613 | Incident | substantial | FAILURE OF THE PILOT-IN-COMMAND TO FOLLOW THE HELICOPTER'S PERFORMANCE DATA WHILE TRANSLATING OUT OF TRANSLATIONAL LIFT TO AND OUT OF GROUND EFFECT. |
| Feb 26, 1992 | GRAND ISLE, | N2750F | Incident | substantial | HEAVY SEA STATE DUE TO THE HIGH WINDS. A FACTOR WAS THE POWER LOSS. |
| Feb 15, 1992 | SOUTH PELTO #1, | N3120X | Incident | destroyed |
THE PILOT'S INABILITY TO CONTROL THE HELICOPTER DUE TO SPATIAL DISORIENTATION. FACTORS WERE THE FOG AND THE PILOT'S FAILURE TO RECEIVE A WEATHER BRIEF…THE PILOT'S INABILITY TO CONTROL THE HELICOPTER DUE TO SPATIAL DISORIENTATION. FACTORS WERE THE FOG AND THE PILOT'S FAILURE TO RECEIVE A WEATHER BRIEFING PRIOR TO THE FLIGHT. |
| Dec 12, 1991 | CHARLOTTE, NC | N206CM | Incident | substantial |
THE PILOT IN COMMANDS FAILURE TO MAINTAIN TAILROTOR GROUND CLEARANCE WHILE HOVERING RESULTING IN THE TAIL STRIKING THE GROUND AND THE SUBSEQUENT SEPAR…THE PILOT IN COMMANDS FAILURE TO MAINTAIN TAILROTOR GROUND CLEARANCE WHILE HOVERING RESULTING IN THE TAIL STRIKING THE GROUND AND THE SUBSEQUENT SEPARATION OF THE TAILROTOR AND GEARBOX. |
| Dec 10, 1991 | ARLINGTON, TX | N2770X | Incident | substantial |
THE HELICOPTER'S AUTOROTATIONAL LANDING PERFORMANCE CAPABILITY WAS EXCEEDED. FACTORS WERE THE PROPER DESCENT RATE WAS NOT POSSIBLE FOR THE PIC AND SUF…THE HELICOPTER'S AUTOROTATIONAL LANDING PERFORMANCE CAPABILITY WAS EXCEEDED. FACTORS WERE THE PROPER DESCENT RATE WAS NOT POSSIBLE FOR THE PIC AND SUFFICIENT INFORMATION FROM THE MANUFACTURER WAS NOT PROVIDED. |
| Oct 06, 1991 | HOLLYWOOD, FL | N78CF | Incident | substantial | THE FAILURE OF THE PILOT TO MAINTAIN ROTOR RPM AND THE FAILURE OF THE CFI TO MONITOR THE CONTROLS. |