Cessna T210 Safety Record
Complete NTSB accident and incident history. 792 events recorded from 1982 to 2025.
| Date | Location | Reg# | Severity | Damage | Probable Cause |
|---|---|---|---|---|---|
| Dec 21, 1994 | Kellogg, ID | N4607Q | Incident | substantial |
THE PILOT'S IMPROPER POSITIONING OF THE FUEL SELECTOR VALVE, HIS INADEQUATE REMEDIAL ACTION, AND STARVATION OF FUEL TO THE ENGINE. FACTORS INCLUDE A S…THE PILOT'S IMPROPER POSITIONING OF THE FUEL SELECTOR VALVE, HIS INADEQUATE REMEDIAL ACTION, AND STARVATION OF FUEL TO THE ENGINE. FACTORS INCLUDE A SIGN POST ALONGSIDE THE ROAD ON WHICH THE FORCED LANDING TOOK PLACE. |
| Dec 04, 1994 | WADSWORTH, OH | N7614K | Incident | substantial | The loss of engine power for undetermined reasons which resulted in a forced landing on unsuitable terrain. |
| Nov 22, 1994 | MOUNT HAMILTON, CA | N2221R | Minor | substantial |
the pilot's failure to obtain/maintain an adequate airspeed and inadvertent entry into a stall/mush condition during the initial climb due to frost o…the pilot's failure to obtain/maintain an adequate airspeed and inadvertent entry into a stall/mush condition during the initial climb due to frost on the airframe which impeded the airplane's climb performance. Contributing factors were the pilot's improper preflight inspection and inadequate frost removal procedures. |
| Nov 14, 1994 | MONTGOMERY, AL | N146U | Incident | substantial | Investigation pending |
| Oct 26, 1994 | BEULAH, ND | N526HK | Minor | substantial | the failure of the pilot to maintain directional control. |
| Oct 10, 1994 | LAKOTA, ND | CGHRG | Minor | substantial |
PARTIAL LOSS OF ENGINE POWER DUE TO PREIGNITION AND/OR DETONATION, WHICH RESULTED IN FAILURE OF THE NUMBER 4 CYLINDER. THE UNFAVORABLE TAILWIND FOR LA…PARTIAL LOSS OF ENGINE POWER DUE TO PREIGNITION AND/OR DETONATION, WHICH RESULTED IN FAILURE OF THE NUMBER 4 CYLINDER. THE UNFAVORABLE TAILWIND FOR LANDING WAS A RELATED FACTOR. |
| Oct 01, 1994 | RICHMOND, UT | N732VK | Fatal (2) | destroyed |
THE LOSS OF ENGINE OIL PRESSURE DUE TO AN OIL LEAK FROM A LOOSE OIL LINE FITTING. FACTORS WERE THE OBSCURATION, AND THE UNSUITABLE TERRAIN AT THE PILO…THE LOSS OF ENGINE OIL PRESSURE DUE TO AN OIL LEAK FROM A LOOSE OIL LINE FITTING. FACTORS WERE THE OBSCURATION, AND THE UNSUITABLE TERRAIN AT THE PILOT'S DISPOSAL. |
| Sep 11, 1994 | TUNKHANNOCK, PA | N8603U | Incident | substantial | USE OF IMPROPER PROCEDURES DURING A SHORT FIELD LANDING WHICH RESULTED IN AN OVERRUN AND NOSEOVER. |
| Sep 08, 1994 | WILLACOOCHE, GA | N761GQ | Incident | substantial |
THE PILOT'S EXCESSIVE FUEL LEANING DURING IMPROPER USE OF THE MIXTURE CONTROL, WHICH RESULTED IN PRE-IGNITION/DETONATION AND A TOTAL LOSS OF ENGINE PO…THE PILOT'S EXCESSIVE FUEL LEANING DURING IMPROPER USE OF THE MIXTURE CONTROL, WHICH RESULTED IN PRE-IGNITION/DETONATION AND A TOTAL LOSS OF ENGINE POWER. FACTORS WERE THE ELECTRICAL WIRES AND VEHICLES. |
| Sep 03, 1994 | KETTLEMAN CITY, CA | N732DT | Incident | substantial | The pilot's selection of the wrong runway for takeoff and his failure to maintain runway alignment. The sun glare was a factor in this accident. |
| Aug 27, 1994 | AMARILLO, TX | N1779X | Minor | substantial |
THE PILOT'S FAILURE TO ATTAIN PROPER ALIGNMENT OF THE AIRPLANE WITH THE RUNWAY DURING THE LANDING FLARE/TOUCHDOWN. A FACTOR WAS THE PARTIAL LOSS OF EN…THE PILOT'S FAILURE TO ATTAIN PROPER ALIGNMENT OF THE AIRPLANE WITH THE RUNWAY DURING THE LANDING FLARE/TOUCHDOWN. A FACTOR WAS THE PARTIAL LOSS OF ENGINE POWER DUE TO UNDETERMINED REASONS. |
| Jul 26, 1994 | RATHDRUM, ID | N761TK | Incident | substantial | THE FATIGUE FAILURE OF THE CRANKSHAFT AND A SLIPPED BEARING. |
| Jul 25, 1994 | TYLER, TX | N823RH | Serious (1) | substantial | THE PILOT'S FAILURE TO REFUEL. |
| Jul 08, 1994 | BEAVER ISLAND, MI | N88XH | Fatal (2) | destroyed |
Spatial disorientation of the pilot-in-command due to flight into known instrument meteorological conditions; factors in the accident were the fog and…Spatial disorientation of the pilot-in-command due to flight into known instrument meteorological conditions; factors in the accident were the fog and low ceiling. |
| Jun 24, 1994 | CHILOQUIN, OR | N59187 | Minor | substantial | FUEL EXHAUSTION DUE TO A FALSE INDICATION ON THE FUEL QUANTITY SENSOR. |
| Jun 16, 1994 | SANTA TERESA, NM | N199CH | Incident | substantial | A POWER LOSS DUE TO ENGINE DRIVEN FUEL PUMP FAILURE. A FACTOR WAS THE LACK OF SUITABLE TERRAIN FOR A FORCED LANDING. |
| May 14, 1994 | BURLINGTON, IA | N6737B | Serious (2) | destroyed | fuel exhaustion resulting from the failure of the pilot to refuel en route. |
| Mar 31, 1994 | POMONA, MO | N732YK | Incident | substantial | The seperation of the landing gear door actuator, resulting in total loss of hydraulic fluid. |
| Feb 23, 1994 | BAXLEY, GA | N7793U | Incident | substantial | DAMAGE TO THE CRANKSHAFT INTERNAL OIL TUBE BY OTHER MAINTENANCE PERSONS DURING THE ENGINE OVERHAUL THAT RESULTED IN OIL STARVATION. |
| Feb 16, 1994 | EMMETT, ID | N5182Y | Fatal (1) | destroyed | AN INADVERTENT STALL. FACTORS CONTRIBUTING TO THE ACCIDENT WERE FUEL EXHAUSTION AND THE TAILWIND. |
| Feb 08, 1994 | HAVRE, MT | N5520A | Incident | substantial | AN UNDETERMINED LOSS OF ENGINE POWER. |
| Feb 04, 1994 | ARCATA, CA | N93159 | Serious (2) | substantial |
fuel starvation resulting from the pilot's improper in-flight planning and his failure to correctly monitor the aircraft's fuel system and to position…fuel starvation resulting from the pilot's improper in-flight planning and his failure to correctly monitor the aircraft's fuel system and to position the selector valve on a tank containing fuel. |
| Feb 03, 1994 | MCALLEN, TX | N6914R | Minor | destroyed | THE PILOT'S INADVERTENT STALL OF THE AIRPLANE. FACTORS WERE THE PILOT'S FAILURE TO REFUEL AND THE RESULTANT FUEL EXHAUSTION. |
| Feb 03, 1994 | PRENTISS, MS | N6572M | Fatal (2) | destroyed |
A total loss of engine power due to the number five piston crown structure sustaining detonation/pre-ignition damage for undetermined reasons. The num…A total loss of engine power due to the number five piston crown structure sustaining detonation/pre-ignition damage for undetermined reasons. The number two connecting rod and rod bolts failed due to an oil distress event. This resulted in a subsequent in-flight collision with trees and terrain while attempting a forced landing at night. |
| Jan 27, 1994 | OLATHE, KS | N1215M | Serious (1) | substantial |
the pilot's failure to follow procedures and directives regarding the positioning of the fuel tank selector to the fullest tank for the landing portio…the pilot's failure to follow procedures and directives regarding the positioning of the fuel tank selector to the fullest tank for the landing portion of flight. |