Cessna T210M Safety Record
Complete NTSB accident and incident history. 189 events recorded from 1982 to 2025.
| Date | Location | Reg# | Severity | Damage | Probable Cause |
|---|---|---|---|---|---|
| Feb 17, 1995 | MONTROSE, CO | N6094B | Incident | substantial |
THE BENT LANDING GEAR EMERGENCY EXTENSION ASSEMBLY AND THE ACCUMULATION OF AIRFRAME ICE WHICH INTERFERED WITH LANDING GEAR ACTIVATION. A FACTOR WAS TH…THE BENT LANDING GEAR EMERGENCY EXTENSION ASSEMBLY AND THE ACCUMULATION OF AIRFRAME ICE WHICH INTERFERED WITH LANDING GEAR ACTIVATION. A FACTOR WAS THE ALTERNATOR FAILURE FOR UNKNOWN REASONS. |
| 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. |
| 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 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. |
| 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. |
| May 14, 1994 | BURLINGTON, IA | N6737B | Serious (2) | destroyed | fuel exhaustion resulting from the failure of the pilot to refuel en route. |
| 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. |
| Jul 27, 1993 | NEOSHO, MO | N761DD | Incident | substantial |
IS THE PILOT IN COMMAND'S FAILURE TO MAINTAIN PROPER CLEARANCE. FACTORS RELATING TO THIS ACCIDENT ARE THE PILOT IN COMMAND'S INADEQUATE PREFLIGHT PRE…IS THE PILOT IN COMMAND'S FAILURE TO MAINTAIN PROPER CLEARANCE. FACTORS RELATING TO THIS ACCIDENT ARE THE PILOT IN COMMAND'S INADEQUATE PREFLIGHT PREPARATION AND THE LOSS OF TOTAL ENGINE POWER AS A RESULT OF FUEL EXHAUSTION. |
| Apr 06, 1993 | SCAPPOSE, WA | N16CE | Incident | substantial | CLEARANCE FROM OBJECTS WAS NOT MAINTAINED. THE PILOT'S POOR INFLIGHT PLANNING AND THE WEATHER CONDITIONS WERE FACTORS. |
| Feb 16, 1993 | COALINGA, CA | N761NE | Fatal (2) | destroyed |
THE PILOTS INADEQUATE PREFLIGHT PLANNING AND HIS FAILURE TO SELECT A CRUISE ALTITUDE WHICH WOULD ENSURE ADEQUATE TERRAIN CLEARANCE DURING THE NIGHT CR…THE PILOTS INADEQUATE PREFLIGHT PLANNING AND HIS FAILURE TO SELECT A CRUISE ALTITUDE WHICH WOULD ENSURE ADEQUATE TERRAIN CLEARANCE DURING THE NIGHT CROSS COUNTRY. FACTORS IN THE ACCIDENT WERE: THE MOUNTAINOUS NATURE OF THE TERRAIN AND THE DARK NIGHT LIGHT CONDITIONS |
| Feb 21, 1992 | WASHINGTON, IN | N732TR | Incident | substantial | THE TOTAL LOSS OF ENGINE POWER DUE TO A FATIGUE-FRACTURED CRANKSHAFT. |
| Dec 01, 1991 | LA VETA, CO | N6179N | Incident | minor | FAILURE OF THE NO 1 CONNECTING ROD DUE TO LACK OF LUBRICATION FROM BLOCKED OIL PORTS. |
| Aug 03, 1991 | ATLANTIC CITY, NJ | N6877M | Incident | substantial | THE FAILURE OF THE PILOT OF N6877M TO INSURE THE RUNWAY WAS CLEAR PRIOR TO PULLING ONTO THE RUNWAY. |
| Apr 19, 1991 | LITTLETON, CO | N761CM | Serious (2) | destroyed |
IMPROPER REASSEMBLY OF THE OVERHAULED TURBOCHARGER BY MAINTENANCE PERSONNEL, AND THE PILOT'S IMPROPER USE OF THE MIXTURE CONTROL AND BOOST PUMP. FAC…IMPROPER REASSEMBLY OF THE OVERHAULED TURBOCHARGER BY MAINTENANCE PERSONNEL, AND THE PILOT'S IMPROPER USE OF THE MIXTURE CONTROL AND BOOST PUMP. FACTORS RELATED TO THE ACCIDENT WERE: THE ADVERSE WEATHER CONDITIONS AND UNSUITABLE TERRAIN IN THE EMERGENCY LANDING AREA. |
| Mar 02, 1991 | TAOS, NM | N761MU | Fatal (1) | destroyed |
THE PILOT'S DECISION TO INITIATE FLIGHT INTO FREEZING RAIN WHICH RESULTED IN STRUCTURAL ICING THAT EXCEEDED THE ABILITY OF THE AIRCRAFT TO MAINTAIN FL…THE PILOT'S DECISION TO INITIATE FLIGHT INTO FREEZING RAIN WHICH RESULTED IN STRUCTURAL ICING THAT EXCEEDED THE ABILITY OF THE AIRCRAFT TO MAINTAIN FLIGHT. A FACTOR WAS: IMPROPER DEICING. |
| Jan 26, 1991 | SACRAMENTO, CA | N210TW | Fatal (1) | destroyed | A LOSS OF ENGINE POWER FOR UNDETERMINED REASONS AND THE PILOT'S FAILURE TO MAINTAIN AIRSPEED DURING THE ENSUING EMERGENCY LANDING. |
| Jan 06, 1991 | SACRAMENTO, CA | N6148B | Fatal (1) | destroyed |
THE FAILURE OF THE PILOT-IN-COMMAND TO MAINTAIN CONTROL OF THE AIRPLANE WHILE FLYING IN INSTRUMENT METEOROLOGICAL CONDITIONS AND SPATIAL DISORIENTATIO…THE FAILURE OF THE PILOT-IN-COMMAND TO MAINTAIN CONTROL OF THE AIRPLANE WHILE FLYING IN INSTRUMENT METEOROLOGICAL CONDITIONS AND SPATIAL DISORIENTATION OF THE PILOT-IN-COMMAND. CONTRIBUTING TO THE ACCIDENT WAS DIVERSION OF THE PILOT'S ATTENTION TO NAVIGATIONAL TASKS SECONDS BEFORE THE LOSS OF CONTROL. |
| Dec 01, 1990 | MARSHALL, MI | N761LZ | Incident | substantial | DIRECTIONAL CONTROL NOT MAINTAINED BY THE PIC. |
| Oct 25, 1990 | CARBONDALE, CO | N761TW | Fatal (2) | destroyed | FAILURE OF THE PILOT TO SEE-AND-AVOID THE POWER LINE. |
| Oct 10, 1990 | ENGLEWOOD, CO | N565RA | Incident | substantial | ENGINE FAILIURE RESULTING FROM MAINTENANCE DISCREPANCIES. |
| Aug 17, 1990 | SODA SPRINGS, CA | N732VS | Minor | substantial |
ENGINE FAILURE DUE TO INADEQUATE VAPOR RECOVERY SYSTEM (INADEQUATE AIRCRAFT MAINTENANCE/SERVICE) AND INCORRECT FUEL GRADE. A FACTOR IN THE ACCIDENT WA…ENGINE FAILURE DUE TO INADEQUATE VAPOR RECOVERY SYSTEM (INADEQUATE AIRCRAFT MAINTENANCE/SERVICE) AND INCORRECT FUEL GRADE. A FACTOR IN THE ACCIDENT WAS UNSUITABLE TERRAIN. |
| Jul 07, 1990 | WHARTON, TX | N351WB | Minor | substantial | THE LOSS OF POWER DUE TO AN OUT-OF-RIG CONDITION IN THE AUTOMATIC AUXILIARY BOOST PUMP MECHANISM. |