Cessna 320 Safety Record
Complete NTSB accident and incident history. 89 events recorded from 1982 to 2026.
| Date | Location | Reg# | Severity | Damage | Probable Cause |
|---|---|---|---|---|---|
| Feb 09, 2026 | Bartow, FL | N3034T | Incident | — | Investigation pending |
| Jun 21, 2011 | Phoenix, AZ | N6160Q | Incident | substantial |
The mechanic's failure to properly secure the nose landing gear actuator push-pull tube to the landing gear door hinge clevis, which resulted in the g…The mechanic's failure to properly secure the nose landing gear actuator push-pull tube to the landing gear door hinge clevis, which resulted in the gear jamming and not fully retracting after takeoff. |
| Sep 18, 2010 | Denton, TX | N56VP | Incident | substantial | The failure of the landing gear push-pull rod. |
| Apr 13, 2007 | McKinney, TX | N3022T | Incident | substantial | The collapsed of the right main landing gear as result of the failure of the over center down lock. |
| Apr 01, 2007 | Stockton, CA | N3424Q | Incident | substantial |
The landing gear collapsed during taxi as a result of incorrect rigging of the landing gear by other maintenance personnel that prevented the landing …The landing gear collapsed during taxi as a result of incorrect rigging of the landing gear by other maintenance personnel that prevented the landing gear downlock from functioning as designed. |
| May 14, 2006 | Long Beach, CA | N5799X | Incident | substantial | the pilot's inadequate compensation for the crosswind condition and failure to maintain lateral control of the airplane during takeoff. |
| May 30, 2003 | McCarthy, AK | N5712X | Incident | substantial | The collapse of the left main landing gear during the landing roll for undetermined reasons. |
| Sep 26, 2002 | GATESVILLE, TX | N382MR | Incident | substantial | The loss of engine power to the left engine for undetermined reasons. A contributing factor was the rough and uneven terrain. |
| Nov 30, 2000 | ENGLEWOOD, CO | N3043T | Incident | substantial | the failure of the nose landing gear to fully extend due to a bent extension rod. |
| Mar 16, 1999 | BROOMFIELD, CO | N4127T | Incident | substantial |
A partial loss of power on the left engine for undetermined reasons. A factor was the pilot's failure to maintain directional control of the aircraft…A partial loss of power on the left engine for undetermined reasons. A factor was the pilot's failure to maintain directional control of the aircraft during landing flare/touchdown. |
| May 27, 1998 | ROCKPORT, TX | N986J | Incident | substantial |
The pilot's failure to maintain airspeed during a go around which resulted in an inadvertent stall. Factors were the pilot's lack of experience in th…The pilot's failure to maintain airspeed during a go around which resulted in an inadvertent stall. Factors were the pilot's lack of experience in the make and model aircraft, his failure to follow the before landing checklist, and his improper use of the powerplant controls. |
| May 01, 1998 | GREYBULL, WY | N3316Q | Incident | substantial | Stress overload failure of the bellcrank assembly of the left landing gear. |
| Feb 27, 1998 | LINCOLN, ME | N6189Q | Incident | substantial | The pilot's failure to maintain adequate altitude which resulted in left main landing gear contacting a snowbank during the landing approach. |
| Oct 18, 1996 | LONGMONT, CO | N430N | Incident | substantial | The partial failure of the fuel control servo, causing an excessive flow/output of fuel to, and flooding of, the right engine. |
| Apr 28, 1996 | MAMMOTH LAKES, CA | N5752X | Incident | substantial |
the partial failure of the right engine turbocharger wastegate butterfly valve to fully close due to mechanical binding and the low setting of its ass…the partial failure of the right engine turbocharger wastegate butterfly valve to fully close due to mechanical binding and the low setting of its associated absolute pressure controller. A related factor was the high density altitude which reduced the engine's ability to produce adequate manifold pressure. |
| Oct 30, 1993 | SPIRIT LAKE, ID | N3057T | Incident | substantial | THE PILOT'S FAILURE TO MAINTAIN AIRSPEED. THE PILOT'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL WAS A FACTOR. |
| May 28, 1993 | ANCHORAGE, AK | N4198T | Incident | substantial |
AN UNDETERMINED FAILURE THAT RESULTED IN AN OVERVOLTAGE CONDITION OF THE ELECTRICAL SYSTEM, OVERHEATING OF THE BATTERY, OVERDRIVE (OVERTORQUE) OF THE …AN UNDETERMINED FAILURE THAT RESULTED IN AN OVERVOLTAGE CONDITION OF THE ELECTRICAL SYSTEM, OVERHEATING OF THE BATTERY, OVERDRIVE (OVERTORQUE) OF THE LANDING GEAR EXTENSION SYSTEM, A DISCONNECT OF THE EMERGENCY EXTENSION SYSTEM, AND A SUSBSEQUENT COLLAPSE OF THE MAIN GEAR WHEN IT COULD NOT BE LOCKED IN THE EXTENDED POSITION. |
| Apr 21, 1993 | NO. LITTLE ROCK, AR | N3057T | Incident | substantial | THE FAILURE OF THE PILOT TO FOLLOW THE CHECKLIST. A FACTOR WAS THE POPPED CIRCUIT BREAKER |
| Apr 17, 1993 | MESA, AZ | N5711X | Incident | substantial |
the separation of the steering spring from the steering yoke assembly due to inadequate installation. A factor in the accident was inadequate mainten…the separation of the steering spring from the steering yoke assembly due to inadequate installation. A factor in the accident was inadequate maintenance on the aircraft. |
| Sep 24, 1992 | LOWELL, ID | N9811L | Incident | destroyed |
RAM INDUCTION AIR STARVATION OF BOTH ENGINES AND INABILITY OF THE PILOT IN COMMAND TO CLEAR TREES DURING THE FORCED LANDING. FACTORS CONTRIBUTING TO T…RAM INDUCTION AIR STARVATION OF BOTH ENGINES AND INABILITY OF THE PILOT IN COMMAND TO CLEAR TREES DURING THE FORCED LANDING. FACTORS CONTRIBUTING TO THE ACCIDENT WERE LOW CEILINGS AND TREES. |
| Sep 14, 1992 | DARLINGTON, SC | N5754X | Incident | substantial | THE IMPROPER SERVICING OF THE AIRPLANE WITH CONTAMINATED FUEL BY THE OWNER PILOT. |
| Aug 09, 1992 | NOVATO, CA | N3014R | Incident | substantial | THE LOCKED LEFT BRAKE ASSEMBLY DUE TO THE MISSING BRAKE RETAINING CLIPS. |
| Jun 18, 1992 | AZTEC, NM | N3307Q | Incident | substantial |
FAILURE OF THE RIGHT PROPELLER TO FEATHER AND INOPERATIVE GEAR RETRACTION SYSTEM. FACTORS WERE THE HIGH DENSITY ALTITUDE AND THE POWER LOSS DUE TO CON…FAILURE OF THE RIGHT PROPELLER TO FEATHER AND INOPERATIVE GEAR RETRACTION SYSTEM. FACTORS WERE THE HIGH DENSITY ALTITUDE AND THE POWER LOSS DUE TO CONNECTING ROD FAILURE. |
| Jul 08, 1991 | RENO, NV | N3011T | Incident | substantial | THE FATIGUE FAILURE OF THE PROPELLER FEATHERING COUNTER WEIGHT CLAMP ASSEMBLY. |
| Jun 08, 1991 | WASHINGTON, IN | N6158Q | Incident | substantial |
EXCEEDING THE AIRCRAFT'S PROPER DESCENT RATE BY THE PILOT IN COMMAND. FACTORS RELATED TO THE ACCIDENT WERE INOPERATIVE RUNWAY EDGE LIGHTS, PROPER ALIG…EXCEEDING THE AIRCRAFT'S PROPER DESCENT RATE BY THE PILOT IN COMMAND. FACTORS RELATED TO THE ACCIDENT WERE INOPERATIVE RUNWAY EDGE LIGHTS, PROPER ALIGNMENT NOT ATTAINED, IMPROPERLY PLANNED APPROACH, AND INADEQUATE FACILITY MAINTENANCE. |