Cessna 180 Safety Record
Complete NTSB accident and incident history. 1114 events recorded from 1981 to 2025.
| Date | Location | Reg# | Severity | Damage | Probable Cause |
|---|---|---|---|---|---|
| Jun 22, 1991 | CHALLIS, ID | N4700U | Minor | substantial | THAT THE PILOT ENCOUNTERED UNSUITABLE TERRAIN DURING A FORCED LANDING AFTER A POWER LOSS DUE TO A FRACTURED CYLINDER BOSS AND A BENT ENGINE PUSHROD. |
| Jun 21, 1991 | GRAYLING, MI | N2755C | Incident | substantial | THE PILOT IN COMMAND'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL DURING LANDING ROLL. |
| Jun 21, 1991 | GRAND RAPIDS, MN | N6503A | Incident | substantial |
THE PILOT'S FAILURE TO MAINTAIN A PROPER AIRSPEED DURING LANDING AND THE IMPROPER RECOVERY FROM A BOUNCED LANDING. FACTORS RELATED TO THE ACCIDENT WER…THE PILOT'S FAILURE TO MAINTAIN A PROPER AIRSPEED DURING LANDING AND THE IMPROPER RECOVERY FROM A BOUNCED LANDING. FACTORS RELATED TO THE ACCIDENT WERE THE PILOT'S LACK OF TOTAL EXPERIENCE IN SEAPLANES AND THE GUSTY WIND CONDITION. |
| Jun 16, 1991 | ORR, MN | N4636B | Incident | substantial |
BECAUSE OF INADEQUATE COMPENSATION FOR THE WIND CONDITIONS, AIRCRAFT CONTROL WAS LOST BY THE PILOT. A FACTOR RELATED TO THE ACCIDENT WAS A GUSTY CROS…BECAUSE OF INADEQUATE COMPENSATION FOR THE WIND CONDITIONS, AIRCRAFT CONTROL WAS LOST BY THE PILOT. A FACTOR RELATED TO THE ACCIDENT WAS A GUSTY CROSSWIND LANDING ENVIRONMENT. |
| Jun 13, 1991 | PILOT POINT, AK | N420SB | Incident | substantial | FUEL EXHAUSTION, DUE TO THE PILOT'S INADEQUATE PREFLIGHT. CONTRIBUTING TO THE ACCIDENT WAS THE SOFT AND ROUGH TERRAIN. |
| Jun 13, 1991 | WAUSA, NE | N1721C | Serious (1) | substantial | THE PILOT'S DELAYED DECISION TO TURN AROUND AFTER ENCOUNTERING IFR FLIGHT CONDITIONS. FACTORS WERE RESTRICTED FORWARD VISIBILITY AND POWER LINES. |
| Jun 09, 1991 | NEAR ILIAMNA, AK | N5296D | Incident | substantial | THE PILOT'S DECISION TO LAND ON AN UNIMPROVED AREA. THE SOFT TERRAIN WAS A RELATED FACTOR. |
| May 26, 1991 | DEVILS LAKE, ND | N115F | Incident | substantial | DIRECTIONAL CONTROL NOT MAINTAINED BY THE PILOT. A FACTOR RELATED TO THE ACCIDENT WAS A CROSSWIND CONDITION. |
| May 19, 1991 | SCOTTSBLUFF, NE | N66266 | Incident | substantial |
FAILURE OF THE PILOT TO MAINTAIN DIRECTIONAL CONTROL DURING THE LANDING ROLL. FACTORS RELATED TO THE ACCIDENT WERE A CROSSWIND CONDITION AND LACK OF …FAILURE OF THE PILOT TO MAINTAIN DIRECTIONAL CONTROL DURING THE LANDING ROLL. FACTORS RELATED TO THE ACCIDENT WERE A CROSSWIND CONDITION AND LACK OF TOTAL EXPERIENCE IN TYPE OF AIRCRAFT BY THE PILOT. |
| May 10, 1991 | DREWSEY, OR | N51612 | Minor | destroyed | THE PILOT DELAYED IN GOING-AROUND. |
| May 04, 1991 | TRUCKEE, CA | N9147C | Incident | substantial |
THAT THE PILOT IMPROPERLY USED THE FLIGHT CONTROLS AND BRAKES TO ARREST THE RUNWAY EXCURSION. CONTRIBUTING TO THIS ACCIDENT WAS ENCOUNTERING UNFAVORA…THAT THE PILOT IMPROPERLY USED THE FLIGHT CONTROLS AND BRAKES TO ARREST THE RUNWAY EXCURSION. CONTRIBUTING TO THIS ACCIDENT WAS ENCOUNTERING UNFAVORABLE WINDS, CROSSWIND CONDITIONS, AND LACK OF EXPERIENCE IN THIS TYPE OF AIRPLANE. |
| Apr 26, 1991 | VERNAL, UT | N40LT | Incident | substantial | THE PILOT'S IMPAIRMENT DUE TO ALCOHOL CONSUMPTION AND HIS FAILUE TO CONTROL THE AIRPLANE DURING LANDING. |
| Apr 04, 1991 | YUKON RIVER, AK | N2117Z | Incident | substantial | A CARBURETOR FUEL LEAK DUE TO INADEQUATE ANNUAL INSPECTION. CONTRIBUTING TO THE ACCIDENT WAS THE SNOW COVERED TERRAIN. |
| Mar 29, 1991 | FRIDAY HARBOR, WA | N2601Y | Minor | substantial | THE PILOT'S FAILURE TO MAINTAIN A PROPER CLIMB GRADIENT AND RATE AS A RESULT OF HIS INADEQUATE COMPENSATION FOR WIND CONDITIONS. |
| Mar 10, 1991 | AMOS LAKES, AK | N66036 | Incident | substantial | THE PILOT'S SELECTION OF TERRAIN THAT WAS ROUGH, SNOW-COVERED AND ICY FOR TAKEOFF. |
| Feb 25, 1991 | GLASGOW, MT | N7676A | Incident | substantial |
THE LOSS OF ENGINE POWER DUE TO CARBURETOR ICING. FACTORS RELATING TO THE ACCIDENT WERE THE STRONG WINDS, HIGH OBSTRUCTIONS IN THE AREA AND TAILWIND …THE LOSS OF ENGINE POWER DUE TO CARBURETOR ICING. FACTORS RELATING TO THE ACCIDENT WERE THE STRONG WINDS, HIGH OBSTRUCTIONS IN THE AREA AND TAILWIND CONDITIONS FOR LANDING AT THE ONLY AVAILABLE AREA. |
| Jan 18, 1991 | PATTERSON, LA | N63130 | Fatal (1) | minor | THE PILOT'S FAILURE TO IDENTIFY AN UNSAFE OR HAZARDOUS CONDITION. FACTORS WERE: ROUGH WATER AND HIGH WINDS. |
| Nov 22, 1990 | YOUNG, AZ | N2574K | Serious (1) | substantial | THE PILOT SELECTED THE WRONG RUNWAY AND ATTEMPTED TO LAND WITH A TAILWIND. |
| Nov 04, 1990 | ANCHORAGE, AK | N4597B | Incident | substantial | THE PILOT-IN-COMMAND'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL OF THE AIRPLANE DURING THE LANDING ROLL. |
| Nov 04, 1990 | NORTHWOOD, ND | N2987C | Incident | substantial | POOR IN-FLIGHT PLANNING AND DECISION, UNSUITABLE TERRAIN SELECTED BY THE PIC. |
| Oct 10, 1990 | ANCHORAGE, AK | N3330D | Incident | substantial |
THE PILOT'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL. CONTRIBUTING TO THE ACCIDENT WAS THE EXCESSIVE TAXI SPEED AND INADEQUATE MAINTENANCE ON THE BRAKE…THE PILOT'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL. CONTRIBUTING TO THE ACCIDENT WAS THE EXCESSIVE TAXI SPEED AND INADEQUATE MAINTENANCE ON THE BRAKES BY THE PILOT. |
| Oct 01, 1990 | SWIFT RIVER, AK | N9339T | Incident | substantial | THE PILOT-IN-COMMAND'S FAILURE TO UNDERSTAND THE PERFORMANCE DATA OF THE AIRPLANE, AND HIS FAILURE TO IDENTIFY UNSUITABLE TERRAIN. |
| Sep 26, 1990 | KINGSTON, NH | N2620Y | Serious (2) | destroyed |
AN INFLIGHT COLLISION WITH WATER WHILE MANEUVERING FOR A FORCED LANDING. A FACTOR TO THE ACCIDENT WAS A POWER LOSS DUE TO THE PILOT'S IMPROPER USE OF …AN INFLIGHT COLLISION WITH WATER WHILE MANEUVERING FOR A FORCED LANDING. A FACTOR TO THE ACCIDENT WAS A POWER LOSS DUE TO THE PILOT'S IMPROPER USE OF THE MIXTURE CONTROL. |
| Sep 20, 1990 | WOOD CREEK, AK | N5276D | Incident | substantial | THE PILOT-IN-COMMAND'S FAILURE TO ATTAIN PROPER LIFT OFF AIRSPEED. CONTRIBUTING TO THE ACCIDENT WAS ROUGH AND UNEVEN TERRAIN. |
| Sep 17, 1990 | ENTERPRISE, OR | N3117D | Incident | substantial | THE PILOT'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL OF THE AIRCRAFT DURING LANDING. |