Probable cause
The pilot’s failure to attain a climb gradient sufficient to clear the rising terrain, which resulted in his decision to make a forced landing on a road.
NTSB analysis
Before departure, the pilot calculated the density altitude and the required takeoff distance. Due to density altitude considerations, he did not fill the fuel tanks to capacity. His calculations indicated that the required runway length was as at least 2,000 feet less than the available 5,781-foot-long runway. After the airplane lifted off, and the pilot observed a positive rate of climb, retracted the flaps to zero, and selected the landing gear to the retracted position. However, the landing gear did not retract. Due to rising terrain directly ahead, the pilot decided to make a forced landing to a road. On short final, the airplane drifted to the right and the left main landing gear struck a chain link fence. The airplane came to rest upright in a watermelon patch. Postaccident examination of the airplane did not reveal any mechanical anomalies that would have precluded normal operation. According to the airplane manufacturer, for the prevailing ambient conditions, the airplane was capable of climbing 227 feet per minute.
Text from the NTSB. Open the NTSB docket for WPR11LA013 for the full record.
Event
- Date
- Oct 10, 2010
- Type
- Accident
- Place
- Blanding, Utah
- Nearest airport
- Blanding Municipal Airport (BDG)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Beech C24
- N-number
- N5063M
- Category
- Airplane
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Personal
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.