WPR14CA204
2014-05-22 · Wellington, Nevada, United States · None · 1 aircraft · Status: Completed
Airport NV72
Current FAA registration · N2068Z
- Make / Model
- CESSNA 150C
- Year of manufacture
- 1963 · 51 years old at event
- Engine
- CONT MOTOR 0-200 SERIES (100 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19630308
- ADS-B equipped
- Yes — Mode-S A1ABD5
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain aircraft control while departing from a wet runway.
Factual narrative
The pilot reported that during the takeoff roll on a wet dirt airstrip, the airplane reached rotation speed quickly but indicated no further speed. The pilot felt the main gear impact softer areas on either side while keeping the airplane under control just prior to lifting off. The airplane was airborne briefly then settled back down. As the airplane was approaching the departure end of the runway where the surface slopes down it became airborne. The pilot reported that he turned toward lower terrain and attempted to follow the airport access road but failed to maintain aircraft control. The airplane did not attain sufficient altitude and collided with a fence and nosed over. The wings, vertical stabilizer and rudder were substantially damaged. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. The pilot reported that during the takeoff roll on a wet dirt airstrip, the airplane reached rotation speed quickly but indicated no further speed. The pilot felt the main gear impact softer areas on either side while keeping the airplane under control just prior to lifting off. The airplane was airborne briefly then settled back down. As the airplane was approaching the departure end of the runway where the surface slopes down it became airborne. The pilot reported that he turned toward lower terrain and attempted to follow the airport access road but failed to maintain aircraft control. The airplane did not attain sufficient altitude and collided with a fence and nosed over. The wings, vertical stabilizer and rudder were substantially damaged. The pilot reported no preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Altitude-Not attained/maintained - C
- — Environmental issues-Physical environment-Object/animal/substance-Fence/fence post-Contributed to outcome
- — Environmental issues-Physical environment-Runway/land/takeoff/taxi surface-Wet-Contributed to outcome
Verbatim from NTSB's published report. Source file
NTSB_2014_WPR14CA204.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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