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ERA10CA181

2010-03-21 · Connelsville, Pennsylvania, United States · None · 1 aircraft · Status: Completed

Airport VVS

Current FAA registration · N8921V

Make / Model
CESSNA 172M
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19741105
ADS-B equipped
Yes — Mode-S AC4F51

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

A total loss of engine power due to fuel exhaustion due to the pilot's failure to refuel.

Factual narrative

The airplane’s fuel tanks were last filled on the day prior to the accident. It was then flown for 1.3 hours before the accident flight, and not refueled. While en route, the airplane experienced a total loss of engine power. The pilot attempted to perform a forced landing to a field, but the airplane’s nose landing gear contacted a power line. The airplane subsequently impacted the ground inverted. From the time of the last fuel service, to the time of the accident, the airplane accrued 6.0 hours of total Hobbs time. Examination of the airplane, including the fuel feed system, by Federal Aviation Administration inspectors revealed no preimpact mechanical anomalies. Only residual and unusable fuel was found in the tanks. According to the airplane owner's manual, the fuel endurance at cruise power setting is 5.9 hours. That figure does not include, engine start, taxi, takeoff, and climb. The airplane’s fuel tanks were last filled on the day prior to the accident. It was then flown for 1.3 hours before the accident flight, and not refueled. While en route, the airplane experienced a total loss of engine power. The pilot attempted to perform a forced landing to a field, but the airplane’s nose landing gear contacted a power line. The airplane subsequently impacted the ground inverted. From the time of the last fuel service, to the time of the accident, the airplane accrued 6.0 hours of total Hobbs time. Examination of the airplane, including the fuel feed system, by Federal Aviation Administration inspectors revealed no preimpact mechanical anomalies. Only residual and unusable fuel was found in the tanks. According to the airplane owner's manual, the fuel endurance at cruise power setting is 5.9 hours. That figure does not include, engine start, taxi, takeoff, and climb. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Personnel issues-Task performance-Planning/preparation-Fuel planning-Pilot - C

Verbatim from NTSB's published report. Source file NTSB_2010_ERA10CA181.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.