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 ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
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Related research
Matched on aircraft type or causal vocabulary (fuel exhaustion). All research papers
- AOPA Air Safety Institute 2023 · Safety advisor Safety Advisor: Fuel Awareness
AOPA Air Safety Institute safety advisor on preventing fuel-exhaustion and fuel-starvation accidents in general aviation. Covers pre-flight fuel planning, reserve requirements (14 CFR 91.151, 91.167),…
- NASA NTRS 2019 · Abstract U.S. Civil Rotorcraft Accidents, 1963 through 1997
The U.S. National Transportation Safety Board (NTSB) has recorded 8,436 rotorcraft accidents during the period mid - 1963 through the end of 1997.
- NASA NTRS 2019 · Contractor Report (CR) A study of carburetor/induction system icing in general aviation accidents
An assessment of the frequency and severity of carburetor/induction icing in general-aviation accidents was performed. The available literature and accident data from the National Transportation Safet…
- NASA NTRS 2018 · Other Parachuting to Safety
NASA's Langley Research Center awarded Ballistic Recovery Systems, Inc., three Small Business Innovation Research (SBIR) contracts to research and develop a new, low cost, lightweight recovery system …