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ERA25LA324

2025-08-29 · New Smyrna Beach, Florida, United States · Minor · 1 aircraft · Status: Completed

Airport EVB

Current FAA registration · N1607F

Make / Model
CESSNA 172H
Year of manufacture
1966 · 59 years old at event
Engine
CONT MOTOR 0-300 SER (145 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19670104
ADS-B equipped
Yes — Mode-S A0F501

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

Maintenance personnel’s failure to detect and address water contamination of the airplane’s fuel system, which resulted in a total loss of engine power during initial climb.

Factual narrative

The pilot/owner stated she had recently purchased the airplane and that during the preflight inspection, had found water in the fuel tanks. She then drained fuel from the sumps until no water was observed. Engine start, taxi, run up, and one circuit of the traffic pattern were uneventful. After completing a touch-and-go landing, during initial climb, the engine experienced a total loss of power. The pilot elected to land straight ahead and transferred control of the airplane to the pilot in the right seat. When he cycled the throttle from idle to full the engine sputtered before losing power again. The airplane subsequently struck a fence, nosed over, and came to reset inverted resulting in substantial to the airplane’s fuselage and both wings. Postaccident examination of the airplane found water in the fuel lines from the right wing fuel tank, in the strainer, and in the carburetor bowl. The fuel filler caps, and filler necks were corroded and the mechanic who had last performed maintenance on the airplane reported that he had removed water from the airplane’s fuel system and had changed the gaskets on the fuel tank caps one month prior to the accident. No maintenance log entries documenting this work were found in the supplied maintenance logbooks; the last entry was for the annual inspection completed about 9 months before the accident. Fueling records showed the airplane had last been fueled about 5 months before the accident. The examination otherwise found no evidence of any preaccident mechanical malfunctions or failures that would have precluded normal operation of the airframe or engine. Based on this information, the loss of engine power was likely the result of water contamination of the airplane’s fuel system that had not been detected or addressed by the mechanic. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • — Aircraft-Fluids/misc hardware-Fluids-Fuel-Fluid condition
  • — Aircraft-Fluids/misc hardware-Fluids-Fuel-Inadequate inspection
  • — Personnel issues-Task performance-Inspection-Scheduled/routine inspection-Maintenance personnel

Verbatim from NTSB's published report. Source file NTSB_2025_ERA25LA324.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

Matched on aircraft type or causal vocabulary (maintenance). All research papers