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GAA20CA010

2019-10-07 · Fallon, Nevada, United States · None · 1 aircraft · Status: Completed

Airport FLX

Current FAA registration · N50618

Make / Model
CESSNA 150J
Year of manufacture
1968 · 51 years old at event
Engine
CONT MOTOR 0-200 SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19680906
ADS-B equipped
Yes — Mode-S A652D6

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's improper preflight fuel planning and quantity inspection, which resulted in fuel exhaustion, a total loss of engine power, a forced landing on unsuitable terrain, and a subsequent nose-over.

Factual narrative

The pilot reported that during the preflight inspection, the fuel gauges indicated that each tank was half-full. The pilot did not visually inspect the fuel tanks to verify the fuel gauge's indicated reading. After a 40-minute local flight, the engine lost power during the right turn to the base leg of the airport traffic pattern. The pilot recalled that airplane's fuel gauge indicated that ¼ of the fuel capacity remained. He forced landed in a "flat" attitude on the desert. The nose landing gear dug into the soft, dry surface and the airplane nosed over. The airplane sustained substantial damage to horizontal stabilizer and the rudder. Additionally, the pilot reported that the accident could have been prevented by visually inspecting the fuel tanks using a fuel stick to assess the airplane's fuel quantity. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The pilot reported that, during the preflight inspection, the fuel gauges indicated that each tank was half full. The pilot did not visually inspect the fuel tanks to verify the fuel gauges' indicated reading. After a 40-minute local flight, the engine lost power as the pilot was turning the airplane onto the base leg of the airport traffic pattern. The pilot recalled that the fuel gauge indicated that 1/4 tank of fuel remained. He made a forced landing in a flat attitude in a desert. The nose landing gear dug into the soft, dry surface, and the airplane nosed over. The airplane sustained substantial damage to the horizontal stabilizer and rudder. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. He added that the accident could have been prevented if he had visually inspected the fuel tanks using a fuel stick to assess the fuel quantity. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Aircraft-Fluids/misc hardware-Fluids-Fuel-Inadequate inspection - C
  • C Personnel issues-Task performance-Planning/preparation-Fuel planning-Pilot - C
  • C Personnel issues-Task performance-Inspection-Preflight inspection-Pilot - C
  • C Environmental issues-Physical environment-Runway/land/takeoff/taxi surface-Soft surface-Effect on operation - C

Verbatim from NTSB's published report. Source file NTSB_2019_GAA20CA010.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 (fuel exhaustion). All research papers