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FTW00LA025

1999-11-03 · IOWA PARK, Texas, United States · Minor · 1 aircraft · Status: Completed

Airport F14

Current FAA registration · N415

Make / Model
STREIFTHAU BABY GREAT LAKES
Year of manufacture
1977 · 22 years old at event
Engine
CONT MOTOR C85 SERIES (85 hp)
Seats / Engines
1 seats · 1 engine
Last airworthiness date
19800121
ADS-B equipped
Yes — Mode-S A4E6B2

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The loss of engine power due to fuel exhaustion as a result of the pilot's failure to refuel the airplane.

Factual narrative

On November 3, 1999, at 0730 central standard time, a Streifthau Baby Great Lakes experimental amateur-built airplane, N415, was substantially damaged during a forced landing following a loss of engine power near the Wichita Valley Airport, Iowa Park, Texas. The airplane was registered to and operated by the private pilot, who sustained minor injuries. Visual meteorological conditions prevailed for the 14 Code of Federal Regulations Part 91 personal flight and a flight plan was not filed. The flight originated from the Wichita Valley Airport at 0720. The pilot reported during a telephone interview that he had recently purchased the airplane, and the previous owner had informed him that the airplane required fuel before its next flight. He reported in the Pilot/Operator Aircraft Accident Report that he was performing high-speed taxi tests and simulated takeoffs, when the airplane started to veer toward the edge of the taxiway. He elected to take off and fly one traffic pattern. He realized during the approach to land that the airplane's airspeed was too fast, and he initiated a go-around. The pilot pitched the airplane nose up and applied full power, simultaneously the engine "began to sputter" and subsequently, lost total power. The airplane contacted the ground and came to rest upright, 0.5 miles northeast of the departure end of runway 22. The pilot reported that he did not check the quantity of fuel prior to the flight. According to the FAA inspector, who examined the airplane at the accident site, the engine firewall was displaced and the engine mounts were damaged. The wings, including the wing spars, were structurally damaged. He estimated that there was "one cup of fuel in the fuselage mounted fuel tank." In the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2), in the section titled "Recommendation (How Could This Accident Have Been Prevented)," the pilot stated the following: Fuel aircraft before taxi testing. Note: Extensive personal injury prevented by the use of a 4-point harness and full face motorcycle helmet. During a go-around, the airplane's engine lost power as a result of fuel exhaustion. The pilot stated that he had recently purchased the airplane, and the previous owner had informed him that the airplane required fuel before its next flight. The pilot was performing high-speed taxi tests and simulated takeoffs on a taxiway when the airplane began to veer toward the edge of the taxiway. The pilot elected to take off and fly one traffic pattern. While on approach to the runway, he realized the airplane's airspeed was high, and he initiated a go-around. As the airplane reached a nose-up attitude, the engine 'sputtered' and lost total power. A forced landing was executed and the airplane impacted the ground. An FAA inspector examined the airplane at the accident site and reported that there was 'one cup of fuel in the fuselage mounted fuel tank.' Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1999_FTW00LA025.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, go-around). All research papers