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 ↗.
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Related research
Matched on aircraft type or causal vocabulary (fuel exhaustion, go-around). All research papers
- NASA NTRS 2025 · Conference Paper A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- Semantic Scholar 2022 · Article (Journal of Safety Research) Go-around accidents and general aviation safety.
INTRODUCTION Changes in General Aviation (GA) accident rates, specifically in the go-around phase, are examined by comparing the number of accidents, the proportion of fatal accidents, and the proport…
- Semantic Scholar 2021 · Article (Aerospace) Classification and Analysis of Go-Arounds in Commercial Aviation Using ADS-B Data
Go-arounds are a necessary aspect of commercial aviation and are conducted after a landing attempt has been aborted. It is necessary to conduct go-arounds in the safest possible manner, as go-arounds …
- NASA NTRS 2021 · Accepted Manuscript (Version with final changes) Go-Around Criteria Refinement for Transport Category Aircraft
Presently, airline pilots are trained to go around if, when lower than 500 ft above the ground, they are outside of a handful of parameters such as airspeed, position, and rate of descent.
- NASA NTRS 2019 · Conference Paper Validation of Proposed Go-Around Criteria Under Various Environmental Conditions
This paper evaluates the effects of environmental conditions on touchdown performance under varying approach states and validates proposed go-around criteria developed using data from a previously con…