NTSB CAROL · Event
Event FTW00LA124
Aircraft involved
Probable cause & findings
The pilot's inadequate preflight inspection, which resulted in the pilot attempting to takeoff with the elevator and ailerons locked by the passenger side seatbelt.
Factual narrative
On April 16, 2000, at 1400 central daylight time, a Luscombe 8C tail wheel equipped airplane, N25270, was substantially damaged when it impacted terrain during takeoff initial climb near Galveston, Texas. The commercial pilot, sole occupant and registered owner of the airplane, was not injured. Visual meteorological conditions prevailed and a flight plan was not filed for the Title 14 Code of Federal Regulations Part 91 personal flight. The local flight was originating from the Scholes Field Airport near Galveston, Texas, at the time of the accident. According to the FAA inspector, who visited the accident site, the pilot attempted to takeoff on runway 17 with the co-pilot's seatbelt wrapped around the co-pilot's flight control. The pilot stated that after the airplane became airborne, he reduced the engine power and attempted to land on the runway. The FAA inspector stated that the airplane impacted the runway with the tail wheel and the right main landing gear first. The right main landing gear collapsed and the outboard 5 feet of the right wing was structurally damaged upon impact with the ground. The airplane then impacted the ground with the left main landing gear, which collapsed. The airplane subsequently nosed down, structurally damaging the firewall. Numerous attempts to obtain a completed Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) from the pilot were unsuccessful. The pilot attempted to takeoff in the tailwheel equipped airplane with the co-pilot's seatbelt wrapped around the co-pilot's flight control. After the airplane became airborne, the pilot reduced the engine power and attempted to land on the runway. The airplane impacted the runway with the tail wheel and the right main landing gear first. The right main landing gear collapsed and the right wing impacted the ground. Subsequently, the left main landing gear collapsed and the airplane nosed down. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_FTW00LA124.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2020 · arXiv preprint
A Lean and Highly-automated Model-Based Software Development Process Based on DO-178C/DO-331
The emergence of a global market for urban air mobility and unmanned aerial systems has attracted many startups across the world.
- NASA NTRS 2019 · Conference Paper
A digital fly-by-wire technology development program using an F-8C test aircraft
A digital fly-by-wire flight control system has been installed in an F-8C test airplane and has undergone extensive ground and flight testing as part of an overall program to develop digital fly-by-wi…
- NASA NTRS 2016 · Conference Paper
Design and development experience with a digital fly-by-wire control system in an F-8C airplane
To assess the feasibility of a digital fly-by-wire system, the mechanical flight control system of an F-8C airplane was replaced with a digital system and an analog backup system.
- NASA NTRS 2019 · Conference Proceedings
Description and Flight Test Results of the NASA F-8 Digital Fly-by-Wire Control System
A NASA program to develop digital fly-by-wire (DFBW) technology for aircraft applications is discussed. Phase I of the program demonstrated the feasibility of using a digital fly-by-wire system for ai…
- NASA NTRS 2019 · Presentation
Failure Analysis of T-38 Aircraft Burst Hydraulic Aileron Return Line
During maintenance troubleshooting for fluctuating hydraulic pressures, a technician found that a right hand aileron return line, on the flight hydraulic side, was ruptured (Fig. 1, 2).
- Embry-Riddle Scholarly Commons 2016 · Journal article (IJAAA)
A Comparison of Cervical and Trunk Musculoskeletal Characteristics between Female and Male Army Helicopter Pilots
Introduction: Neck pain (NP) and low back pain (LBP) are prevalent among military helicopter pilots. Although there have been few studies on sex differences in the NP/LBP prevalence in this population…
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