NTSB CAROL · Event
Event FTW83FA407
Aircraft involved
Factual narrative
THE ACFT HAD IMPACTED IN A STEEP RIGHT WING DOWN, NOSE LOW ATTITUDE. NO PREIMPACT, MECHANICAL MALFUNCTION OR FAILURE WAS FOUND. THE PLT'S BLOOD ALCOHOL LEVEL WAS 0.054%. THERE WERE NO ENTRIES IN THE PLT'S LOG BOOK FOR PREVIOUS FLTS IN LUSCOMBE ACFT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1983_FTW83FA407.txt.
Findings + structured fields enriched from FAA avall.mdb.
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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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