NTSB CAROL · Event
Event LAX90LA009
Aircraft involved
Probable cause & findings
PILOT'S INADEQUATE COMPENSATION FOR ADVERSE WINDS. FACTORS RELATED TO THE ACCIDENT WERE: THE ADVERSE WIND CONDITIONS.
Factual narrative
THE PILOT ATTEMPTED TO LAND HIS 65 HP ACFT AT THE BEGINNING OF RWY 05, WHICH WAS 5200 FT LONG. AT THE TIME, THE GUSTY SURFACE WIND WAS ESTIMATED TO BE FROM 140 DEGREES AT 25 TO 35 KNOTS. ON SHORT FINAL APPROACH, IN THE NEAR 90 DEGREE RIGHT X-WIND CONDITION, THE PILOT LOST CONTROL OF HIS ACFT & IT COLLIDED WITH TERRAIN 250 FT SHORT OF THE THRESHOLD. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1989_LAX90LA009.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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