SEA93LA036
1992-12-11 · TWIN FALLS, Idaho, United States · Minor · 1 aircraft · Status: Completed
Airport TWF
Aircraft involved
Probable cause & findings
THE PILOT'S FAILURE TO MAINTAIN THE ILS GLIDE PATH.
Factual narrative
AFTER AN ALL DAY FLIGHT FROM VERO BEACH, FLORIDA, THE PILOT DIVERTED FROM HIS DESTINATION TO HIS ALTERNATE AND ATTEMPTED A COUPLED ILS APPROACH AT TWIN FALLS, IDAHO. DURING THE APPROACH, HIS AUTOPILOT DISENGAGED AND HE MISSED THE APPROACH, AND THEN ELECTED TO HAND FLY AN APPROACH, WHEN HE COULDN'T REENGAGE THE AUTOPILOT. DURING THE SECOND APPROACH ATTEMPT, HE DESCENDED BELOW THE GLIDE PATH AND IMPACTED TERRAIN. WEATHER AT THE TIME OF THE OCCURRENCE WAS ONE HALF MILE VISIBILITY AND 200 FEET OBSCURED CLOUD LAYER. THE AIRCRAFT ROLLED OVER AFTER IMPACTING IN A LEVEL PLOWED FIELD. THE PILOT TURNED ON THE ELT AFTER TRYING HIS RADIOS AND DISCOVERING THAT THE ELT WAS NOT TRANSMITTING. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1992_SEA93LA036.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 (autopilot). All research papers
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ROSflight is a lean, open-source autopilot ecosystem for unmanned aerial vehicles (UAVs). Designed by researchers for researchers, it is built to lower the barrier to entry to UAV research and acceler…
- arXiv 2025 · arXiv preprint ROSplane 2.0: A Fixed-Wing Autopilot for Research
Unmanned aerial vehicle (UAV) research requires the integration of cutting-edge technology into existing autopilot frameworks.
- arXiv 2024 · arXiv preprint A Data-Driven Autopilot for Fixed-Wing Aircraft Based on Model Predictive Control
Autopilots for fixed-wing aircraft are typically designed based on linearized aerodynamic models consisting of stability and control derivatives obtained from wind-tunnel testing.
- arXiv 2022 · arXiv preprint Experimental Flight Testing of a Fault-Tolerant Adaptive Autopilot for Fixed-Wing Aircraft
This paper presents an adaptive autopilot for fixed-wing aircraft and compares its performance with a fixed-gain autopilot.
- arXiv 2021 · arXiv preprint An Adaptive Digital Autopilot for Fixed-Wing Aircraft with Actuator Faults
This paper develops an adaptive digital autopilot for a fixed-wing aircraft and compares its performance with a fixed-gain autopilot.
- arXiv 2026 · arXiv preprint Robust Adaptive Sliding-Mode Control for Damaged Fixed-Wing UAVs
Many unmanned aerial vehicles (UAVs) can remain aerodynamically flyable after sustaining structural or control surface damage, yet insufficient robustness in conventional autopilots often leads to mis…