NTSB CAROL · Event
Event LAX93LA326
Registry · N205AS
FAA Aircraft Registry record.
Make / Model
CIRRUS DESIGN SR22T
Year of manufacture
2023
Engine
CONT MOTOR TSIO-550-K (315 hp)
Seats / Engines
5 seats · 1 engine
Last airworthiness date
20230422
ADS-B equipped
Yes — Mode-S A1A4A7
Registrant of record
TURNBULL MOAK & PENDERGRASS LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
FAILURE OF THE PILOT TO CONDUCT ADEQUATE PREFLIGHT CHECKS WHICH RESULTED IN THE GLIDER TAKING OFF WITH A FRAYED RELEASE HOOK CABLE, THE PILOT'S FAILURE TO MAINTAIN AIRSPEED, AND THE INADVERTENT STALL.
Factual narrative
On August 17, 1993, at 1515 hours Pacific daylight time, a Pilatus B4-PC11AF glider, N205AS, collided with the runway surface at the Truckee Tahoe Airport, Truckee, California, after experiencing an inflight loss of control during an aero tow. The pilot was beginning a local visual flight rules personal flight. The glider, operated by Ames Soaring Club, Livermore, California, sustained substantial damage. The certificated private pilot, the sole occupant, received serious injuries. Visual meteorological conditions prevailed. The glider was being towed behind an airplane. Witnesses observed some erratic movement by the glider, followed by a tow line release by the glider. The pilot tried to make a 180 degree turn back to the runway. The glider then lost control and collided with the runway in a nose down, right wing low attitude. The glider was transported to J.J. Glider Repair, Placerville California, for examination. The tow release cable was inspected by the FAA Aviation Safety Inspector from the Reno Flight Standards District Office. The inspector reported he found that the cable was frayed and 50 percent of the strands were broken where the cable exits the instrument panel. He stated that the frayed and broken strands allowed the cable to bind in the housing which prevented complete locking of the tow hook. THE PILOT FAILED TO DISCOVER A FRAYED TOW RELEASE CABLE DURING THE PREFLIGHT CHECK. THE CABLE WAS BINDING WHEN THE PILOT ATTEMPTED TO ABORT HIS TAKEOFF. THE PILOT INADVERTENTLY STALLED THE GLIDER AND IMPACTED THE RUNWAY SURFACE IN A NOSE DOWN, RIGHT WING LOW ATTITUDE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1993_LAX93LA326.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 or causal vocabulary (stall, loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Semantic Scholar 2016 · Article (Interacción)
Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
This paper describes the design and development of an ecological display to aid pilots in the recovery of an In-Flight Loss of Control event due to a Stall (ILOC-S).
- NTSB Aircraft Accident Reports 2010 · Accident report
Loss of Control on Approach — Colgan Air Flight 3407
Colgan Air 3407 / Continental Connection (Q400) Buffalo NY, February 12, 2009 — 50 fatalities. Definitive investigation of the Colgan 3407 stall-stick-pusher crash on approach to Buffalo.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- arXiv 2025 · arXiv preprint
Quadratic Programming Approach to Flight Envelope Protection Using Control Barrier Functions
Ensuring the safe operation of aerospace systems within their prescribed flight envelope is a fundamental requirement for modern flight control systems.
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
Browse the full corpus — academia portal ↗