Skip to content

Atlas / NTSB / LAX93LA326

NTSB CAROL · Event

Event LAX93LA326

1993-08-17 TRUCKEE, California, United States Airport · TRK Serious 1 aircraft Status: Completed

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 ↗.

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.

Browse the full corpus — academia portal ↗