Aviation Crash Map

Toland S/Thornburgh J TWIN 503SL N426MT

27 February 2009 · Torrance, California, United States · Fatal

Summary

On 27 February 2009 at about 05:00 local time, a Toland S/Thornburgh J TWIN 503SL registered N426MT was involved in an accident near Torrance, California, United States. 2 people were on board and one died, one was seriously injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 05:00
Classification
Accident
Location
Torrance, California, United States
Nearest airport
Zamperini Field Airport (TOA)
Coordinates
33.8033, -118.3394
Aircraft
Toland S/Thornburgh J TWIN 503SL
Registration
N426MT
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Torrance → Torrance
Aircraft damage
Substantial
Weather
VMC
Light
Night
NTSB number
WPR09LA130

People

1 person died.

On board Died Serious Minor Uninjured
2 1 1 0 0

Probable cause

The passenger’s inadvertent activation of the engine throttle.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The owner/pilot said that the pilot-rated passenger, who was seated in the front seat, had been shown the function of the steering bar, the pedals, the brake, and the throttle. After engine start and while performing the pre-taxi checklist, the steering control bar was tied to the glider's frame tube with a bungee cord. The pilot performed a brake check from the rear seat and then asked the passenger to perform the brake check from the front seat. The glider foot controls are similar to airplane controls, except when the top of the left pedal is depressed it activates the nosewheel brake. When the top of the right pedal is depressed it activates the throttle instead of activating the brake. After the pilot asked the passenger to perform the brake check, the glider engine accelerated to full power and the glider became airborne. Because the control bar was tied to the main frame of the glider the pilot was unable to attain control before the glider stalled. The owner/pilot indicated that the glider did not have a mechanical malfunction or failure.

Quoted verbatim from the NTSB record.

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