Plane Crash List

Payne/Foster GLASAIR N250CH

24 August 2011 · Ocala, Florida, United States · No injuries

Summary

On 24 August 2011 at about 22:13 local time, a Payne/Foster GLASAIR registered N250CH, operated by Garner Walter C, was involved in an accident near Ocala, Florida, United States. One person was on board and nobody was 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 22:13
Classification
Accident
Location
Ocala, Florida, United States
Nearest airport
Ocala International Airport (OCF)
Coordinates
29.1697, -82.2211
Aircraft
Payne/Foster GLASAIR
Registration
N250CH
Category
Airplane
Engines
1
Operator
Garner Walter C
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Melbourne → Ocala
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
ERA11CA471

People

Nobody was injured.

On board Died Serious Minor Uninjured
1 0 0 0 1

Probable cause

The failure of the tailwheel locking mechanism to remain engaged while landing in a crosswind, which resulted in a loss of directional control and runway excursion.

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

Read the full NTSB narrative

According to the pilot, he landed the airplane with a crosswind, and during the rollout the airplane veered to the left, ground looped, and departed the left side of the runway. The right main landing gear became caught in a grassy area, which brought the airplane to rest and resulted in substantial damage to the fuselage. A postaccident examination of the airplane revealed that the tailwheel lock mechanism of the free-castering tailwheel assembly was unable to keep the tailwheel engaged in the locked position. The mechanism that locked the tailwheel assembly in place was not broken; however, the spring of that particular tailwheel assembly kit worked in compression, rather than tension, which resulted in less pressure being applied to the tailwheel lock and greater susceptibility for the tailwheel to unlock during a crosswind landing. Subsequently, when the lock mechanism was moved repetitively, it became dislodged from the notch.

Quoted verbatim from the NTSB record.

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