N244GRNORTH AMERICAN AT-6F2012-08-31 NTSB Accident Report

Substantial
None

NORTH AMERICAN AT-6FS/N: 121-42642

Summary

On August 31, 2012, a North American AT-6F (N244GR) was involved in an incident near Council Bluffs, IA. All 2 people aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: An unlocking of the excessively worn tailwheel lock mechanism, which resulted in a loss of directional control during landing.

Immediately after liftoff the flight instructor simulated an engine failure and the pilot executed a rejected takeoff, landing on the runway remaining. When the tailwheel contacted the runway it began to "shimmy violently and disengaged the steering pin." The airplane veered to the left and the pilot was unable to stop the veer using right rudder and brake. The airplane exited the left side of the runway moving sideways to the right. The right main landing gear collapsed causing substantial damage to the right wing. An examination of the tailwheel mechanism showed excessive wear in both the locking collar hole and the drag links in the tailwheel assembly.

This incident is documented in NTSB report CEN12CA607. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N244GR.

Accident Details

Date
Friday, August 31, 2012
NTSB Number
CEN12CA607
Location
Council Bluffs, IA
Event ID
20120905X45522
Coordinates
41.256111, -95.755279
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

An unlocking of the excessively worn tailwheel lock mechanism, which resulted in a loss of directional control during landing.

Aircraft Information

Registration
Make
NORTH AMERICAN
Serial Number
121-42642
Engine Type
Reciprocating
Model / ICAO
AT-6FT6
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Analysis

Immediately after liftoff the flight instructor simulated an engine failure and the pilot executed a rejected takeoff, landing on the runway remaining. When the tailwheel contacted the runway it began to "shimmy violently and disengaged the steering pin." The airplane veered to the left and the pilot was unable to stop the veer using right rudder and brake. The airplane exited the left side of the runway moving sideways to the right. The right main landing gear collapsed causing substantial damage to the right wing. An examination of the tailwheel mechanism showed excessive wear in both the locking collar hole and the drag links in the tailwheel assembly. Both pilots stated that they had locked the mechanism before takeoff and had good directional control of the airplane during the takeoff run.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN12CA607