N10415

Substantial
None

HUGHES 269A S/N: 76-0629

Accident Details

Date
Tuesday, November 8, 1994
NTSB Number
FTW95LA039
Location
MONTICELLO, AR
Event ID
20001206X02592
Coordinates
33.619129, -91.790710
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

THE LOSS OF ENGINE POWER DUE TO A FATIGUED ROD END BOLT. A FACTOR WAS THE LACK OF SUITABLE TERRAIN FOR LANDING.

Aircraft Information

Registration
N10415
Make
HUGHES
Serial Number
76-0629
Year Built
1966
Model / ICAO
269A

Registered Owner (Historical)

Name
WHEATLEY DAVID L JR
Address
3373 CHISHOLM TRL SW
Status
Deregistered
City
MARIETTA
State / Zip Code
GA 30060-6186
Country
United States

Analysis

On November 8, 1994, at 1445 central standard time, a Hughes 269A, N10415, was substantially damaged during a forced landing near Monticello, Arkansas. The airplane, operated by ARKLATEX Helicopters, Inc., and flown by a commercial pilot, was on a local controlled burning defoliation flight. There was no flight plan filed and visual meteorological conditions prevailed. The pilot, the sole occupant, was not injured.

According to the pilot, he lost engine power and initiated an autorotation. During the descent, he extended his glide in order to clear a pile of logs. The aircraft subsequently touched down in a mud hole and rolled over on its right side. The pilot stated that after extricating himself from the wreckage, he noticed a piston push rod protruding from the case. He also reported that "suitable terrain for landing was not available in the immediate area."

An examination of the aircraft revealed that it had sustained substantial damage to the airframe and dynamic components. The examination also revealed that the fuel system maintained its integrity and contained approximately 12 gallons of fuel. The engine casing exhibited evidence that a malfunction of the rod had occurred. Additional examination of the engine revealed that the rod end bolts had failed. Two bolts were forwarded to the National Transportation Safety Board's Metallurgical Laboratories for detailed examination. Their examination revealed that the rod end bolts had failed in "fatigue" and that the bolt exhibited "fretting." Physical evidence demonstrated that the bolt "may have been initially installed with insufficient torque or became loose during service."

The helicopter and all retained parts were released to the owner.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW95LA039