N6702K

Substantial
None

Grumman-Schweizer G-164CS/N: 23C

Accident Details

Date
Thursday, April 25, 2002
NTSB Number
LAX02LA143
Location
Olivehurst, CA
Event ID
20020506X00630
Coordinates
39.100276, -121.500831
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

Fuel starvation due to the failure of an engine accessory component. A contributing factor was the rough terrain.

Aircraft Information

Registration
N6702K
Make
GRUMMAN-SCHWEIZER
Serial Number
23C
Engine Type
Turbo-shaft
Year Built
1978
Model / ICAO
G-164CG64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
HAUGHEY HAL W TRUSTEE
Address
C/O MCGARITY FLYING SERVICE
25 ELIZABETH RD
Status
Deregistered
City
SIKESTON
State / Zip Code
MO 63801-9758
Country
United States

Analysis

On April 25, 2002, about 1257 Pacific daylight time, a Grumman-Schweizer G-164C, N6702K, experienced a total loss of engine power while maneuvering during an aerial application flight about 2 miles east of Olivehurst, California. The pilot made a forced landing in a rough field. During the landing rollout, the airplane nosed over and was substantially damaged. The commercial pilot was not injured. The airplane was operated by Moe's Crop Dusting, Marysville, California. Visual meteorological conditions prevailed. The flight was performed under the provisions of 14 CFR Part 137, and it originated from a field near the crash site about 1254.

The pilot holds a Federal Aviation Administration airframe and power plant mechanic certificate. He reported to the National Transportation Safety Board investigator that at the time of the mishap, the airplane's fuel tanks were about 1/2 full. The pilot stated that the airplane had been operating normally during the flight while he was applying fertilizer to the underlying field. Without warning, the Garrett turbine engine lost all power.

Subsequently, the engine was removed from the airframe and examined. The pilot reported that the examination revealed the engine's torque sensor-bearing shaft was broken. This broken gearbox component inhibited proper operation of the fuel control, and the fuel supply to the engine was thereby shut off.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX02LA143