N6656Q

Destroyed
Minor

Grumman-Schweizer G164B S/N: 182B

Accident Details

Date
Wednesday, November 11, 1998
NTSB Number
ATL99LA017
Location
CUTHBERT, GA
Event ID
20001211X11366
Aircraft Damage
Destroyed
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The fatigue failure of the accessory gear shaft which resulted in fuel starvation and the loss of engine power. A factors was the fuel system filter restriction.

Aircraft Information

Registration
N6656Q
Make
GRUMMAN-SCHWEIZER
Serial Number
182B
Engine Type
Turbo-shaft
Model / ICAO
G164B G64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
AG PILOTS INC
Address
RT 1 BOX 88A
Status
Deregistered
City
PELAHATCHIE
State / Zip Code
MS 39145
Country
United States

Analysis

On November 11, 1998 about 1700 eastern standard time, a Grumman-Schweizer G164B, N6656Q collided with tree stumps and the ground during a forced landing near Cuthbert, Georgia. The aerial application flight was operated by the pilot under Title 14 CFR Part 137 and visual flight rules. Visual meteorological conditions prevailed at the time of the accident and no flight plan was filed for this flight. The commercial pilot received minor injuries, and the airplane was destroyed. The flight originated in Cuthbert, Georgia, at 1655.

According to the pilot, he was flying 500 feet above the ground and was repositioning the airplane to conduct a spraying operation when the engine lost power. The pilot selected a forced landing area and executed a forced landing. During the emergency land, the airplane collided with tree stumps and nosed over.

During the engine examination there was a fatigue fracture noticed within the fuel control gear shaft. A crack was detected in the web portion of the gear shaft, and heavy wear was noted on the loaded side of the outer dimension (OD) gear teeth and on the shoulder on the OD surface of the shaft brackets. During the fracture examination, it was noted that the "peeling" type fatigue fracture, and the angling of the final separation through the shaft were typical of torsional loading. The failed gear shaft provided direct drive to the engine fuel pump.

During the wreckage examination by FAA Inspectors, it was discovered that the fuel control and the fuselage fuel filters were clogged. An undetermined amount of Jet fuel was discovered at the accident site. Fuel was also found throughout the airframe fuel system. A review of the airframe maintenance logs disclosed that this airplane was retrofitted with Garrett turboprops engine without a Supplemental Type Certificate (STC). There was no STC for the installation of this engine into this airplane.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL99LA017