N48594

Substantial
None

GRUMMAN G164S/N: 1677

Accident Details

Date
Tuesday, December 1, 2020
NTSB Number
CEN21LA072
Location
Elton, LA
Event ID
20201202102362
Coordinates
30.438259, -92.671434
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, which resulted in a forced landing on unsuitable terrain. The reason for the loss of engine power could not be determined based on available evidence.

Aircraft Information

Registration
N48594
Make
GRUMMAN
Serial Number
1677
Engine Type
Turbo-shaft
Year Built
1976
Model / ICAO
G164G64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
RICELAND AVIATION INC
Address
PO BOX 877
Status
Deregistered
City
JENNINGS
State / Zip Code
LA 70546-0877
Country
United States

Analysis

On December 1, 2020, about 1430 central standard time, a Grumman G164 airplane, N48594, was involved in an accident near Elton, Louisiana. The commercial pilot was not injured, and the airplane sustained substantial damage. The airplane was operated as a Title 14 Code of Federal Regulations Part 137 aerial application flight.

According to the pilot, the airplane contained a load of fertilizer and was near maximum gross weight when it departed from the local grass strip to fertilize a ryegrass field about 3.5 miles to the north. Shortly after takeoff, the engine began “running bad", and the pilot added power, but the engine began running worse. The pilot reported the engine then stopped developing power and he made a forced landing in a muddy field about ¼ mile from the grass strip. The airplane nosed over during the landing and came to rest inverted. The airplane sustained substantial damage to the vertical stabilizer and rudder.

The engine and airframe were examined at the operator by inspectors from the Federal Aviation Administration. Visual examination of the engine revealed no anomalies. The engine fuel filter and oil filter were clean and clear of contaminants. Compression was noted on all engine cylinders. The magnetos were removed and tested at a repair facility. A functional test of the magnetos revealed no anomalies.

The atmospheric conditions at the time of the accident were conducive to the accumulation of carburetor ice while operating at cruise or glide power setting. However, the engine power setting used during the takeoff would have been significantly higher than the cruise or descent engine setting; therefore, it is unlikely that carburetor ice accumulated during the accident takeoff.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN21LA072