N6583

Substantial
None

GRUMMAN G-164AS/N: 720

Accident Details

Date
Saturday, July 7, 2012
NTSB Number
CEN12LA458
Location
Egeland, ND
Event ID
20120719X02902
Coordinates
48.626388, -99.097221
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The partial loss of engine power for reasons that could not be determined during postaccident examinations.

Aircraft Information

Registration
Make
GRUMMAN
Serial Number
720
Engine Type
Reciprocating
Year Built
1970
Model / ICAO
G-164AG64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
G-164A

Registered Owner (Current)

Name
SCHWEND BRIAN DBA
Address
PO BOX 45
City
FORSYTH
State / Zip Code
MT 59327-0045
Country
United States

Analysis

On July 7, 2012, about 1300 central daylight time, a Grumman G-164/A, N6583, sustained substantial damage during a forced landing to a wheat field after a reported loss of power near Egeland, North Dakota. The pilot was not injured. The airplane was registered to and operated by the pilot under the provisions of the 14 Code of Federal Regulations Part 137 as an aerial application flight. Visual meteorological conditions prevailed at the time of the accident. No flight plan was filed. The local flight departed from the Cando Municipal Airport (9D7), Cando, North Dakota, at an unknown time.

The pilot reported that he made two application passes over the wheat field. During the reversal turn on the second pass, the airplane cleared a set of power lines and began to settle. The pilot applied full throttle, but the engine did not respond, and he airplane continued to sink. He flared the airplane and landed in the wheat field. During the landing roll, the landing gear failed resulting in substantial damage to the right wing. The pilot stated, "As far as I could tell, the engine stopped making power and settled in the field."

The airplane was equipped with a 450-horsepower Pratt and Whitney R-985 carbureted engine. The examination of the propeller blades revealed that both propeller blades exhibited leading edge gouges, chordwise scratches, and blade twist, which was consistent with the engine operating at the time of ground impact.

At 1235, the surface weather observation at Rugby, North Dakota, located 39 nautical miles southwest of the accident site, was: wind 250 degrees at 9 knots; 10 miles visibility; sky clear; temperature 25 degrees Celsius; dew point 17 degrees Celsius; altimeter 30.23 inches of mercury.

The FAA Carburetor Icing Probability Chart indicated that there was the potential of accruing carburetor ice while operating at a sustained idle engine power setting.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN12LA458