N6816Q

Substantial
Minor

Grumman-Schweizer G-164BS/N: 320B

Accident Details

Date
Tuesday, July 31, 2001
NTSB Number
MIA01LA204
Location
Edison, GA
Event ID
20010803X01601
Coordinates
31.549999, -84.750000
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

Partial loss of engine power for undetermined reasons during takeoff resulting in the airplane descending, colliding with the ground, and nosing over.

Aircraft Information

Registration
N6816Q
Make
GRUMMAN-SCHWEIZER
Serial Number
320B
Engine Type
Turbo-shaft
Year Built
1977
Model / ICAO
G-164BG64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
OWEN TOMMY A JR DBA
Address
RR 2 BOX 155
Status
Deregistered
City
EDISON
State / Zip Code
GA 31746-9403
Country
United States

Analysis

On July 31, 2001, about 1805 eastern daylight time, a Grumman G-164B, N6816Q, registered to an individual, crashed while attempting a forced landing following loss of engine power during takeoff at Edison, Georgia, while on a 14 CFR Part 137 aerial application flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The airplane received substantial damage and the commercial-rated pilot received minor injuries. The flight was originating at the time of the accident.

The pilot stated the takeoff was normal with the airplane accelerating normally and producing power. Once the main tires cleared the ground, he heard 3 short backfire sounds followed by a loss of engine rpm. He tried to make a slow right hand turn to attempt a landing on a field road. He decided not to continue straight ahead because of trees. The airplane was losing forward speed and altitude as he continued the right turn. Before he could dump the load of 135 gallons of chemical the airplane stalled. The left main landing gear struck the ground first followed by a nose over with the airplane on its back at final rest.

Postcrash examination of the airplane was conducted by an FAA inspector. The inspector stated the engine showed evidence of running at substantial power on contact with soil in the field. The propeller blades were bent in the direct that would prove without a doubt that there was no obvious problem with the engine. The inspector stated the winds had been gusting to 30 to 40 knots that day and the pilot had taken off downwind with a full load of fuel and chemical. (See FAA Inspector Statement)

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA01LA204