N8151K

Substantial
None

Grumman-Schweizer G-164B S/N: 12121

Accident Details

Date
Thursday, July 13, 2000
NTSB Number
FTW00LA209
Location
KAPLAN, LA
Event ID
20001212X21464
Coordinates
30.000791, -92.280441
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 for an undetermined reason. A factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N8151K
Make
GRUMMAN-SCHWEIZER
Serial Number
12121
Engine Type
Turbo-shaft
Model / ICAO
G-164B G64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
CONSOLIDATED VULTEE AIRCRAFT CORP
Address
GENERAL DELIVERY
Status
Deregistered
City
WAYNE
State / Zip Code
MI 48033
Country
United States

Analysis

On July 13, 2000, at 1630 central daylight time, a Grumman-Schweizer G-164B agricultural airplane, N8151K, was substantially damaged during a forced landing following a complete loss of engine power near Kaplan, Louisiana. The airplane was registered to and operated by Vincent Flying Service, Inc., of Kaplan, Louisiana. The commercial pilot, sole occupant, was not injured. Visual meteorological conditions prevailed for the 14 Code of Federal Regulations Part 137 aerial application flight and a flight plan was not filed. The local flight originated from the operator's private grass airstrip at 1600.

According to the pilot, he completed his 12th application flight of the day and was returning to the operator's airstrip. The airplane was in cruise flight at 200 feet agl when the engine began to "run rough, pop, and then quit." During the ensuing forced landing to a rice field, the airplane nosed over and came to rest inverted.

According to the FAA inspector, who examined the airplane at the accident site, the empennage was bent 180 degrees and "the vertical stabilizer and rudder were resting on the cockpit." He added that the wing struts were bent. Fuel was observed in both wing fuel tanks. The 600-horsepower Pratt and Whitney R-1340-AN1 engine had accumulated a total of 7,386 hours (1,182 hours since overhaul) and underwent its most recent annual inspection on February 17, 2000, approximately 300 hours prior to the accident.

The reason for the loss of engine power was not determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW00LA209