N8661H

Substantial
None

Grumman G-164AS/N: 1453

Accident Details

Date
Tuesday, September 28, 2004
NTSB Number
FTW04CA246
Location
Gilbert, LA
Event ID
20041013X01614
Coordinates
32.014167, -91.663887
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of a piston connecting rod for undetermined reasons resulting in the loss of engine power. A contributing factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N8661H
Make
GRUMMAN
Serial Number
1453
Engine Type
Turbo-shaft
Year Built
1975
Model / ICAO
G-164AG64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
AACM LLC
Address
225 S MAIN STE 1
REGIONAL AIRPORT (ARG)
Status
Deregistered
City
JONESBORO
State / Zip Code
AR 72401
Country
United States

Analysis

On September 28, 2004, at 0900 central daylight time, a Grumman G-164A single-engine agricultural biplane, registered to a private individual and operated by The Airport, of Gilbert, Louisiana, was substantially damaged during a forced landing following a loss of engine power near Gilbert, Louisiana. The commercial pilot, sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 137 aerial application flight. The local flight originated from a private airstrip near Gilbert, Louisiana, at 0830.

The 11,000-hour pilot reported in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) that after he performed a preflight inspection on the airplane, he conducted a 45-minute aerial application flight. After reloading the hopper with a chemical load, he departed the private airstrip to commence a second aerial application on a nearby field. During the aerial application flight, the "engine began running rough," and the pilot initiated a turn back toward the airport while "attempting to gain altitude." At an altitude of approximately 200 feet above ground level and approximately 1/2 mile from the runway, the engine "shuttered violently and quit." The pilot initiated a forced landing to a nearby pasture. During the landing roll, the airplane impacted a fence, crossed two ditches, a road, impacted a second fence, crossed another pasture, and impacted a third fence before coming to rest upright in a plowed field.

Examination of the airplane by an Federal Aviation Administration (FAA) inspector, who responded to the site of the accident, revealed the lower right wing was separated from the fuselage. The upper wing was completely separated from its mount. Examination of the Pratt and Whitney R-1340 radial engine revealed a piston connecting rod was separated from the piston.

The operator reported that at the time of the accident, the engine had accumulated 462 hours since the last major overhaul, and 300 hours since the last annual inspection.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW04CA246