N48378

Substantial
None

GRUMMAN ACFT ENG COR-SCHWEIZER G-164AS/N: 1620

Accident Details

Date
Monday, August 29, 2011
NTSB Number
CEN11LA610
Location
Monette, AR
Event ID
20110831X81308
Coordinates
35.904998, -90.336669
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The fracture of the throttle cable in tensile overstress because of wear damage, which resulted in the partial loss of engine power.

Aircraft Information

Registration
N48378
Make
GRUMMAN ACFT ENG COR-SCHWEIZER
Serial Number
1620
Engine Type
Turbo-shaft
Year Built
1976
Model / ICAO
G-164AG64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
TRI-AIR LLC
Address
PO BOX 767
Status
Deregistered
City
MONETTE
State / Zip Code
AR 72447-0767
Country
United States

Analysis

On August 29, 2011, approximately 1745 central daylight time, a Grumman Aircraft Eng G-164A, N48378, was substantially damaged during a forced landing, following a loss of engine power, near Monette, Arkansas. The commercial pilot was not injured. The airplane was registered to and operated by Tri-Air LLC., of Monette, Arkansas, under the provisions of 14 Code of Federal Regulations Part 137 as an aerial application flight. Visual meteorological conditions prevailed and a flight plan had not been filed for the local flight.

According to the pilot, after takeoff and when the airplane was approximately 150 feet above ground level, the engine lost partial power. Unable to maintain altitude, the pilot executed a forced landing to a cotton field. During the rollout the airplane nosed over and came to rest inverted. The airplane sustained substantial damage to the fuselage and both wings.

During the postaccident examination the throttle cable was found separated near the carburetor. The cable was removed and examined at the National Transportation Safety Board’s materials laboratory. The examination revealed that the throttle cable was fractured in tensile overstress which was associated with wear damage. The wear damage is consistent with a sharp bend in the cable trajectory.

No further mechanical discrepancies were noted that would have contributed to the partial loss of engine power.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN11LA610