N48584

Substantial
None

GRUMMAN G164A S/N: 1664

Accident Details

Date
Friday, June 25, 1993
NTSB Number
ATL93LA116
Location
BRUNDIDGE, AL
Event ID
20001211X12539
Coordinates
31.710685, -85.809783
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

THE BROKEN CARBURETOR ACCELERATOR PUMP PISTON RIVET WHICH LODGED UNDER THE NEEDLE VALVE, ALLOWED THE FLOAT CHAMBER TO FLOOD WITH FUEL, AND THE ENGINE TO QUIT. THE LACK OF SUITABLE TERRAIN FOR A FORCED LANDING WAS A FACTOR.

Aircraft Information

Registration
N48584
Make
GRUMMAN
Serial Number
1664
Engine Type
Turbo-shaft
Model / ICAO
G164A G64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MATNEY FRED H II DBA
Address
PO BOX 245
Status
Deregistered
City
BRUNDIDGE
State / Zip Code
AL 36101
Country
United States

Analysis

On June 25, 1993, at about 0845 central daylight time, a Grumman G164A, N48584, collided with trees and the ground, following a loss of engine power, during cruise flight near Brundidge, Alabama. The airplane was operated by Brundidge Spray Service under 14 CFR Part 91 and visual flight rules. Visual meteorological conditions prevailed at the accident site. A flight plan was not filed for the aerial application flight. There were no injuries to the commercial pilot, while the airplane was substantially damaged. Origination of the flight was Brundidge, Alabama, about 40 minutes prior to the accident.

The pilot reported he had completed spraying a cotton field and was returning to the airfield. He had climbed to 150 to 200 feet when the engine emitted a puff of black smoke from the exhaust, and quit. The airplane descended into and collided with the heavily wooded terrain. He also reported that the engine had been operated about 13 hours since a zero time major overhaul.

The engine examination revealed that two of six rivets that fasten the carburetor accelerator pump piston had failed. Both of the rivets were found in the float chamber. One of the rivets was found near the needle and seat. A Malfunction or Defect Report submitted by an airworthiness inspector stated that the loose rivet may have caused the [carburetor] needle to stay open.

Engine records revealed that the engine was overhauled on May 11, 1993. According to the operator's report of the accident, the engine had 13 hours since the overhaul. The engine records also revealed that the engine was operated on a test stand, following the overhaul, with a slave carburetor. An Accessory Inspection Record attached to the overhaul records indicated that magnetos were inspected. A carburetor was not listed.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL93LA116