N8626H

Substantial
Minor

Grumman-Schweizer G-164A S/N: 1437

Accident Details

Date
Saturday, March 14, 1998
NTSB Number
ATL98LA055
Location
MARIANNA, FL
Event ID
20001211X09627
Coordinates
30.850915, -85.230812
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The failure of maintenance personnel to secure the magneto cover that resulted in water contamination and the subsequent loss of engine power. A factor was rough and uneven terrain.

Aircraft Information

Registration
N8626H
Make
GRUMMAN-SCHWEIZER
Serial Number
1437
Engine Type
Turbo-shaft
Model / ICAO
G-164A G64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
YON JUDY
Address
RR 1 BOX 270
Status
Deregistered
City
BLOUNTSTOWN
State / Zip Code
FL 32424-9764
Country
United States

Analysis

On March 14, 1998, at 0910 central standard time, a Grumman-Schweizer G-164A, N8626H, nosed over, according to the pilot, during a full stop landing on a county road near Marianna Florida. The aerial application flight operated under the provisions of 14 CFR Part 137 with no flight plan filed. The pilot reported that visual weather conditions prevailed at the time of the accident. The commercial rated pilot received minor injuries. According to the pilot, the airplane sustained substantial structural damage. The flight departed the staging area near Marianna, Florida, at 0905.

Approximately five minutes into the flight the pilot reported that the engine developed a rough running condition. The pilot tried several power settings in an effort to reduce the condition, but no action on his part resolved the rough running condition. Since the pilot could not maintain altitude, he then selected an adjacent field for an emergency landing. The pilot said that landing surface was rough and uneven.

Examination of the engine assembly disclosed that the right magneto cover was not secure and that the five screws that secure the cover to the magneto assembly were missing. The visual examination of the internal components of the magneto assembly showed evidence of water stains on the magneto block. Internal component continuity was established when the engine was rotated completely through. Low compression was also noted on all cylinders. A small quantity of fuel was recovered from the carburetor. According to the aircraft wreckage recovery crew, a substantial amount of fuel was recovered from the wing tanks at the accident site.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL98LA055