N8819H

Substantial
None

Grumman-Schweizer G-164A S/N: 1539

Accident Details

Date
Wednesday, October 15, 1997
NTSB Number
FTW98LA016
Location
ALTUS, OK
Event ID
20001208X09011
Coordinates
34.639423, -99.309478
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 due to the cracked cylinder. A factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N8819H
Make
GRUMMAN-SCHWEIZER
Serial Number
1539
Engine Type
Turbo-shaft
Model / ICAO
G-164A G64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
BROWN KEVIN
Address
RT 1 BOX 57
Status
Deregistered
City
DRUMRIGHT
State / Zip Code
OK 74030
Country
United States

Analysis

On October 15, 1997, at 1800 central daylight time, a Grumman-Schweizer G-164A agricultural airplane, N8819H, sustained substantial damage during a forced landing following a loss of engine power near Altus, Oklahoma. The commercial pilot, the sole occupant, was not injured. The airplane was registered to and operated by the pilot, who was doing business as Brown's Flying Service of Drumright, Oklahoma. No flight plan was filed and visual meteorological conditions prevailed for the Title 14 CFR Part 137 local aerial application flight.

During a telephone interview conducted by the NTSB investigator-in-charge and in the attached NTSB Pilot/Operator Aircraft Accident Report, the pilot reported that the engine lost power as he was turning the airplane between spray passes. The pilot further reported that the ensuing forced landing was made to a soft field, and during the landing roll, the airplane nosed over and came to rest inverted. According to the FAA inspector who inspected the airplane at the accident site, the top wing and vertical stabilizer sustained structural damage. Examination of the radial engine, a Pratt & Whitney R-985-14B, by the FAA inspector revealed that a circumferential crack had completely separated the #4 cylinder head from the cylinder barrel.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW98LA016