N211JM

Substantial
None

GRUMMAN G-164B S/N: 698

Accident Details

Date
Thursday, June 8, 1995
NTSB Number
FTW95LA392
Location
SPRINGLAKE, TX
Event ID
20001207X03728
Coordinates
34.229171, -102.299606
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 UNCONTAINED FAILURE OF THE THIRD STAGE TURBINE WHEEL. A FACTOR WAS THE LACK OF SUITABLE TERRAIN FOR THE FORCED LANDING.

Aircraft Information

Registration
Make
GRUMMAN
Serial Number
698
Engine Type
Reciprocating
Year Built
1976
Model / ICAO
G-164B G64T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
G-164B

Registered Owner (Current)

Name
SANDERSON GRAIN INC
Address
PO BOX 116
City
SPRINGLAKE
State / Zip Code
TX 79082-0116
Country
United States

Analysis

On June 7, 1995, approximately 2000 central daylight time, a Grumman G-164B, N211JM, was substantially damaged during a forced landing near Springlake, Texas. The airline transport rated pilot was not injured. The airplane was being operated by Sanderson Grain Inc., under Title 14 CFR Part 137. Visual meteorological conditions prevailed for the aerial application flight for which no flight plan was filed.

According to the pilot, the engine lost power when he added power to execute a go around when overflying the runway at his home based airport. The pilot stated that the "engine failed then a big stream of fire followed coming out of the exhaust pipe." The pilot added that he pulled the engine emergency fuel shutoff, and the fire was extinguished.

In the enclosed pilot/operator report, the pilot states that he elected to continue straight ahead and attempt a forced landing in a corn field beyond the county road at the departure end of the runway. The pilot added that the tailwheel impacted a drainage ditch between the road and the corn field, and the airplane nosed over coming to rest in the inverted position. The airplane sustained structural damage to a wing spar and the tail wheel attaching point.

Post examination of the engine by the owners representative revealed that the loss of engine power, and subsequent fire, was attributed to the uncontained failure of the third stage turbine wheel assembly.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW95LA392