N3654G

Substantial
None

Air Tractor AT-400 S/N: 400-0281

Accident Details

Date
Monday, August 25, 1997
NTSB Number
FTW97LA321
Location
SUDAN, TX
Event ID
20001208X08633
Coordinates
34.060611, -102.520744
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 failure of a compressor turbine blade. A factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
Make
AIR TRACTOR
Serial Number
400-0281
Engine Type
Turbo-prop
Model / ICAO
AT-400 A400
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
AT-400

Registered Owner (Current)

Name
DIXIE FLYING SERVICE INC
Address
PO BOX 270
City
BRADLEY
State / Zip Code
AR 71826-0270
Country
United States

Analysis

On August 25, 1997, approximately 1230 central daylight time, an Air Tractor AT-400 agricultural airplane, N3654G, registered to and operated by King Ag Aviation, sustained substantial damage during a forced landing following a loss of engine power near Sudan, Texas. The commercial pilot, the sole occupant, was not injured. No flight plan was filed and visual meteorological conditions prevailed for the Title 14 CFR Part 137 local aerial application flight.

In a written statement provided to the investigator-in-charge, the pilot reported that "the motor blew up," and he was forced to land the airplane in a field "going across" the furrows. During the ground roll, the left main wheel separated from the landing gear leg, the airplane "got sideways," and the right main landing gear leg then separated from the fuselage.

The FAA inspector who examined the accident site reported that the airplane touched down in a cotton field and rolled about 400 to 500 feet across the furrows before coming to rest in an upright position. He further reported that the fuselage forward of the tail section was twisted.

On September 9, 1997, the engine, a Pratt & Whitney PT6A-20, S/N PCE 22438, was examined under the supervision of a FAA inspector at Dallas Airmotive, Inc., in Dallas, Texas. According to the FAA inspector, "the engine experienced blade failure at the Compressor Turbine disk" resulting in "extensive damage to the hot section of the engine." The inspector reported that his review of the engine maintenance records indicated the blades had 11,381.6 hours total time in service. He further reported that "the blades still had some time left in accordance with the manufacturer's specifications."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW97LA321