N73127

Substantial
None

Air Tractor AT-400 S/N: 301-0667

Accident Details

Date
Saturday, April 19, 1997
NTSB Number
FTW97LA169
Location
FLUVANNA, TX
Event ID
20001208X07715
Coordinates
32.890659, -101.150459
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 the reduction gear box. A factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
Make
AIR TRACTOR
Serial Number
301-0667
Engine Type
Turbo-prop
Year Built
1987
Model / ICAO
AT-400 A400
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
AT-400A

Registered Owner (Current)

Name
GEORGES AIRCRAFT REPAIR
Address
11674 US HIGHWAY 70 S
City
VERNON
State / Zip Code
TX 76384-8360
Country
United States

Analysis

On April 19, 1997, at 1400 central daylight time, an Air Tractor AT-400 agricultural airplane, N73127, registered to and operated by Benny White Flying Service, Inc., as a Title 14 CFR Part 137 aerial application flight, was substantially damaged during a forced landing following a loss of engine power near Fluvanna, Texas. The commercial pilot was not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the local flight that originated from a private airstrip near Lamesa, Texas.

According to the pilot, he was performing a swath run when he felt a vibration, followed by a loss of engine power. A forced landing was initiated to a plowed field. During the landing sequence, the left main landing gear separated from the fuselage, and the right wing spar was bent upward.

Examination of the PT6A-27 engine by a mechanic and the FAA inspector revealed that the turbine disc was missing approximately half of its blades. The engine was sent to Dallas Airmotive in Dallas, Texas, for further examination. On May 22, 1997, a teardown inspection revealed that the reduction gear box failed and sheared the drive shaft. According to the FAA inspector, "It was impossible to determine which part failed first. This failure allowed a turbine over speed to the point that the turbine blades separated from the wheel causing a contained catastrophic failure."

According to the operator, the engine had accumulated a total of 2,430 hours since new, with approximately 1,300 hours since last overhaul.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW97LA169