Air Tractor AT802

Columbus, MS — September 27, 2019

Event Information

DateSeptember 27, 2019
Event TypeACC
NTSB NumberCEN19LA334
Event ID20190930X81213
LocationColumbus, MS
CountryUSA
Coordinates33.44333, -88.50889
Highest InjurySERS

Aircraft

MakeAir Tractor
ModelAT802
CategoryAIR
FAR Part137
Aircraft DamageSUBS

Conditions

Light ConditionDAYL
WeatherVMC

Injuries

Fatal0
Serious1
Minor0
None0
Total Injured1

Event Location

Probable Cause

A total loss of engine power control for undetermined reasons.

Full Narrative

On September 27, 2019, about 1045 eastern daylight time, an Air Tractor AT802 airplane, N801BF, sustained substantial damage during an impact with terrain following a partial loss of engine power near Columbus, Mississippi. The airplane was registered to and operated by Brignac Flying Service as a Title 14 Code of Federal Regulations Part 137 aerial application flight. The commercial pilot sustained serious injuries. Visual meteorological conditions prevailed and no flight plan had been filed.
According to the pilot, during a chemical application pass over a field from north to south, he noticed the engine torque "had crept up." As he departed the field to the south, he attempted to reduce engine torque, but noticed the power lever "felt stuck." Since there was more room on the north end of the field to maneuver, he left the power lever where it was and re-entered the field. Following the subsequent pass from south to north, he pulled up and again tried to move the power lever. When it would not move, he increased pressure and it "broke free." The engine then went uncommanded to idle power. He attempted to increase the power but moving the power lever had no effect on the engine. During the forced landing, the left wing impacted a tree and the airplane cartwheeled prior to coming to rest on its landing gear, upright. The airplane sustained substantial damage to both wings, the fuselage, and tail section.
A post-accident examination of the airframe and engine found no mechanical malfunctions or anomalies that would have precluded normal operation. The engine was disassembled and contained signatures consistent with a low power setting. Engine control continuity was established from the cockpit to the engine with no binding. During the examination of the fuel control unit, the power lever and condition lever shaft could not be easily moved by hand as a result of damage sustained during the impact. The fuel control unit was disassembled; however, the cause of the binding was not found. No anomalies were observed.

About This NTSB Record

This aviation event was investigated by the National Transportation Safety Board (NTSB). NTSB investigates all U.S. civil aviation accidents to determine probable cause and issue safety recommendations to prevent future accidents.

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