No fatalities

27 Sep 2019: Air Tractor AT802 A (N801BF) — Brignac Flying Service Llc — Columbus, MS

Columbus, MS, United States

On 27 Sep 2019, an Air Tractor AT802 A (registration N801BF) operated by Brignac Flying Service Llc was involved in an aviation accident near Columbus, MS. No fatalities were reported. Investigators recorded the probable cause as: A total loss of engine power control for undetermined reasons. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On September 27, 2019, an Air Tractor AT802 (N801BF) sustained substantial damage after a partial power loss and forced landing near Columbus, Mississippi. The commercial pilot was seriously injured; no mechanical anomalies were found.

Accident Overview

On September 27, 2019, at approximately 1045 eastern daylight time, an Air Tractor AT802 airplane, registration N801BF, impacted terrain following a partial loss of engine power near Columbus, Mississippi. The aircraft 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.

Pilot Account

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 found the power lever "felt stuck." Since more room was available on the north end of the field to maneuver, he left the power lever in place 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 uncommanded to idle power. He attempted to increase power but moving the power lever had no effect on the engine.

Forced Landing and Damage

During the forced landing, the left wing impacted a tree, and the airplane cartwheeled before coming to rest on its landing gear, upright. The airplane sustained substantial damage to both wings, the fuselage, and tail section.

Post-Accident Examination

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 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.

Contributing factors

Engine controls