Aviation Accident Summaries

Aviation Accident Summary FTW99LA204

VICTORIA, TX, USA

Aircraft #1

N4393S

Air Tractor AT-301

Analysis

The agricultural airplane was on its first swath run of a boll weevil eradication flight when the engine cowling separated and struck the propeller and engine. The engine lost power, and the pilot executed a forced landing to a cotton field. During the landing roll, the aircraft 'spun' around. The FAA inspector reported that the fractured engine cowling support bracket had a 'dull surface like it had been broken for a while.' Examination of the aircraft's engine revealed that four push rod tubes were bent.

Factual Information

On July 26, 1999, at 1530 central daylight time, an Air Tractor AT-301 agricultural airplane, N4393S, registered to a private individual and operated by ANF Air Services of Garwood, Texas, was substantially damaged during a forced landing, following a loss of engine power near Victoria, Texas. The commercial pilot, sole occupant of the aircraft, was not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 137 aerial application flight. The local flight originated from the Victoria Regional Airport, Victoria, Texas. According to the FAA inspector, the aircraft was on its first swath run of a boll weevil eradication flight when the engine cowling separated from the aircraft. As the cowling separated it struck the engine and propeller. The engine lost power and the pilot executed a forced landing to a cotton field. During the landing roll, the aircraft "spun" around. Examination of the aircraft by an FAA inspector revealed that the right main landing gear was sheared off, and the left wing was pulled away from the fuselage. Further examination of the engine revealed that four push rod tubes were bent. According to the FAA inspector, the fractured engine cowling support bracket had a "dull surface like it had been broken for a while." The pilot and operator failed to return a completed Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1/2.

Probable Cause and Findings

The separation of the engine cowling due to a fractured support bracket, which resulted in the cowling striking and bending four engine push rods causing a loss of engine power. A factor was the lack of suitable terrain for the forced landing.

 

Source: NTSB Aviation Accident Database

Get all the details on your iPhone or iPad with:

Aviation Accidents App

In-Depth Access to Aviation Accident Reports