No fatalities

14 Jun 2010: AIR TRACTOR INC AT-602 (N4257R) — REYNOLDS FLYING SERVICE INC — Penrose, AR

Penrose, AR, United States

On 14 Jun 2010, an AIR TRACTOR INC AT-602 (registration N4257R) operated by REYNOLDS FLYING SERVICE INC was involved in an aviation accident near Penrose, AR. No fatalities were reported. Investigators recorded the probable cause as: A fatigue crack in the evacuated bellows of the fuel control unit, originating from corrosion pits, which resulted in reduced fuel flow and a subsequent loss of engine power. This summary draws on records from NTSB; 13 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

An Air Tractor AT-602 sustained substantial damage during a forced landing following a partial loss of engine power near Penrose, Arkansas. The commercial pilot suffered minor injuries. Investigation found a fatigue crack in the fuel control unit's bellows led to reduced fuel flow.

Accident Overview

On June 14, 2010, about 0915 central daylight time, an Air Tractor Inc. AT-602, registration N4257R, was substantially damaged during a forced landing after a partial loss of engine power near Penrose, Arkansas. The commercial pilot, the sole occupant, sustained minor injuries. The airplane was registered to and operated by Reynolds Flying Service Inc., of McCrory, Arkansas. Visual meteorological conditions prevailed, and a company flight plan was filed for the 14 Code of Federal Regulations Part 137 agricultural application flight. The local flight departed at an unknown time.

Pilot Account

According to the pilot, while approximately 75 feet above the ground, the turbine-powered airplane experienced a partial loss of engine power. Unable to maintain altitude, the pilot performed a forced landing to a wet rice field. During landing, the airplane impacted a dirt mound, nosed over, and came to rest inverted.

Damage and Examination

A Federal Aviation Administration (FAA) inspector responded to the accident site and reported that the airplane's empennage, left wing, and fuselage sustained structural damage. The FAA inspector, along with a representative from Pratt & Whitney Canada Inc., examined the engine. The compressor turbine and the first stage power turbine vane ring displayed contact signatures consistent with the engine being powered near idle at the time of impact.

Fuel Control Unit Findings

Functional testing of the fuel control unit revealed that the unit's evacuated bellows had developed a fatigue crack in the outer ply surface. This crack would have resulted in a reduced fuel flow to the engine and a subsequent loss of engine power. Laboratory analysis concluded that the crack had originated in an area of several corrosion pits. The cause of the corrosion could not be conclusively determined.

Probable cause

A fatigue crack in the evacuated bellows of the fuel control unit, originating from corrosion pits, which resulted in reduced fuel flow and a subsequent loss of engine power.

Contributing factors

Fatigue/wear/corrosion