No fatalities

15 Jan 2009: AIR TRACTOR INC AT-301 (N3170C) — FLYING B AVIATION LLC — Beaver, UT

Beaver, UT, United States

On 15 Jan 2009, an AIR TRACTOR INC AT-301 (registration N3170C) operated by FLYING B AVIATION LLC was involved in an aviation accident near Beaver, UT. No fatalities were reported. Investigators recorded the probable cause as: A loss of engine power while maneuvering due to a sheared propeller blade's pitch change link. Contributing to the accident was lack of suitable terrain for the forced landing. 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

An Air Tractor AT-301 experienced engine vibration and partial power loss during an aerial application flight, leading to a forced landing on a snow-covered field where it nosed over, causing substantial damage and minor injury to the pilot.

Incident

On January 15, 2009, at approximately 0845 mountain standard time, an Air Tractor AT-301, registration N3170C, operated by Flying B Aviation, LLC, was conducting an aerial application flight about 10 miles southeast of Beaver, Utah. While maneuvering, the engine began to vibrate severely and lost partial power. The pilot performed a forced landing on a snow-covered field. During the rollout, the airplane nosed over, bending a wing and the rudder. The commercial certificated pilot sustained a minor injury, and the airplane was substantially damaged. Visual meteorological conditions prevailed, and no flight plan had been filed. The flight was conducted under 14 Code of Federal Regulations Part 137 and had originated from Beaver at about 0830.

Investigation

The pilot verbally reported to a National Transportation Safety Board investigator that while seeding the designated area, the engine started vibrating very badly. The Pratt & Whitney R-1340 engine had been overhauled several times, and the pilot suspected a mechanical malfunction had occurred.

The airplane was subsequently recovered from the accident site and examined under Federal Aviation Administration (FAA) supervision. The FAA inspector reported finding no evidence of internal engine malfunction when the crankshaft was rotated. No contaminating material was observed in the oil, which appeared clean.

Findings

The FAA inspector noted one observation that, in their opinion, may have related to the vibration reported by the pilot: one of the propeller's pitch change steel pins, which changes the beta angle of the propeller blade, was found sheared in two. No "Aircraft Accident Report" NTSB form 6120.1 was received by the Safety Board from the pilot or operator.

Contributing factors

Causes

Propeller controlling system — Failure

Other contributing factors

Contributed to outcome