No fatalities

25 Jul 2012: Scotts-Bell 47 Inc 47G-2A (N73252) — SCOTTS HELICOPTER SERVICE INC — Akeley, MN

Akeley, MN, United States

On 25 Jul 2012, a Scotts-Bell 47 Inc 47G-2A (registration N73252) operated by SCOTTS HELICOPTER SERVICE INC was involved in an aviation accident near Akeley, MN. No fatalities were reported. Investigators recorded the probable cause as: The pilot’s failure to maintain helicopter control during low altitude agricultural operations. This summary draws on records from NTSB; 3 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On July 25, 2012, a Bell 47G-2A helicopter (N73252) was substantially damaged during an agricultural spraying operation near Akeley, Minnesota. The pilot reported a yaw and vibration before the helicopter impacted terrain. No preimpact anomalies were found.

Accident Overview

On July 25, 2012, about 1245 central daylight time, a Scotts-Bell 47 Inc. 47G-2A helicopter, registration N73252, was substantially damaged when it impacted terrain while spraying a potato field near Akeley, Minnesota. The commercial pilot sustained minor injuries. The helicopter was registered to and operated by Scotts Helicopter Service, Inc., under 14 Code of Federal Regulations Part 137 as an agricultural application flight. Day visual meteorological conditions prevailed, and no flight plan was filed.

Pilot Report

The pilot reported he was on a “clean up” pass and descending into the field, over a set of 20-foot power lines, when he experienced a slight yaw to the right and felt a slight vibration that seemed to be coming from the rear of the helicopter. As he began to apply left pedal input, the helicopter immediately entered an excessively nose-low attitude with an increased yaw to the right. After the pilot applied aft cyclic control, the helicopter impacted terrain and came to rest on its left side.

Damage and Examination

The fuselage, tail boom, and main rotor were bent, crushed, and wrinkled. The tail rotor gear box and tail rotor separated from the helicopter. One separated tail rotor blade was observed 50 feet to the north of the main wreckage, and the other blade was observed 50 feet to the south. An examination of the helicopter and its systems revealed no preimpact anomalies, and there was no evidence of a wire strike. The source of the vibration could not be determined.

Contributing factors

Attain/maintain not possiblePilot