N73252

Substantial
Minor

Scotts-Bell 47 Inc 47G-2AS/N: 2720

Accident Details

Date
Wednesday, July 25, 2012
NTSB Number
CEN12LA480
Location
Akeley, MN
Event ID
20120726X21248
Coordinates
46.903888, -94.723609
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot’s failure to maintain helicopter control during low altitude agricultural operations.

Aircraft Information

Registration
N73252
Make
SCOTTS-BELL 47 INC
Serial Number
2720
Engine Type
Reciprocating
Year Built
1962
Model / ICAO
47G-2AB47G
Aircraft Type
Rotorcraft
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
BOSQUES DE AFRICA NO 167
BOSQUES DE ARAGON
Status
Deregistered
City
STATE MEXICO
State / Zip Code
57170
Country
United States

Analysis

On July 25, 2012, about 1245 central daylight time, a Scotts-Bell 47 Inc. 47G-2A helicopter, 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 the provisions of 14 Code of Federal Regulations Part 137, as an agricultural application flight. Day visual meteorological conditions prevailed and no flight plan was filed.

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. When 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.

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 of the main wreckage. 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.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN12LA480