N3170C

Substantial
Minor

AIR TRACTOR INC AT-301S/N: 301-0591

Accident Details

Date
Thursday, January 15, 2009
NTSB Number
WPR09LA085
Location
Beaver, UT
Event ID
20090117X33913
Coordinates
38.192222, -112.505554
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

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.

Aircraft Information

Registration
N3170C
Make
AIR TRACTOR INC
Serial Number
301-0591
Year Built
1984
Model / ICAO
AT-301

Registered Owner (Historical)

Name
SALE REPORTED
Address
XXXX
Status
Deregistered
City
NONE
State / Zip Code
OK 73125
Country
United States

Analysis

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

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

The airplane was subsequently recovered from the accident site and examined under Federal Aviation Administration (FAA) supervision. In summary, 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 looked clean.

The FAA inspector reported one observation that, in his opinion, may have related to the vibration reported by the pilot. The FAA inspector stated that 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/operator.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR09LA085