No fatalities

2 Jan 2011: PIPER PA-18-180 (N6774B) — UNITED STATES DEPARTMENT AGRICULTURE — Shoshoni, WY

Shoshoni, WY, United States

On 2 Jan 2011, a PIPER PA-18-180 (registration N6774B) operated by UNITED STATES DEPARTMENT AGRICULTURE was involved in an aviation accident near Shoshoni, WY. No fatalities were reported. Investigators recorded the probable cause as: A total loss of engine power for undetermined reasons. This summary draws on records from NTSB; 4 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On January 2, 2011, a Piper PA-18-180 experienced a gear collapse during a forced landing near Shoshoni, Wyoming. The pilot and passenger were uninjured; the aircraft sustained substantial damage. The engine power loss cause remains undetermined.

Accident Details

On January 2, 2011, at approximately 1315 mountain standard time, a Piper PA-18-180, registration N6774B, sustained substantial damage during a forced landing about 10 miles southeast of Shoshoni, Wyoming. The commercial pilot and his passenger were not injured. The aircraft was owned by STP Aviation LLP and operated by the United States Department of Agriculture. The flight was a local Public Use wildlife aerial observation mission, which had departed Riverton Municipal Airport, Riverton, Wyoming, about four hours earlier. Visual meteorological conditions prevailed, and no flight plan had been filed.

Forced Landing

According to the pilot, during the aerial observation flight, the engine suddenly stopped producing power. He checked the fuel selector, applied carburetor heat, ensured the magneto switch was set to both, and attempted to restart the engine. The engine did not restart, prompting the pilot to execute a forced landing on rough, brush-covered terrain. Although the touchdown was successful, during the landing roll, the airplane went off a low bank. Upon contacting the terrain at the bottom of the bank, the main landing gear support structure failed, causing both gear struts to fold outward. The left wing lift strut was bent to the extent that it required replacement.

Postaccident Investigation

A postaccident examination of the airplane's fuel system revealed that more than one hour of fuel (10+ gallons) remained. The engine was test run for several minutes with no anomalies detected. The investigation also determined that the ambient temperature (10 degrees Fahrenheit) and dew point (1 degree Fahrenheit) were outside the range at which carburetor icing would be expected in maneuvering flight. No other fuel system or engine anomalies were found, and the reason for the loss of engine power could not be determined.

Contributing factors

Contributed to outcome