No fatalities

10 Mar 2015: MAULE M 7-260C 260C (N55000) — Oregon, MO

Oregon, MO, United States

On 10 Mar 2015, a MAULE M 7-260C 260C (registration N55000) was involved in an aviation accident near Oregon, MO. No fatalities were reported. Investigators recorded the probable cause as: Engine vibration for reasons that could not be determined based on the available evidence. 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

On March 10, 2015, a Maule M7 (N55000) nosed over during a precautionary landing near Oregon, Missouri, after a partial loss of engine power. The pilot was not injured. The airplane sustained substantial damage to the vertical stabilizer and rudder.

Accident Details

On March 10, 2015, about 1210 central daylight time, a Maule M7 airplane, registration N55000, sustained substantial damage when it nosed over during a precautionary landing near Oregon, Missouri. The event occurred after a partial loss of engine power during cruise flight. The pilot was not injured. The airplane sustained substantial damage to the vertical stabilizer and rudder.

The aircraft was registered to Aardvark Aircraft Acquisition LLC and operated by the pilot under 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed, and the flight was not on a flight plan. The flight originated from North Omaha Airport (3NO), Omaha, Nebraska, about 1125, and was destined for Rosecrans Memorial Airport (STJ), St. Joseph, Missouri.

Pilot Report

The pilot reported that after climbing to cruise altitude and leaning the engine, he noted an unusual engine vibration. He responded by enriching the fuel mixture slightly above normal, and the vibration seemed to improve. After descending and increasing power to level off, the engine vibration became "much worse," prompting the pilot to perform an off-airport precautionary landing. The landing was normal, but during the landing roll, the main landing gear "dug in" and the airplane nosed over.

Postaccident Examination

Postaccident examination of the airplane did not reveal any preimpact anomalies. The engine fuel servo, flow divider, and nozzles were sent to the manufacturer's facility for testing under the direct supervision of NTSB investigators. The flow divider was tested and met all production test standards. The fuel nozzles were not flow tested but did not show any evidence of obstruction. The fuel servo was tested on the manufacturer's flow bench, and the measured fuel flow rates were about 1.5 pounds per hour (1/4 gallon per hour) leaner than specified service limits.