No fatalities

7 Oct 2012: MUELLER MICHAEL WALTER CHALLENGER II CW SPC (N530MW) — Donald F Myers, Jr. — Sandwich, IL

Sandwich, IL, United States

On 7 Oct 2012, a MUELLER MICHAEL WALTER CHALLENGER II CW SPC (registration N530MW) operated by Donald F Myers, Jr. was involved in an aviation accident near Sandwich, IL. No fatalities were reported. Investigators recorded the probable cause as: Failure of the power takeoff lower rod bearing due to corrosion. This summary draws on records from NTSB.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On October 7, 2012, a Challenger II experimental aircraft suffered a total loss of engine power after takeoff and made a forced landing in a cornfield near Sandwich, Illinois. The pilot was not injured and the aircraft sustained minor damage. Investigation revealed corrosion-related bearing failure.

Accident Overview

On October 7, 2012, at approximately 1430 central daylight time, a Challenger II CW Experimental aircraft, registration N530MW, sustained minor damage during a forced landing near Sandwich, Illinois. The certificated private pilot, who owned and operated the aircraft, was not injured. The flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91 with no flight plan filed, and visual meteorological conditions prevailed.

According to pilot testimony, the airplane experienced a total loss of engine power after initial takeoff from Woodlake Landing Airport (IS65). The pilot conducted a forced landing into a cornfield off the departure end of the runway.

Aircraft and Engine Details

The aircraft was equipped with a Rotax 503 engine, serial number M5555721. This two-stroke, two-cylinder in-line engine is utilized with experimental, uncertificated aircraft and is no longer in production. The engine had accumulated a total of 163 hours over a nine-year period, having been operated infrequently. The owner had recently purchased the airplane and operated the engine for approximately four hours.

Investigation Findings

Examination of the engine revealed a failure of the power takeoff lower rod bearing due to corrosion. Debris from the lower rod bearing transferred through the transfer port to the top of the piston, damaging the piston and cylinder head. In addition, oil leaks around the cylinder head gasket were observed, as well as corrosion on two of the four cylinder head bolts, with one cylinder head bolt absent.

The Rotax operations manual directs short- and long-term engine preservation instructions, and the maintenance schedule directs an engine overhaul at 300 hours or five years, whichever comes first. According to the mechanic who performed the examination, the engine overhaul and preservation instructions were not accomplished.

Probable cause

Failure of the power takeoff lower rod bearing due to corrosion.

Contributing factors

Causes

Fatigue/wear/corrosion

Other contributing factors

Incorrect service/maintenance