No fatalities

1997-08-19: Swearingen SA226 Metro II (N224AM) — Superior Aviation — Des Moines, United States of America

Des Moines, United States of AmericaLanding (descent or approach)

On August 19, 1997, a Swearingen SA226 Metro II (registration N224AM) operated by Superior Aviation was involved in an aviation accident near Des Moines, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The pilot's improper in-flight planning/decision and failure to perform the emergency procedure for shut-down of the right engine. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 7 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781205869Data APIEditorial standards

During a landing approach, the right engine remained at high power. The pilot performed a missed approach, then a second landing, but lost directional control, went off the runway, and struck the localizer antenna. The power control cable had disconnected.

Incident Overview

During a landing approach, the pilot observed that the right engine remained at a high power setting when he moved the power levers to reduce power. He executed a missed approach and experienced difficulty keeping the airplane straight and level. Subsequently, he maneuvered for a second approach to land. After touchdown, the pilot could not maintain directional control of the airplane. He attempted a go-around, but the airplane departed the end of the runway and impacted the localizer antenna. The pilot did not advise air traffic control of the problem nor did he declare an emergency.

Pilot's Operating Handbook Procedures

The Pilot's Operating Handbook (POH) stated that for a power plant control malfunction, the affected engine should be shut down and a single-engine landing should be made. The pilot did not follow this procedure.

Mechanical Findings

Examination revealed that the power control cable was disconnected from its anchoring point. A safety tab was broken off the housing, allowing the housing to unscrew. Approximately one month before the accident, maintenance had been performed on the right engine to correct a discrepancy regarding a stiff power lever. The mechanic re-rigged the right engine power cable during that maintenance.

Probable Cause

The official probable cause was the pilot's improper in-flight planning/decision and failure to perform the emergency procedure for shutdown of the right engine. Factors relating to the accident were the power lever cable becoming disconnected from the fuel control unit due to improper maintenance, and reduced directional control of the airplane when one engine remained at a high power setting.