No fatalities

2003-04-15: Swearingen SA226 Metro II (N229AM) — Superior Aviation — Denver-Intl, United States of America

Denver-Intl, United States of AmericaLanding (descent or approach)

On April 15, 2003, a Swearingen SA226 Metro II (registration N229AM) operated by Superior Aviation was involved in an aviation accident near Denver-Intl, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: The failure of the landing gear system and the flight crew's failure to ascertain that the landing gear was down and locked. A contributing factor was the inadequate maintenance inspections performed by maintenance personnel. 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 1781201135Data APIEditorial standards

An aircraft landed with its landing gear retracted after a malfunction. The crew, following a heavy jet, had noted recurring gear unsafe indications. Postaccident examination found the main gear stowed.

Incident Summary

An aircraft executed a wheels-up landing after its landing gear failed to extend properly. The incident occurred during an approach behind a heavy jet, prompting the crew to fly a slightly higher path to avoid wake turbulence.

Flight Details

The first officer, handling the controls, called for landing gear extension. When the captain moved the gear handle down, red in-transit lights illuminated. The captain recycled the gear, but the lights persisted. Consulting the emergency checklist, the captain believed he had manually extended the gear after hearing a normal "clunk feel" and observing a decrease in airspeed. Additionally, the gear unsafe warning horn did not sound when power was reduced to flight idle. The first officer concurred, noting 2,000 pounds of hydraulic pressure.

Landing Gear Issues

The crew had previously experienced recurring gear unsafe indications, which had been attributed to a frozen squat switch in the wheel well. Despite this history, the aircraft proceeded to land with the gear retracted.

Postaccident Examination

After the landing, examination revealed that the nose gear had partially extended, but the main landing gear remained fully retracted. Propeller blade fragments had penetrated the fuselage, breaching the pressure vessel.

Probable cause

The failure of the landing gear system and the flight crew's failure to ascertain that the landing gear was down and locked. A contributing factor was the inadequate maintenance inspections performed by maintenance personnel.