8 fatalities

1980-07-21: Cessna 404 Titan (N2683S) — Scenic Airlines — Grand Canyon, United States of America

Grand Canyon, United States of AmericaTakeoff (climb)

On July 21, 1980, a Cessna 404 Titan (registration N2683S) operated by Scenic Airlines was involved in an aviation accident near Grand Canyon, United States of America during takeoff. 8 people were killed. Investigators recorded the probable cause as: The probable cause of the accident was a substantial loss of power from the left engine at a critical point in the takeoff an the failure of the pilot to establish a minimum drag configuration which degraded the marginal single-engine climb performance of the… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 3 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781223728Data APIEditorial standards

Scenic Airlines Flight 306, a Cessna 404 commuter flight, crashed after takeoff from Grand Canyon National Park Airport. The aircraft was destroyed by impact and fire. The pilot and six passengers were killed; one passenger later died from thermal injuries. The probable cause was left engine power loss and failure to establish minimum drag configuration.

Accident

At 1702, Scenic Airlines Flight 306, a Cessna 404 operating under visual flight rules as a commuter flight to Phoenix, crashed approximately three miles south of runway 21 after departing from Grand Canyon National Park Airport. The aircraft traveled through a densely wooded area while maintaining a magnetic heading of 165 degrees. It came to rest upright about 230 feet from the initial point of contact with trees. The impact forces and an intense fire destroyed the aircraft.

Casualties

The accident resulted in the deaths of the pilot and six of the seven passengers. One passenger initially survived but succumbed to thermal injuries five days later.

Probable Cause

According to the official investigation, the probable cause was a substantial loss of power from the left engine at a critical point in the takeoff and the pilot's failure to establish a minimum drag configuration, which degraded the marginal single-engine climb performance of the aircraft. The power loss was attributed to the seizure of the turbocharger following a progressive failure of the turbine wheel blades. This failure was initiated by foreign object ingestion that had occurred prior to the flight and was not detected during maintenance performed on the engine four days before the accident.