Fatal crash of twin-engine aircraft near Davenport Airport

6 fatalities • Davenport, United States of America • Landing (descent or approach)

A twin-engine airplane crashed in an open field near Davenport Airport after the right wing detached during its approach.

What happened

During the final approach to Davenport Airport, a twin-engine aircraft experienced a catastrophic structural failure when the right wing separated from the fuselage. Following the detachment of the wing, the aircraft became uncontrollable and descended into an open field situated several miles away from the airfield. The impact resulted in the total destruction of the airframe. There were no survivors among the six fatalities recorded on board.

Findings

Investigations into the accident identified the primary cause as a structural failure of the right wing during the descent phase. The failure was attributed to fatigue cracks within the airframe, specifically affecting the wing spars. Technical analysis revealed a pre-existing crack on the lower spar cap (WS-81) that had remained undetected for approximately six years. This condition was exacerbated by inadequate inspections performed by maintenance personnel, which allowed the fracture to progress until the right wing folded upward and detached from the aircraft.

Probable cause

The structural failure of the right wing was caused by fatigue cracks in the wing spars that went undetected during maintenance inspections.

Frequently asked questions

What happened in the 1973-04-19 Beechcraft E18 accident near Davenport, United States of America?

A twin-engine airplane crashed in an open field near Davenport Airport after the right wing detached during its approach.

Were there any fatalities in the 1973-04-19 Beechcraft E18 accident?

The accident was fatal, resulting in 6 fatalities.

What aircraft was involved and where did it happen?

The accident on 1973-04-19 involved a Beechcraft E18, registration N310WA, operated by Air Iowa, at Davenport, United States of America.

What was the probable cause of the accident?

The structural failure of the right wing was caused by fatigue cracks in the wing spars that went undetected during maintenance inspections.

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