In-flight breakup of Zantop International Airlines Electra near Cleveland

4 fatalities • Chalkhill, United States of America • Flight

A Zantop International Airlines Lockheed Electra experienced an in-flight structural failure following an unusual attitude and subsequent loss of control during the climb phase.

What happened

Following the completion of cargo loading at Baltimore/Washington International Airport, Flight 931 departed the gate at 0-40 and took off from runway 28 at 01:10. The aircraft, a Lockheed Electra, initially received clearance to climb to 13,000 feet before being cleared further to FL220 by Washington ARTCC.

At approximately 01:32, the crew identified a malfunction involving the number 2 gyro. To address this, they switched to using the number 1 gyro to drive both approach horizons, which initially appeared to resolve the issue. Shortly after being cleared direct to the Dryer VOR by Cleveland ARTCC, the aircraft entered a turn.

During this maneuver, the first officer's approach horizon may have provided inaccurate pitch and roll data. This likely resulted in the flightcrew receiving conflicting information from the two horizons while attempting to correct an unusual attitude. In the process of trying to recover the aircraft, the crew overstressed the airframe, leading to a spiral descent. The Lockheed Electra broke apart in mid-air; while some debris struck residential structures, the majority of the wreckage landed in unpopulated, wooded terrain.

Findings

Investigations into the accident focused on the inability of the crew to properly assess the flight condition before a total loss of control occurred. A failure within the number 2 vertical gyro system—potentially involving the amplifier or related circuitry—is believed to have provided incorrect data to the co-pilot's approach horizon. The structural disintegration of the aircraft was caused by aerodynamic overstress during the recovery attempt.

Probable cause

The crew's inability to identify an unusual attitude, compounded by erroneous instrument data from a malfunctioning gyro system, led to an aerodynamic overload that broke up the aircraft.

Frequently asked questions

What happened in the 1984-05-30 Lockheed L-188 Electra accident near Chalkhill, United States of America?

A Zantop International Airlines Lockheed Electra experienced an in-flight structural failure following an unusual attitude and subsequent loss of control during the climb phase.

Were there any fatalities in the 1984-05-30 Lockheed L-188 Electra accident?

The accident was fatal, resulting in 4 fatalities.

What aircraft was involved and where did it happen?

The accident on 1984-05-30 involved a Lockheed L-188 Electra, registration N5523, operated by Zantop International Airlines, at Chalkhill, United States of America.

What was the probable cause of the accident?

The crew's inability to identify an unusual attitude, compounded by erroneous instrument data from a malfunctioning gyro system, led to an aerodynamic overload that broke up the aircraft.

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