4 fatalities

1984-05-30: Lockheed L-188 Electra (N5523) — Zantop International Airlines — Chalkhill, United States of America

Chalkhill, United States of AmericaFlight

On May 30, 1984, a Lockheed L-188 Electra (registration N5523) operated by Zantop International Airlines was involved in an aviation accident near Chalkhill, United States of America in flight. 4 people were killed. Investigators recorded the probable cause as: The aircraft's entry into an unusual attitude and the inability of the flight crew to analyze the flight condition before there was a complete loss of control. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 2 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781219491Data APIEditorial standards
Aircraft registered N5523
Aircraft registered N5523. Photo: Hunter Desportes / CC BY 2.0, via Wikimedia Commons

Zantop Flight 931 experienced a gyro malfunction and unusual attitude, leading to an in-flight breakup near the Dryer VOR. The probable cause was loss of control due to crew inability to analyze the flight condition, with a possible gyro system failure.

Departure and Initial Flight

Zantop Flight 931 was loaded with cargo at 00:40, with all cargo bulk loaded and tied down on the right side of the airplane for the full length of the cargo compartment. The flight departed the gate at Baltimore/Washington International Airport at 01:05 and took off on runway 28 at 01:10. At 01:11:42, the flight contacted Baltimore departure control and was cleared to 13,000 feet. After switching to Washington ARTCC, the flight was cleared further to flight level 220.

Gyro Malfunction

At 01:32, a No. 2 gyro malfunction prompted the crew to select the No. 1 gyro to drive both approach horizons, and the problem appeared resolved. At 01:43:09, Cleveland ARTCC cleared Flight 931 direct to the Dryer VOR. After the turn to the Dryer VOR, the first officer’s approach horizon may have displayed incorrect pitch and roll information. The flightcrew may have received conflicting pitch and roll information from the two approach horizons as they attempted to recover from an unusual attitude.

Loss of Control and Breakup

The flightcrew overstressed the airplane in an attempt to recover from the unusual attitude as the aircraft spiraled down. The Electra broke up, and falling wreckage damaged some houses; however, most of the wreckage fell in uninhabited, wooded areas.

Probable Cause

The official probable cause states: The aircraft's entry into an unusual attitude and the inability of the flight crew to analyze the flight condition before there was a complete loss of control. Although the precise reason for the loss of control was not identified, an undetermined failure of a component in the No.2 vertical gyro system, perhaps involving the amplifier and associated circuitry, probably contributed to the cause of the accident by incorrectly processing data to the co-pilot's approach horizon. The in-flight structural failure of the aircraft was due to overload.