6 fatalities

1977-05-14: Boeing 707 (G-BEBP) — IAS Cargo Airlines — Lusaka, Zambia

Lusaka, ZambiaLanding (descent or approach)

On May 14, 1977, a Boeing 707 (registration G-BEBP) operated by IAS Cargo Airlines was involved in an aviation accident near Lusaka, Zambia during landing or approach. 6 people were killed. Investigators recorded the probable cause as: The accident was caused by a loss of pitch control following the in-flight separation of the right hand horizontal stabilizer and elevator as a result of a combination of metal fatigue and inadequate failsafe design in the rear spar structure. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781227973Data APIEditorial standards
Aircraft registered G-BEBP
Aircraft registered G-BEBP. Photo: stevefowler747 / CC BY-SA 2.0, via Wikimedia Commons

A cargo flight from London to Lusaka crashed after the right horizontal stabilizer and elevator separated in flight, killing all six occupants.

Incident Overview

On the final leg of a cargo flight from London to Lusaka, with intermediate stops in Athens and Nairobi, the aircraft was conducting a visual approach to runway 10 at Lusaka. The flight from Nairobi had been uneventful. After receiving clearance to descend to FL70 in 1,000-foot steps, the copilot reported the airfield in sight at 09:28. Lusaka control then cleared the aircraft to descend to 6,000 feet (2,221 feet above runway elevation) and shortly thereafter authorized a visual approach for runway 10. At 09:32, flaps were selected to 50°.

Inflight Separation

At 09:33, the complete right-hand horizontal stabilizer and elevator assembly was observed to separate from the aircraft in flight. Immediately, the aircraft pitched rapidly nose-down and dived vertically into the ground from a height of approximately 800 feet. The main wreckage was located 3,660 meters from the runway threshold. The aircraft was totally destroyed, and all six occupants were killed.

Investigation Findings

The official investigation determined that the accident was caused by a loss of pitch control following the in-flight separation of the right-hand horizontal stabilizer and elevator. This separation resulted from a combination of metal fatigue and inadequate failsafe design in the rear spar structure. Additionally, shortcomings in design assessment, certification, and inspection procedures were identified as contributory factors.

Probable cause

The accident was caused by a loss of pitch control following the in-flight separation of the right hand horizontal stabilizer and elevator as a result of a combination of metal fatigue and inadequate failsafe design in the rear spar structure. Shortcomings in design assessment, certification and inspection procedures were contributory factors.