Elevator control cable failure leads to aircraft crash landing

1 fatality • Tau, Samoa Islands (Western Samoa) • Landing (descent or approach)

An aircraft experienced a total loss of elevator control due to a corroded cable during its final approach, resulting in a collision with a terminal building.

What happened

During the final approach phase of flight, approximately 300 feet above ground level, the aircraft experienced a critical failure of the elevator down control cable. In an attempt to manage the pitch of the aircraft type following the loss of control, the pilot utilized engine power and flap settings to maintain semi-stable flight. However, as the aircraft descended to roughly 50 feet above ground level, it entered a stall condition.

During this uncontrolled descent, the left wing of the aircraft struck the roof of a terminal building. The impact resulted in a crash landing at the site.

Findings

Investigations into the mechanical failure revealed that the elevator control cable had separated due to corrosion. While no evidence of fatigue cracking or mechanical wear was identified on the components, corrosion products were present within two inches of the separation point on both segments of the broken cable.

As a result of this incident, the operating company has initiated a fleet-wide maintenance change. The operator is replacing existing steel control cables with stainless steel alternatives to improve resistance to corrosion. Additionally, the mandatory inspection interval for these components is being reduced from 800 hours to 100 hours to ensure earlier detection of potential degradation.

Probable cause

The total failure of the elevator control system was caused by the corrosion-induced separation of the elevator down control cable.

Frequently asked questions

What happened in the 1984-07-21 De Havilland DHC-6 Twin Otter accident near Tau, Samoa Islands (Western Samoa)?

An aircraft experienced a total loss of elevator control due to a corroded cable during its final approach, resulting in a collision with a terminal building.

Were there any fatalities in the 1984-07-21 De Havilland DHC-6 Twin Otter accident?

The accident was fatal, resulting in 1 fatality.

What aircraft was involved and where did it happen?

The accident on 1984-07-21 involved a De Havilland DHC-6 Twin Otter, registration N43SP, operated by South Pacific Island Airways - SPIA, at Tau, Samoa Islands (Western Samoa).

What was the probable cause of the accident?

The total failure of the elevator control system was caused by the corrosion-induced separation of the elevator down control cable.

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