Incident Overview

Date: Wednesday 22 November 1961
Aircraft Type: Douglas C-47A-75-DL (DC-3)
Owner/operator: Rhodesian Air Services
Registration Number: VP-YRX
Location: Salisbury Airport (HRE) – ÿ Zimbabwe
Phase of Flight: Approach
Status: Destroyed, written off
Casualties: Fatalities: 2 / Occupants: 3
Component Affected: Aircraft structure (right wing, propeller, fuselage)Aircraft structure (right wing, propeller, fuselage)
Category: Accident
A DC-3 aircraft, en route from Salisbury, Zimbabwe to Livingstone, Zambia, experienced a critical incident during takeoff. The right wing dipped, followed by a left turn with the 1st propeller windmill, and subsequent inverted landing. The pilot’s actions, including incorrect rudder trim and failure to correct the aircraft’s critical speed yaw, contributed to the incident.A DC-3 aircraft, en route from Salisbury, Zimbabwe to Livingstone, Zambia, experienced a critical incident during takeoff. The right wing dipped, followed by a left turn with the 1st propeller windmill, and subsequent inverted landing. The pilot’s actions, including incorrect rudder trim and failure to correct the aircraft’s critical speed yaw, contributed to the incident.

Description

The DC-3 took off from Salisbury, now Harare, to pick up United Nations troops at Livingstone. After takeoff the right wing dipped. After a slow recovery, it climbed away to 100-150 feet and then went into a turn to the left with the no. 1 prop windmilling. The turn steepened until the DC-3 rolled over and dived inverted to the ground some 600yds southeast of the threshold of runway 06. PROBABLE CAUSE: “Failure of the pilot to execute a successful single-engine forced landing after concluding that there had been a power loss in the port engine. Evidence indicated that a failure of the port engine did not, in fact, occur. The pre-takeoff rudder trimmer check was not carried out correctly as laid down in the checklist, and the aircraft took off with full left rudder trim applied. Once airborne this was misinterpreted as port engine failure, and the port propeller was feathered. No apparent action was taken by the pilot to correct the ensuing critical speed yaw.”

Primary Cause

Pilot error ? failure to execute a successful single-engine forced landing after concluding a power loss in the port engine, despite evidence indicating the port engine did not fail.Pilot error ? failure to execute a successful single-engine forced landing after concluding a power loss in the port engine, despite evidence indicating the port engine did not fail.

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