Incident Overview

Date: Wednesday 23 February 1955
Aircraft Type: Douglas C-47B-15-DK (DC-3)
Owner/operator: Central African Airways
Registration Number: VP-YKO
Location: Salisbury-Belvedere Airport – ÿ Zimbabwe
Phase of Flight: Initial climb
Status: Destroyed, written off
Casualties: Fatalities: 1 / Occupants: 26
Component Affected: Port engine rocker box hose.Port engine rocker box hose.
Category: Accident
Central African Airways Flight 626 experienced a catastrophic accident due to smoke entering the cockpit shortly after takeoff. The pilot-in-command initiated an immediate belly landing, resulting in propeller failure and a collision with a railway line. A fractured rubber hose on the port engine rocker box connecting it to the collector box caused smoke to travel through the wheel bay and interior of the centre section, generating smoke that spread to the flight crew compartment via the air intake. Subsequent investigation revealed this as the primary cause.Central African Airways Flight 626 experienced a catastrophic accident due to smoke entering the cockpit shortly after takeoff. The pilot-in-command initiated an immediate belly landing, resulting in propeller failure and a collision with a railway line. A fractured rubber hose on the port engine rocker box connecting it to the collector box caused smoke to travel through the wheel bay and interior of the centre section, generating smoke that spread to the flight crew compartment via the air intake. Subsequent investigation revealed this as the primary cause.

Description

Central African Airways Flight 626 had just lifted off runway 09 at Salisbury when smoke entered the cockpit. The gear had just been retracted, but the pilot-in-command decided to belly land the aircraft immediately on the remaining runway. The propellers broke off. The no. 1 prop sliced through the fuselage, killing the flight engineer. The DC-3 overran the runway and came to rest across a railway line. PROBABLE CAUSE: “The cause of the accident was the presence of smoke in the flight crew compartment in sufficient quantity to make the captain apprehensive of fire and to cause him to land the aircraft immediately with the undercarriage retracted. The only defect revealed by subsequent investigation of the airframe, engine and accessories, was a fractured rubber hose on the port engine connecting the rocker box of one of the lower cylinders to the collector box. It is the option of the Investigating Officers that oil leaking from this fracture was carried by the airflow on to the exhaust collector ring and generated smoke. Tests carried out later on the same type of aircraft proved conclusively that smoke generated in this region will travel freely to the flight crew compartment via the wheel bay and interior of the centre section leading edge.”

Primary Cause

Smoke in the flight crew compartment caused apprehension regarding fire, prompting immediate landing.Smoke in the flight crew compartment caused apprehension regarding fire, prompting immediate landing.

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