Incident Overview

Date: Sunday 1 January 1950
Aircraft Type: Lockheed 414-08 Hudson IVA
Owner/operator: John Fairfax & Sons
Registration Number: VH-SMK
Location: near Camden Airport, NSW (CDU) – ÿ Australia
Phase of Flight: Initial climb
Status: Destroyed, written off
Casualties: Fatalities: 2 / Occupants: 2
Component Affected: Aircraft engine (no.2)Aircraft engine (no.2)
Investigating Agency: DCA AustraliaDCA Australia
Category: Accident
A Lockheed Hudson aircraft stalled and dived into the ground during a cargo flight from Camden to Dubbo, Australia, immediately after takeoff. Both occupants were killed due to a loss of control. The captain possessed an invalid license, but demonstrated competence as pilot-in-command. The takeoff weight exceeded the maximum permitted weight, and load distribution was not secured. The no.2 engine likely failed prior to impact, potentially contributing to the loss of control.A Lockheed Hudson aircraft stalled and dived into the ground during a cargo flight from Camden to Dubbo, Australia, immediately after takeoff. Both occupants were killed due to a loss of control. The captain possessed an invalid license, but demonstrated competence as pilot-in-command. The takeoff weight exceeded the maximum permitted weight, and load distribution was not secured. The no.2 engine likely failed prior to impact, potentially contributing to the loss of control.

Description

The Lockheed Hudson was engaged in a cargo flight to transport copies of The Sunday Herald newspaper from Camden to Dubbo, Australia. Immediately after takeoff, from a height of about 150 feet, the aircraft stalled and dived into the ground. Both occupants were killed. The investigation showed that the captain did not hold a valid license, but he was competent to act as pilot-in-command of the Hudson. It was not considered to be a factor in the accident. It was also found that the takeoff weight was 213-594 lbs over the maximum permitted weight. The load was correctly distributed, but not secured as required. CAUSE: Loss of control of the aircraft for reasons undetermined. The no.2 engine probably failed prior to impact with the ground and such failure, if it did occur, would be a possible contributory cause of the loss of control.

Source of Information

https://news.google.com/newspapers?id=9TFVAAAAIBAJ&sjid=G5MDAAAAIBAJ&hl=fr&pg=5918%2C357606https://news.google.com/newspapers?id=9TFVAAAAIBAJ&sjid=G5MDAAAAIBAJ&hl=fr&pg=5918%2C357606

Primary Cause

Loss of control due to a failed no.2 engine.Loss of control due to a failed no.2 engine.

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