Incident Overview

Date: Tuesday 23 March 2004
Aircraft Type: Beechcraft 200C Super King Air
Owner/operator: Northern Territory Medical Service
Registration Number: VH-NTH
Location: Darwin Airport, NT (DRW) – ÿ Australia
Phase of Flight: Landing
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 2
Component Affected: Left main landing gear drive shaftLeft main landing gear drive shaft
Category: Accident
A Beech 200 aircraft took off from Katherine, Australia, and experienced a catastrophic landing due to a severed landing gear drive shaft caused by wear and tear on a jubilee clamp tail. The pilot reported a lack of green ‘down and locked’ indication, leading to an emergency landing, and the aircraft subsequently collapsed during touchdown.A Beech 200 aircraft took off from Katherine, Australia, and experienced a catastrophic landing due to a severed landing gear drive shaft caused by wear and tear on a jubilee clamp tail. The pilot reported a lack of green ‘down and locked’ indication, leading to an emergency landing, and the aircraft subsequently collapsed during touchdown.

Description

Shortly after take-off from Katherine, Australia, the left main landing gear of the Beech 200 aircraft did not retract. The flight continued to Darwin with the landing gear extended. During approach to Darwin airport the pilot advised air traffic control that he could not obtain a green ‘down and locked’ indication for the left main landing gear, and declared an emergency prior to landing. During touchdown, the left main landing gear collapsed and the aircraft slewed off the runway. Both occupants evacuated the aircraft with no injuries. The aircraft operator’s maintenance organisation examined the aircraft and found that the left main landing gear drive shaft had severed as a result of fretting against a bleed air duct clamp tail. The bleed air duct clamp (jubilee clamp) had been fitted to the aircraft during an aircraft refurbishment program in September 2003. The jubilee clamp tail had been fastened in close proximity to the landing gear drive shaft. Subsequently, the jubilee clamp tail had come into close contact with the drive shaft, leading to severe wear of the drive shaft section and eventual failure.

Source of Information

https://www.atsb.gov.au/publications/investigation_reports/2004/aair/aair200401024/https://www.atsb.gov.au/publications/investigation_reports/2004/aair/aair200401024/

Primary Cause

Wear and tear on the jubilee clamp tail caused by contact with a bleed air duct clamp, resulting in severe shaft wear and failure.Wear and tear on the jubilee clamp tail caused by contact with a bleed air duct clamp, resulting in severe shaft wear and failure.

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