Incident Overview

Date: Thursday 21 February 1980
Aircraft Type: Beechcraft 200 Super King Air
Owner/operator: Advance Airlines
Registration Number: VH-AAV
Location: Sydney-Kingsford Smith International Airport, NSW (SYD) – ÿ Australia
Phase of Flight: Approach
Status: Destroyed, written off
Casualties: Fatalities: 13 / Occupants: 13
Component Affected: Aircraft engine and control systems.Aircraft engine and control systems.
Category: Accident
A Beechcraft 200 Super King Air aircraft collided with the western sea wall at Sydney-Kingsford Smith International Airport, resulting in a catastrophic accident involving multiple fatalities. The aircraft broke apart during impact, and an explosive fire ensued. The incident occurred approximately 106 seconds after takeoff from runway 25, targeting a scheduled flight to Temora Airport.A Beechcraft 200 Super King Air aircraft collided with the western sea wall at Sydney-Kingsford Smith International Airport, resulting in a catastrophic accident involving multiple fatalities. The aircraft broke apart during impact, and an explosive fire ensued. The incident occurred approximately 106 seconds after takeoff from runway 25, targeting a scheduled flight to Temora Airport.

Description

A Beechcraft 200 Super King Air aircraft, registered VH-AAV, collided with the western sea wall enclosing the extension of runway 16/34, abeam the runway 34 threshold, at Sydney-Kingsford Smith International Airport, NSW (SYD). The aircraft broke apart on impact and there was an explosive fire. The pilot and all twelve passengers were killed. The accident occurred approximately 106 seconds after the aircraft had commenced takeoff from runway 25, on a scheduled flight to Temora Airport, NSW (TEM). The cause of the accident has not been determined, but the most likely explanation is that the aircraft was operated in a reduced power configuration which, under the prevailing conditions, rendered its single-engine performance critical in respect to aircraft handling.

Primary Cause

Reduced power configuration under prevailing conditions resulted in single-engine performance critical, leading to aircraft handling difficulties.Reduced power configuration under prevailing conditions resulted in single-engine performance critical, leading to aircraft handling difficulties.

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