Incident Overview

Date: Monday 26 October 2015
Aircraft Type: Boeing 737-4L7
Owner/operator: British Airways, opb Comair
Registration Number: ZS-OAA
Location: Johannesburg-O.R. Tambo International Airport (JNB) – ÿ South Africa
Phase of Flight: Landing
Status: Substantial, written off
Casualties: Fatalities: 0 / Occupants: 100
Component Affected: Left Main Gear, Shimmey Damper Thermal Relief Valve, Torsion Link BushesLeft Main Gear, Shimmey Damper Thermal Relief Valve, Torsion Link Bushes
Investigating Agency: CAA S.A.CAA S.A.
Category: Accident
A Boeing 737-400, operated by Comair, experienced a severe landing accident at Johannesburg-OR Tambo Airport on 08:20 UTC due to a combination of factors during approach. The aircraft, flight BA6234, was cleared for landing on runway 03R. The first officer initiated a high-speed flare, exceeding recommended procedures. This resulted in a low sink rate and excessive vibrations, leading to a significant ground speed increase and a collapse of the left main gear. The aircraft rolled slightly, and eventually came to a complete stop, resting on its left landing gear and engine, with the nose landing gear in the air. The thermal relief valve malfunctioned, contributing to the vibration. The initial flare and low sink rate caused excessive vibrations, ultimately leading to the failure of the shimmy damper’s torsion link and subsequent vibration build-up.A Boeing 737-400, operated by Comair, experienced a severe landing accident at Johannesburg-OR Tambo Airport on 08:20 UTC due to a combination of factors during approach. The aircraft, flight BA6234, was cleared for landing on runway 03R. The first officer initiated a high-speed flare, exceeding recommended procedures. This resulted in a low sink rate and excessive vibrations, leading to a significant ground speed increase and a collapse of the left main gear. The aircraft rolled slightly, and eventually came to a complete stop, resting on its left landing gear and engine, with the nose landing gear in the air. The thermal relief valve malfunctioned, contributing to the vibration. The initial flare and low sink rate caused excessive vibrations, ultimately leading to the failure of the shimmy damper’s torsion link and subsequent vibration build-up.

Description

A Boeing 737-400, operated by Comair on behalf of British Airways, sustained severe damage in a landing accident at Johannesburg-OR Tambo Airport, South Africa. There were 94 passengers and six crew members on board. The aircraft, flight number BA6234, departed Port Elizabeth Airport at 08:20 UTC on an instrument flight plan rule for Johannesburg. The first officer was the flying pilot for this leg. During approach to Johannesburg the aircraft was cleared for landing on runway 03R. The approach was flown with a tailwind (340ø at 10 knots). After crossing the runway threshold, the first officer began flaring the aircraft at 65 feet instead of 20 feet as recommended by Boeing. This contributed to a low sink rate (1.8 feet/second). The aircraft touched down at an excessive ground speed of 167 knots. The flight crew felt the aircraft vibrating, during which they applied brakes and deployed the reverse thrust. The left main gear collapsed approximately 5 seconds after touchdown, causing the aircraft to roll slightly low to the left. It later came to full stop around 35 seconds later, slightly left of the runway centreline, resting on its right main landing gear and the number one engine, with the nose landing gear in the air. The aircraft sustained substantial damage as the number one engine scraped along the runway surface when the landing gear detached from the fuselage. The occupants were allowed to disembark from the aircraft via the left aft door due to the attitude in which the aircraft came to rest. It was determined that the early flare and low sink rate on touchdown caused a condition in which excessive vibrations build up on the left landing gear and resulted in the upper torsion link failure. The thermal relief valve of the shimmy damper contained oil which could have impaired its effectiveness Significant wear was found on the upper torsion link bushes, which could have contributed with the un-dampened vibration build up during operation. Probable Cause: Unstable approach whereby the aircraft was flared too high with high forward speed resulting with a low sink rate in which during touch down the left landing gear experienced excessive vibration and failed due to shimmy events.

Primary Cause

Unstable approach due to a high-speed flare, resulting in a low sink rate and excessive vibrations.Unstable approach due to a high-speed flare, resulting in a low sink rate and excessive vibrations.

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