Incident Overview

Date: Saturday 23 May 1964
Aircraft Type: Vickers 701 Viscount
Owner/operator: Cambrian Airways
Registration Number: G-AMON
Location: near Barcelona – ÿ Spain
Phase of Flight: En route
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants: 63
Component Affected: The propeller.The propeller.
Category: Accident
A British Airways Airbus A340-300 aircraft experienced a catastrophic event while cruising over the Mediterranean Sea. The captain detected a significant engine synchronization issue, resulting in rapidly decreasing RPM and a low jet pipe temperature. A sudden, rapid increase in RPM caused the propeller to break away, resulting in a large puncture in the fuselage, causing an explosive decompression. The incident was resolved with an emergency landing at Barcelona.A British Airways Airbus A340-300 aircraft experienced a catastrophic event while cruising over the Mediterranean Sea. The captain detected a significant engine synchronization issue, resulting in rapidly decreasing RPM and a low jet pipe temperature. A sudden, rapid increase in RPM caused the propeller to break away, resulting in a large puncture in the fuselage, causing an explosive decompression. The incident was resolved with an emergency landing at Barcelona.

Description

While the aircraft was cruising at FL190, about three hours after leaving Cardiff-Rhoose Airport, for Palma de Mallorca Airport the captain noticed that no. 2 engine was de-synchronized, as compared with no’s 3 and 4, and its rpm were rapidly decreasing. He then heard a “thump”, and saw that the jet pipe temperature on no.2 engine was low. At this time, a sudden, and very rapid, increase in no. 2 engine rpm occurred; before propeller feathering action could be completed, the propeller broke away and punctured the fuselage, causing an explosive decompression. There was no fire but fire drill was carried out as a precaution. An emergency landing was made at Barcelona, without further incident. The puncture in the fuselage proved to be a gash about 5 to 6 ft . long and 6 ins. wide in line with the port forward toilet. It was later established that failure or a tooth in the reduction gear led to disruption or the reduction gear casing, and this in turn led to the shedding of the propeller.

Primary Cause

Failure or a tooth in the reduction gear, resulting in disruption or the reduction gear casing, leading to the shedding of the propeller.Failure or a tooth in the reduction gear, resulting in disruption or the reduction gear casing, leading to the shedding of the propeller.

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