Incident Overview

Date: Tuesday 14 January 1969
Aircraft Type: BAC One-Eleven 201AC
Owner/operator: British United Airways – BUA
Registration Number: G-ASJJ
Location: Milano-Linate – ÿ Italy
Phase of Flight: Initial climb
Status: Destroyed, written off
Casualties: Fatalities: 0 / Occupants: 33
Component Affected: The aircraft’s engine system, specifically the compressor and throttle control system.The aircraft’s engine system, specifically the compressor and throttle control system.
Category: Accident
A BAC One-Eleven aircraft, G-ASJJ, experienced a sudden and catastrophic loss of control during takeoff, resulting in a forced landing. A captain reported a compressor bang immediately after takeoff, prompting a throttle adjustment. The pilot-in-command subsequently reduced the throttle and lowered the nose pitch, but the crew?s error in closing the throttle led to a loss of thrust, ultimately causing the crash.A BAC One-Eleven aircraft, G-ASJJ, experienced a sudden and catastrophic loss of control during takeoff, resulting in a forced landing. A captain reported a compressor bang immediately after takeoff, prompting a throttle adjustment. The pilot-in-command subsequently reduced the throttle and lowered the nose pitch, but the crew?s error in closing the throttle led to a loss of thrust, ultimately causing the crash.

Description

The BAC One-Eleven, G-ASJJ, started the takeoff run from runway 18 and accelerated normally until a bang was heard immediately after takeoff. A captain on the jumpseat (who was supervising the route experience of the co-pilot during the flight), commented that he thought it was the no. 1 engine and advised to close the throttle a little later. The pilot-in-command then closed the throttle and lowered the nose from 12deg to 6deg pitch. The engine was shut down and the airspeed decreased from 140 knots to 115 knots. A forced landing was eventually carried out. PROBABLE CAUSE: “The accident must be attributed to a combination of factors following a compressor bang/surge in no. 2 engine immediately after takeoff and the aircraft crashed because the crew, after fully closing no. 1 throttle in error, failed to recognise their mistake and, in addition, were not aware that the thrust of no. 2 engine had also been partially reduced after an inadvertent displacement of the relevant throttle lever.”

Primary Cause

Compressor surge/bang in the second engine immediately after takeoff, followed by crew error in throttle control and loss of thrust.Compressor surge/bang in the second engine immediately after takeoff, followed by crew error in throttle control and loss of thrust.

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