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Printed page 4. PDF page 16.
minute until the commander reduced power on that engine for the descent. However, the indicated vibration remained at maximum and the indicated fuel flow behaved erratically. The commander later stated that the action of closing the No 2 engine throttleOpen official document at PDF page 16Aircraft Accident Report 4/90
Printed page 144. PDF page 156.
whilst the No 2 engine was running down, the No 1 engine began to stabilise. However, its indicated vibration remained at maximum for at least 3 minutes until this engine was throttled back for the descent. The evidence indicated thatOpen official document at PDF page 156Aircraft Accident Report 4/90