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Printed page 38. PDF page 45.
pressurisation systems. Analysis suggested that this was unlikely to have been greater than 13,000 to 13,500 feet which, when followed by the descent profile flown, would not have promoted sufficient hypoxia to impair either the passengers or the crew. TheOpen official document at PDF page 45Aircraft Accident Report 1/92: BAC One-Eleven G-BJRT, 10 June 1990
Printed page 52. PDF page 59.
It has been calculated that the cabin altitude was unlikely to have been greater than 13,000 to 13,500 feet, achieved within two seconds after the loss of cabin pressure. The left windscreen had been replaced and the task certificated byOpen official document at PDF page 59Aircraft Accident Report 1/92: BAC One-Eleven G-BJRT, 10 June 1990