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Printed page 19. PDF page 27.
requirements for the wing lower skin, nor the access panel. The cast aluminium material had an impact strength approximately one quarter that of the lower wing skin, which formed the tank floor proper. Air conditioning system The aircraft had twoOpen official document at PDF page 27Aircraft Accident Report 8/88: Boeing 737-236 series 1, G-BGJL, Manchester, 22 August 1985
Printed page 164. PDF page 172.
creating a hole which had an area of 42 square inches. The wing tank access panel had an impact strength approximately one quarter that of the lower wing skin; had the dome struck the adjacent skin penetration of the tankOpen official document at PDF page 172Aircraft Accident Report 8/88: Boeing 737-236 series 1, G-BGJL, Manchester, 22 August 1985
Printed page 116. PDF page 124.
the dome had struck the adjoining wing skin rather than the access panel, which has an impact strength approximately one quarter that of the lower skin, penetration of the tank would not have occurred. The wing skin and access panelOpen official document at PDF page 124Aircraft Accident Report 8/88: Boeing 737-236 series 1, G-BGJL, Manchester, 22 August 1985