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Printed page 130. PDF page 141.
Dec.5, 1985) In reference to the aft pressure bulkhead, an inspection program beyond the ‘usual visual inspection should be established to detect the extent of possible multiple site fatigue cracking. f) Evaluation of the fail-safe ¢riteria of the domed aftOpen official document at PDF page 141AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 276.
inspection and repairs are conducted for the portions concerned. The post-flight check is usually made by three personnel in about 50 minutes, 2.4.2 A Maintenance This maintenance is usually done within 250 flying hours. As shown in the table above,Open official document at PDF page 276AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page label not indexed. PDF page 281.
defects and their symptoms by detailed observation on a Particular area. For this reason usually a visual distance is necessary. Defects or symptoms expected to be discovered by this inspection are microscopic abnormality caused in structural materials or elements: forOpen official document at PDF page 281AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119