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Printed page label not indexed. PDF page 112.
part of LI8 splice which should have been spliced by two-row rivets became spliced by one-row rivets, with the result that the strength of this part decréased to about 70% of the original strength. From this, it is estimated thatOpen official document at PDF page 112AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119
Printed page 124. PDF page 135.
part of L18 splice which should have been spliced by two-row rivets became spliced by one-row rivets, with the result that the strength of this part decreased to about 70% of the strength to be obtained by the original spliceOpen official document at PDF page 135AAIC final report: Japan Air Lines Boeing 747SR-100 JA8119