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Printed page 15. PDF page 21.
showed that the primary cause of the separation of the rod end from the piston rod was severe corrosion eausedby moisture on to the mating threads of both components. As a result of the corrosion, the joint was weakened toOpen official document at PDF page 21United Airlines, Inc., McDonnell-Douglas DC-8-61, N8082U, Portland, Oregon, December 28, 1978
Printed page 23. PDF page 29.
Safety Board's ~ investigation revealed that the landing _gear_problem was ceused by severe corrosion in the _mating_threads where the right main landing gear retract cylinder atse mbly actuator-pisten-red-was-connected o the rod end. The corrosion allowed the two partsOpen official document at PDF page 29United Airlines, Inc., McDonnell-Douglas DC-8-61, N8082U, Portland, Oregon, December 28, 1978