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Printed page 67. PDF page 71.
fasteners into contact with the wing clevis.. The pylon to wing attach hardware was properly installed at all attachment points. : | All electrical power to the No. 1 a.c. generator'bus and No. 1 d.e. bus was lost after theOpen official document at PDF page 71NTSB AAR-79/17: American Airlines DC-10-10 N110AA, Chicago
Printed page label not indexed. PDF page 22.
place when the pylon separated and that the-thrust bushing assembly had been installed properly. After the accident, the Federal Aviation Administration (FAA) required a fleetwide inspection of the DC-10. During these inspections, discrepancies were found in the pylon assOpen official document at PDF page 22NTSB AAR-79/17: American Airlines DC-10-10 N110AA, Chicago