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Printed page label not indexed. PDF page 15.
aircraft. The No. 1 and No. 3 hydraulic system's extension and retraction lines and the followup cables for the left' wing's outboard slat drive actuators were severed. Thirty-five of the 36 leading edge slat tracks were examined.. The examination disclosedOpen official document at PDF page 15NTSB AAR-79/17: American Airlines DC-10-10 N110AA, Chicago
Printed page label not indexed. PDF page 39.
consideration was given to an alternate locking mechanism. The slats! hydraulic lines! and followup cables | | | |Open official document at PDF page 39NTSB AAR-79/17: American Airlines DC-10-10 N110AA, Chicago
Printed page 67. PDF page 71.
and No. 4 on each wing, all flight controls were operating. . The hydraulic lines and followup cables of the drive actuator for the left wing's outboard leading edge slat. were severed: by the separation of the pylon and the.Open official document at PDF page 71NTSB AAR-79/17: American Airlines DC-10-10 N110AA, Chicago
Printed page label not indexed. PDF page 96.
and general condition (corrosion, damage, ete.); 2. Visually inspect all slat system followup cables and pulleys in situ for security and general condition (corrosion, damage, ete. ); ere 3. Visually inspect the inboard and outboard slat drive mechanisms while operatingOpen official document at PDF page 96NTSB AAR-79/17: American Airlines DC-10-10 N110AA, Chicago