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Printed page 67. PDF page 71.
stall and subsequent loss of control of the aircraft. The flighterew eould not see the wings and engines from the cockpit. Because of the loss of the slat disagreement light and the stall warning system, the flighterew would not -haveOpen official document at PDF page 71NTSB AAR-79/17: American Airlines DC-10-10 N110AA, Chicago
Printed page label not indexed. PDF page 27.
asymmetric slat-retracted stall speed for the left: ; wing was 159.KIAS; and the estimated wings-level V for the damaged aircraft} was 128 KIAS.: With a 4° left bank-- a bank into the missing engine - 159 KIAS was the minimumOpen official document at PDF page 27NTSB AAR-79/17: American Airlines DC-10-10 N110AA, Chicago