During the takeoff of Flight 191, the engine and pylon assembly separated from the left wing, and fell onto the runway. This separation ripped out electrical and hydraulic systems in the left wing. The electrical system in the left wing controlled the captain’s flight director instrument, stall warning system and slat disagreement warning lights. The hydraulic lines and follow up cables of the drive actuator for the left wing’s outboard leading edge slat were severed, and the slats retracted during climb out. This caused an asymmetric stall and subsequent loss of control of the aircraft. Because of the loss of slat disagreement light and loss of the stall warning system, the flight crew never received warning of the stall. …show more content…
The length of the fracture was determined to be approximately 13