Incident Description
Flight 583 was cruising at an altitude of 33,000 feet when the leading edge slats deployed inadvertently. The autopilot disconnected, and the captain assumed manual control of the aircraft. Subsequently, the airplane underwent several violent pitch oscillations and lost 5,000 feet of altitude before the situation was stabilized.
Investigation Findings
The safety board determined that the inadvertent deployment of the slats was the result of an inadequately designed flap/slat handle. The handle was found to be easily and inadvertently dislodged from the up/retracted position, which caused the slat extension. No other factors were cited in the determination of the cause.
Aftermath
Further details regarding the aircraft, operator, or occupants were not specified in the source material. The incident underscores the importance of design integrity in cockpit controls.