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Printed page 145. PDF page 159.
At 250 knots calibrated airspeed (KCAS), the A300-600 rudder pedal design showed the lightest pedal forces of all airplanes evaluated. In designing the A300-600, Airbus made two changes to the rudder control system originally used on the A300B2/B4, both ofOpen final at PDF page 159In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587
Printed page 146. PDF page 160.
sensitivity with airspeed, which is characteristic of variable stop designs, with the lightest pedal forces of all the transport-category aircraft evaluated by the Safety Board during this investigation. These characteristics likely played a role in the accident sequenceOpen final at PDF page 160In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587
Printed page 160. PDF page 174.
sensitivity with airspeed, which is characteristic of variable stop designs, with the lightest pedal forces of all the transport-category aircraft evaluated by the National Transportation Safety Board during this investigation. 12. The first officer's initial control wheOpen final at PDF page 174In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587