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Printed page 147. PDF page 161.
input in response to the second wake turbulence encounter was too aggressive, and his initial rudder pedal input response was unnecessary to control the airplane. In analyzing the reason for these inputs, the Board evaluated the three factors discussed inOpen final at PDF page 161In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587
Printed page 160. PDF page 174.
input in response to the second wake turbulence encounter was too aggressive, and his initial rudder pedal input response was unnecessary to control the airplane. 13. Certification standards are needed to ensure that future airplane designs minimize the potential forOpen final at PDF page 174In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587