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American Airlines 587

Printed page 161. PDF page 175.

axis throughout the flight envelope, including limits for rudder pedal sensitivity. (A-04-56) After the yaw axis certification standard recommended in Safety Recommendation A-04-56 has been established, review the designs of existing airplanes to determine if they meet
Open final at PDF page 175In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587