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American Airlines 587

Printed page 4. PDF page 18.

are also within the authority of the yaw damper. 15 The FDR indicated that the captain did not subsequently change the airplane's power setting. 16 For information about the vertical stabilizer's attachment fittings, see section 1.6.1. For information about the

Open final at PDF page 18In-Flight Separation of Vertical Stabilizer, American Airlines Flight 587