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Full Deflection?

Gemini Sparkle

Key Takeaways:

  • Maneuvering speed (VA) is a crucial flight limitation for structural integrity, though the American Airlines Flight 587 crash revealed that rapid, opposing control inputs can cause failure even below VA.
  • This incident clarified that VA primarily ensures structural integrity only for a *single* full control deflection, as rapid, opposing movements can exceed design limits regardless of speed.
  • The Cessna 180 in-flight breakup further underscored the importance of VA, demonstrating that abrupt maneuvers performed *above* maneuvering speed can also lead to catastrophic structural failure.
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Maneuvering speed is something fledgling airplane pilots learn about early in their training. It’s one of the more important details to know about any airplane because it has implications for structural integrity. It’s also relevant to operating in turbulence and performing maneuvers, although its value isn’t on an airspeed indicator, mainly because it varies with weight.

Maneuvering speed was taught to many pilots as the speed above which rapid, full control movements must not be made. The implication—and one of the lessons many pilots drew—is that rapid, full control movements could be made below that weight-adjusted speed. Then came American Airlines Flight 587, an Airbus A300 that crashed shortly after departing New York’s John F. Kennedy International Airport on November 12, 2001, killing all 260 aboard and five on the ground.

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