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Full Deflection?

Gemini Sparkle

Key Takeaways:

  • Maneuvering speed (VA) is critical for structural integrity, traditionally understood to permit rapid, full control movements below it, but this understanding was incomplete.
  • The American Airlines Flight 587 crash demonstrated that VA does not protect against rapid, opposing control inputs, even when flying below this speed, revealing a nuanced limitation.
  • Pilots must understand that VA only ensures airframe integrity during a single, full control deflection; exceeding VA or making abrupt, substantial maneuvers (as shown by the Cessna 180 accident) can lead to in-flight 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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