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Pitch movement in flight is stabilized primarily by the aircraft's horizontal stabilizer and elevator. The horizontal stabilizer provides a counteracting aerodynamic force to the pitch changes induced by control inputs or external factors like turbulence. The elevator, located on the trailing edge of the stabilizer, adjusts its angle to control the pitch attitude, allowing the pilot to maintain or change the desired angle of attack. Additionally, the aircraft's design and balance play a critical role in ensuring stable pitch behavior during flight.

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