If the airspeed increases above 210 kts while flaps are moving from 2 to 1, what happens?

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When the airspeed exceeds 210 knots while the flaps are transitioning from configuration 2 to configuration 1, the system is designed to protect the aircraft from exceeding its operational limits regarding flap positions. In this scenario, the flaps will automatically retract to configuration 1.

This design feature ensures that the aircraft maintains optimal performance and prevents potential structural stress that could arise from operating the flaps at high speeds. The flap system is programmed with certain limits to ensure safe operations, and exceeding set airspeeds during flap transitions triggers this automatic retraction to a safer flap position.

The other choices involve configurations that either do not respond correctly to increasing airspeed or incorrectly extend the flaps further, which would not align with the safety protocols implemented in aircraft design.

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