What is the result for flaps from position 2 to 1 when airspeed is above 210 kts?

Study for the A320 General Familiarization Test. Revise with flashcards and multiple choice questions, plus hints and explanations for every query. Prepare thoroughly for your exam!

Multiple Choice

What is the result for flaps from position 2 to 1 when airspeed is above 210 kts?

Explanation:
When transitioning the flaps from position 2 to position 1 in an A320, if the airspeed is above 210 knots, the system is designed to automatically configure the flaps to a specific position that adheres to safe operational limits. In this context, when flying at a speed above 210 knots, the A320's flap system will transition to CONF 1. This ensures that the aircraft remains within the appropriate configurations for flight conditions, maintaining optimal lift and drag characteristics for safe operation. Choosing CONF 1 reflects the design intention to enhance aerodynamic efficiency while also ensuring the safety and controllability of the aircraft as it prepares for further configuration as needed, particularly during approaches and landing phases. The correct designation for this flap configuration process emphasizes the importance of adhering to the aircraft’s speed limitations and configuration guidelines.

When transitioning the flaps from position 2 to position 1 in an A320, if the airspeed is above 210 knots, the system is designed to automatically configure the flaps to a specific position that adheres to safe operational limits. In this context, when flying at a speed above 210 knots, the A320's flap system will transition to CONF 1. This ensures that the aircraft remains within the appropriate configurations for flight conditions, maintaining optimal lift and drag characteristics for safe operation.

Choosing CONF 1 reflects the design intention to enhance aerodynamic efficiency while also ensuring the safety and controllability of the aircraft as it prepares for further configuration as needed, particularly during approaches and landing phases. The correct designation for this flap configuration process emphasizes the importance of adhering to the aircraft’s speed limitations and configuration guidelines.

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