What are the dimensions of the runway for an ALA for an aircraft above 2000kg MTOW?

What are the dimensions of the runway for an ALA for an aircraft above 2000kg MTOW?

• A. 10m x 1
• B. 20m x 2
• C. 15m x 1
• D. 25m x 1

Answer: (C)

For an aircraft with a maximum takeoff weight (MTOW) above 2000 kg, the required dimensions of the runway for an Aerodrome Landing Area (ALA) are specific to ensure safety and accommodate the operational needs of such aircraft. The correct dimensions are 15 meters in width and an operational length that can fit the requirements for different phases of flight, including takeoff and landing. The width of 15 meters provides adequate space for larger aircraft to operate safely, allowing for necessary clearances during takeoff and landing maneuvers. As the aircraft size increases, so do the requirements for runway dimensions to improve safety margins and operational capabilities. Understanding these dimensions is essential for ensuring that any ALA can support the aircraft effectively without compromising safety. The other options provided do not meet the necessary width requirements for aircraft exceeding the specified MTOW, thus are not suitable for this context.

For an aircraft with a maximum takeoff weight (MTOW) above 2000 kg, the required dimensions of the runway for an Aerodrome Landing Area (ALA) are specific to ensure safety and accommodate the operational needs of such aircraft. The correct dimensions are 15 meters in width and an operational length that can fit the requirements for different phases of flight, including takeoff and landing.

The width of 15 meters provides adequate space for larger aircraft to operate safely, allowing for necessary clearances during takeoff and landing maneuvers. As the aircraft size increases, so do the requirements for runway dimensions to improve safety margins and operational capabilities.

Understanding these dimensions is essential for ensuring that any ALA can support the aircraft effectively without compromising safety. The other options provided do not meet the necessary width requirements for aircraft exceeding the specified MTOW, thus are not suitable for this context.