What is the maximum ramp weight (MRW) of the aircraft?

The maximum ramp weight (MRW) of the aircraft is an important specification as it indicates the maximum weight the aircraft is allowed to be at the ramp or on the ground before takeoff. For the Pilatus PC-12 NG, this weight includes the aircraft's empty weight plus the maximum allowable payload and fuel. The MRW is designed to ensure the aircraft can operate safely and effectively within the structural limits established by the manufacturer.

In this case, the correct answer reflects the MRW of the Pilatus PC-12 NG, which is set at 10,495 pounds. This figure is critical for operational planning, helping pilots and flight planners ensure they do not exceed this weight during ground operations, which could impact safety and performance, especially during takeoff and landing. Understanding the MRW allows aviators to make informed decisions regarding load distribution and fuel management, further promoting safety and efficiency in flight operations.