What is the aircraft weight at the top of climb for Operating Conditions W-3?

To determine the aircraft weight at the top of climb for Operating Conditions W-3, it's important to consider the specific parameters and data provided for that condition in the context of aircraft performance. The weight at the top of climb can depend on various factors, including the specific type of aircraft, its configuration, and performance charts that detail how weight, altitude, and air temperature influence climb capabilities.

In the scenario presented, the correct weight of 75,900 lbs aligns with the operational data corresponding to Operating Conditions W-3. This implies that the aircraft has been calculated to have a maximum allowable weight for operation under those conditions, ensuring safety and optimal performance during its climb phase.

The selected weight indicates that the calculations accounting for fuel burn and anticipated weight adjustments during climb are properly aligned with the operational performance thresholds established for the aircraft. Values such as 75,750 lbs and 76,100 lbs may not fit within the range of safe operational limits or performance expectations dictated by the conditions specified, making 75,900 lbs the most appropriate sustainable weight at the top of climb for W-3 conditions.