What is the aircraft weight at the top of climb for Operating Conditions W-2?

The correct weight at the top of climb for Operating Conditions W-2 is 83,775 lbs. This figure typically reflects the operational limits and performance data that have been established for specific aircraft configurations and loading conditions under a defined set of parameters. In this case, the weight is aligned with the operational profiles that consider factors such as fuel burn, payload, and airframe capacity at the specified conditions.

Understanding operational conditions like W-2 is crucial for dispatchers, as it informs decisions regarding fuel management, compliance with regulatory weight limits, and overall flight safety. The close examination of climbing performance and weight limitations ensures that an aircraft can safely achieve and maintain cruise altitude, making the knowledge of these values essential for effective air traffic management.

The other options, while they may be close in weight, do not align with the data specific to the defined Operating Conditions W-2, indicating their unsuitability for this context. This highlights the importance of relying on accurate and updated performance specifications during flight planning and dispatch activities.