What is the maximum distribution load intensity also known as?

The maximum distribution load intensity is known as the maximum permissible floor load. This term refers to the highest load per unit area that can be safely carried by the aircraft's structure, particularly in relation to the floor of the cabin or cargo area. This is a crucial parameter in aircraft design and operations, ensuring that both the aircraft and the safety of passengers and cargo are maintained.

Understanding the maximum permissible floor load helps in properly distributing weight and ensuring that the load does not exceed the structural limits of the aircraft. It ensures that weight is balanced and distributed in a manner that maintains the aircraft's center of gravity within safe operational limits.

The other options, while related to aircraft weight considerations, do not fit the specific definition of maximum distribution load intensity. The absolute maximum weight relates to the overall weight limit of the aircraft, whereas the design load limit refers to the engineering standards set during construction. The critical weight limit typically refers to weight thresholds that impact performance characteristics or operational capabilities, rather than floor-specific load capacities.