The maximum weight used in weight and balance control of a given aircraft can normally be found in which document?

The maximum weight used in weight and balance control of a given aircraft can normally be found in which document?

• A. the pilot's operating handbook.
• B. in the Aircraft Specification or TCDS.
• C. the maintenance manual.
• D. the airworthiness directive.

Answer: (B)

The critical limit that defines how heavy the aircraft can be for safe weight and balance calculations is a certification limit published by the aircraft’s type design. This information is found in the Aircraft Specification or Type Certificate Data Sheet (TCDS), which lists the maximum takeoff weight (and other weight limits) for the aircraft model. That document establishes the official envelope the airplane is certified to operate within, and weight-and-balance calculations use these limits to ensure the center of gravity remains within permitted bounds. The pilot’s operating handbook may show current weight data and CG ranges for planning a specific flight, but the maximum weight itself is defined by the TCDS. The maintenance manual and airworthiness directive don’t provide these maximum weight limits.

The critical limit that defines how heavy the aircraft can be for safe weight and balance calculations is a certification limit published by the aircraft’s type design. This information is found in the Aircraft Specification or Type Certificate Data Sheet (TCDS), which lists the maximum takeoff weight (and other weight limits) for the aircraft model. That document establishes the official envelope the airplane is certified to operate within, and weight-and-balance calculations use these limits to ensure the center of gravity remains within permitted bounds. The pilot’s operating handbook may show current weight data and CG ranges for planning a specific flight, but the maximum weight itself is defined by the TCDS. The maintenance manual and airworthiness directive don’t provide these maximum weight limits.