What is the center-of-gravity range for Piper aircraft model PA-28-235 at 1,950 pounds?

The center-of-gravity (CG) range for an aircraft is crucial for ensuring safe flight operations, as it affects stability and control. For the Piper PA-28-235 at a weight of 1,950 pounds, the correct CG range is from (+85.1) to (93.5).

This range indicates that the center of gravity must be maintained between these two measurements to ensure optimal performance and safety. If the CG is too far forward or aft of this range, it could result in poor handling characteristics, affecting the aircraft's stability during flight and potentially leading to dangerous conditions.

While the other options reflect different CG ranges, they either fall outside the specifications required for this specific weight or are not accurate according to the Piper PA-28-235 aircraft design. Knowing the specific CG range for various weights is essential for pilots and maintenance personnel to evaluate loading conditions and ensure compliance with aircraft operational limits.