Answer:
Option B is correct ( difficulty in recovering from a stalled condition.)
Explanation:
Option B is correct ( difficulty in recovering from a stalled condition.)
If you load airplane in such manners CG has changed then it will have huge impact on the longitudinal stability. Due to this airplane would face difficulty in recovering from a stalled condition.
Stall is the phenomena in which air resistance is increased on the wings which causes decrease in lift. So it is important to remain with in CG limit put by manufacturer to avoid stall condition.
One undesirable flight characteristic a pilot might experience with this plane is : ( B ) difficulty in recovering from a stalled condition.
When loading an aircraft the CG limit should not be exceeded as stated by the manufacturer, this is because when the aircraft is loaded above the limit the longitudinal stability of the aircraft will be affected because more air resistance will be exerted on the wings of the plane which leads to a condition known as stall
Hence we can conclude that one undesirable flight characteristic a pilot might experience with this plane is difficulty in recovering from a stalled condition.
Learn more about aircraft stalled condition : https://brainly.com/question/5120608
