Airbus designed limitation tolerance
Hi, guys
I have a question on aircraft limitation torlerance and i'd appreciate any replies just to broaden my knowledge. Airbus has limitations on all systems as well as operational limitation of the aircraft, do they have any toleratable margin for those and exactly how many percents do they apply on that?
Example: for A321 maximum landing weight of 75.500 kg, what would be the toleratable margin applied for that weight?
If you have any reference please give me. Thanks guys!