Load Factor Vs. Aircraft Weight
Hi all,
Currently doing my Instructor Rating and am trying to answer the following: What effect (if any) does aircraft weight have on load factor? I realise that:
1. To be in the "utility" cat. of the c172 we need to be under 2000lbs, which permits more "G" than when heavier (CofG limits aside); yet:
2. Va increases with aircraft weight, which almost seems to be conflicting with this
I'm imagining the answer may be "no effect", as a 172 or 777 will pull the same "G" if in an equally banked turn while maintaining altitude...so i may be scratching my head over nothing here...all thoughts appreciated! thanks!