Bell 407 Internal Max Weight Graph FMS28
Hi guys/gals, looking at the Bell 407 OGE hover ceiling graph (FMS 28). Wondering why the MAX GW Internal line deviates to the left about 2/3rds of the way up? Effectively reducing the allowable internal weight considerably with altitude compared to what you can carry externally.
Have heard a few 'theories' from fellow 407 pilots. The most likely so far being extra safety margins for internal load as it cannot be jettisoned like external?
Thoughts?