§29.321 General

(a) The flight load factor must be assum ed to act n ormal to th e lo ngitudinal ax is of the rotorcraft, and to be equal i n m agnitude and opposite i n di rection t o t he rot orcraft i nertia load factor at the centre of gravity. (b) Compliance with th e flig ht load requirements of this Subpart must be shown: (1) At each weight from the design minimum weight to t he desi gn m aximum weight; and (2) With any pract ical di stribution of disposable load within the operating limitations in the rotorcraft flight manual.