VTOL.2100 Mass and centre
of gravity
n/a
(a)Â Â Â Â The applicant must determine limits for mass and centre of gravity that provide for the safe operation of the aircraft.
(b)    The applicant’s design must comply with each requirement of this Subpart at critical combinations of mass and centre of gravity within the aircraft’s range of loading conditions using acceptable tolerances.
(c)Â Â Â Â Â The condition of the aircraft at the time of determining its empty mass and centre of gravity must be well defined and easily repeatable.
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