n/a
(a) The aircraft must be free from flutter, control reversal, and divergence:
(1) at all speeds within and sufficiently beyond the structural design envelope;
(2) for any configuration and condition of operation;
(3) accounting for critical degrees of freedom; and
(4) accounting for any critical failures or malfunctions.
(b) The applicants' design must account for tolerances for all quantities that affect flutter.
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