VTOL.2210 Structural
design loads
n/a
(a) The applicant must:
(1) determine structural design loads resulting from likely externally or internally applied pressure, force or moment which may occur in flight, ground and water operations, ground- and water-handling, and while the aircraft is parked or moored;
(2) determine the loads required by VTOL.2210(a)(1) at all critical combinations of parameters, on and within the boundaries of the structural design envelope; and
(3) the magnitude and distribution of these loads must be based on established physical principles within the structural design envelope.
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