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VTOL.2210 Structural design loads
Available versions for ERULES-1963177438-22449
n/a
found in: Small Category VCA (Revision 0) SC-VTOL (Oct 2024)
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Small Category VCA... (Oct 2024)
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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](#_DxCrossRefBm1877490441)(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.