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CS 27.341 Gust loads
Available versions for ERULES-1963177438-4894
ED Decision 2003/15/RM
found in: CS-27 Amdt 9 - Small Rotorcraft (Dec 2021)
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CS 27.341 Gust loads ED Decision 2003/15/RM The rotorcraft must be designed to withstand, at each critical airspeed including hovering, the loads resulting from a vertical gust of 9.1 m/s (30 ft/s).
CS 27.341 Gust loads ED Decision 2003/15/RM The rotorcraft must be designed to withstand, at each critical airspeed including hovering, the loads resulting from a vertical gust of 9.1 m/s (30 ft/s).