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CS 27.481 Tail-down landing conditions
Available versions for ERULES-1963177438-4909
ED Decision 2003/15/RM
found in: CS-27 Amdt 10 - Small Rotorcraft (Feb 2023)
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CS-27 Amdt 10 - Sm... (Feb 2023)
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CS 27.481 Tail-down landing conditions ED Decision 2003/15/RM (a) The rotorcraft is assumed to be in the maximum nose-up attitude allowing ground clearance by each part of the rotorcraft. (b) In this attitude, ground loads are assumed to act perpendicular to the ground.
CS 27.481 Tail-down landing conditions ED Decision 2003/15/RM (a) The rotorcraft is assumed to be in the maximum nose-up attitude allowing ground clearance by each part of the rotorcraft. (b) In this attitude, ground loads are assumed to act perpendicular to the ground.