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CS 29.481 Tail-down landing conditions
Available versions for ERULES-1963177438-5428
ED Decision 2003/16/RM
found in: CS-29 Amdt 11 - Large Rotercraft (Feb 2023)
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CS-29 Amdt 12 - La... (Mar 2026)
CS-29 Amdt 11 - La... (Feb 2023)
CS-29 Amdt 10 - La... (Jan 2023)
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CS 29.481 Tail-down landing conditions ED Decision 2003/16/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 29.481 Tail-down landing conditions ED Decision 2003/16/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 29.481 Tail-down landing conditions *ED Decision 2003/16/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.