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CS 27.483 One-wheel landing conditions
Available versions for ERULES-1963177438-4910
ED Decision 2003/15/RM
found in: CS-27 Amdt 9 - Small Rotorcraft (Dec 2021)
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CS-27 Amdt 10 - Sm... (Feb 2023)
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CS 27.483 One-wheel landing conditions ED Decision 2003/15/RM For the one-wheel landing condition, the rotorcraft is assumed to be in the level attitude and to contact the ground on one aft wheel. In this attitude: (a) The vertical load must be the same as that obtained on that side under [CS 27.479(b)(1)](#_DxCrossRefBm472493296); and (b) The unbalanced external loads must be reacted by rotorcraft inertia.
CS 27.483 One-wheel landing conditions ED Decision 2003/15/RM For the one-wheel landing condition, the rotorcraft is assumed to be in the level attitude and to contact the ground on one aft wheel. In this attitude: (a) The vertical load must be the same as that obtained on that side under [CS 27.479(b)(1)](#_DxCrossRefBm8893865); and (b) The unbalanced external loads must be reacted by rotorcraft inertia.