PURPOSE: To provide a landing device securing a cabin space and preventing damage due to FOD, etc., during ground run.

CONSTITUTION: In a landing device for aircraft having a nose landing gear 1 allowed to be housed in a nose landing gear housing space 3 in a front fuselage 2, an operating device 4 for elevating and driving the nose landing gear 1, and a controlling device 6 for ground run for controlling the hose landing gear 1, a pair of side partition members 11 are provided in the nose landing gear housing space 3 at both the sides. The space at the front fuselage 2 is divided into the nose landing gear housing space 3 and right and left side chambers 13. The operating device 4 is provided in one side chamber 13. The controlling device 6 is provided in the other side chamber 13. The operating device 4 and the controlling device 6 are shielded by the side partition members 11 to eliminate damage due to FOD, etc., and are positioned at the nose landing gear 1 sides to sacrifice no cabin space.