A tool for adjusting an orientation of a nose landing gear of an aircraft is disclosed herein. The nose landing gear has an axle to which a wheel is mounted. The axle has an opening extending therethrough. The opening is defined by an inner surface of the axle. The tool includes, but is not limited to, a unitary member having a handle portion at a first end of the unitary member and an axle-engaging portion at a second end of the unitary member. The handle portion is configured for engagement with a hand of an operator. The axle-engaging portion is configured to be inserted into the opening and to engage with the inner surface.
NOSE LANDING GEAR ADJUSTMENT TOOL
2023-05-25
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Emerald Group Publishing | 2000
NTIS | 1979
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