| 摘要 |
A lifting device for replacing dynamic or static components of helicopter-type rotary wing aircraft comprising a lifter capable of moving components between an installation/removal position and a loading/unloading position located near the aircraft, a supporting structure on which the lifter is mounted, and at least one support member is rigidly attached to the supporting structure. The at least one support member can rest on and be directly secured to the airframe of the aircraft. |
