The system for restraining aircraft wheels using at least one body having a rounded top surface and a squared bottom edge connected via a pair of sloped side walls. A pair of bodies being secured along a length of reflective rope. At least a bottom surface of the body being made of a material having a coefficient of friction sufficient to prevent sliding on a surface to prevent movement of the aircraft wheels.

The system for restraining aircraft wheels using at least one body having a rounded top surface and a squared bottom edge connected via a pair of sloped side walls. A pair of bodies being secured along a length of reflective rope. At least a bottom surface of the body being made of a material having a coefficient of friction sufficient to prevent sliding on a surface to prevent movement of the aircraft wheels.

Liquid dispensing assemblies including adhesive anchoring assemblies configured to adhere to a support surface external to a device such as a vehicle. An air vehicle includes (a) a fluid adhesive container assembly detachably attached to the air vehicle, wherein the fluid adhesive container assembly comprises: (i) an adhesive container comprising fluid adhesive; and (ii) one or more fibers, wherein the one or more fibers are configured, or a brush of fibers, or a fabric of fibers, is configured to conduct the fluid adhesive and to structurally support an adhesive bond between the one or more fibers and a surface; and (b) means for dispensing the fluid adhesive from the fluid adhesive container, to the one or more fibers.

Liquid dispensing assemblies including adhesive anchoring assemblies configured to adhere to a support surface external to a device such as a vehicle. An air vehicle includes (a) a fluid adhesive container assembly detachably attached to the air vehicle, wherein the fluid adhesive container assembly comprises: (i) an adhesive container comprising fluid adhesive; and (ii) one or more fibers, wherein the one or more fibers are configured, or a brush of fibers, or a fabric of fibers, is configured to conduct the fluid adhesive and to structurally support an adhesive bond between the one or more fibers and a surface; and (b) means for dispensing the fluid adhesive from the fluid adhesive container, to the one or more fibers.

A displacement arrangement for use in a combination dolly-pallet includes an impelling member movable between first and second positions. A linkage is pivotally connected to the impelling member. When the impelling member moves between the first and second positions, the linkage moves pivotally relative to the impelling member to an extended position.

A displacement arrangement for use in a combination dolly-pallet includes an impelling member movable between first and second positions. A linkage is pivotally connected to the impelling member. When the impelling member moves between the first and second positions, the linkage moves pivotally relative to the impelling member to an extended position.

A device to engage with a steering mechanism of a nose landing gear of an aircraft to limit steering rotation of the nose landing gear. The device includes a first chock sized to fit within a first space formed in the nose landing gear at a first cylinder of a steering mechanism, and a second chock sized to fit within a second space formed in the nose landing gear at a second cylinder. The first chock is configured to engage with the first cylinder and to compress to prevent retraction of the first cylinder beyond a first predetermined length. The second chock is configured to engage with the second cylinder and to compress to prevent retraction of the second cylinder beyond a second predetermined length.

A device to engage with a steering mechanism of a nose landing gear of an aircraft to limit steering rotation of the nose landing gear. The device includes a first chock sized to fit within a first space formed in the nose landing gear at a first cylinder of a steering mechanism, and a second chock sized to fit within a second space formed in the nose landing gear at a second cylinder. The first chock is configured to engage with the first cylinder and to compress to prevent retraction of the first cylinder beyond a first predetermined length. The second chock is configured to engage with the second cylinder and to compress to prevent retraction of the second cylinder beyond a second predetermined length.

A landing gear platform is positionable between rearward and forward tires on one side of an aircraft landing gear and rearward and forward tires on the opposite side of the aircraft landing gear. The platform includes a pair of chocks that engage between the rearward and forward tires on the one side of the aircraft landing gear and the rearward and forward tires on the opposite side of the aircraft landing gear and prevent the tires from rotating. A panel spans over the tops of the pair of chocks. A top surface of the panel can be reached by a worker using a stepstool, enabling the worker to stand on the top surface of the panel when performing work on the landing gear above the rearward and forward tires of the aircraft landing gear.