Abstract: An apparatus for supporting a wing assembly at a wing assembly support height. Base sections are provided, each having a different predetermined height with respect to one another. A movable platform carries a plurality of base sections, and a plurality of wing assembly support sections rest on base sections and include wing assembly connectors, which are movable in a first plane and a second plane generally perpendicular relative to the first plane. A differential height is defined between the wing assembly support height and the combined heights of the platform and the height of wing assembly connector, relative to the bottom of the wing assembly support section. At least one of the base sections is of a predetermined height approximating the differential height and is carried on the platform. The wing assembly support section is carried on such base section.

Abstract: An apparatus for supporting a wing assembly at a wing assembly support height. Base sections are provided, each having a different predetermined height with respect to one another. A movable platform carries a base section, and a wing assembly support section rests on a selected base section and includes a wing assembly connector, which is movable in a first plane and a second plane generally perpendicular relative to the first plane. A differential height is defined between the wing assembly support height and the combined heights of the platform and the height of wing assembly connector, relative to the bottom of the wing assembly support section. At least one of the base sections is of a predetermined height approximating the differential height and is carried on the platform. The wing assembly support section is carried on such base section.

Abstract: An apparatus for supporting a wing assembly at a wing assembly support height. Base sections are provided, each having a different predetermined height with respect to one another. A movable platform carries a plurality of base sections, and a plurality of wing assembly support sections rest on base sections and include wing assembly connectors, which are movable in a first plane and a second plane generally perpendicular relative to the first plane. A differential height is defined between the wing assembly support height and the combined heights of the platform and the height of wing assembly connector, relative to the bottom of the wing assembly support section. At least one of the base sections is of a predetermined height approximating the differential height and is carried on the platform. The wing assembly support section is carried on such base section.

Abstract: An apparatus for supporting a wing assembly at a wing assembly support height. Base sections are provided, each having a different predetermined height with respect to one another. A movable platform carries a base section, and a wing assembly support section rests on a selected base section and includes a wing assembly connector, which is movable in a first plane and a second plane generally perpendicular relative to the first plane. A differential height is defined between the wing assembly support height and the combined heights of the platform and the height of wing assembly connector, relative to the bottom of the wing assembly support section. At least one of the base sections is of a predetermined height approximating the differential height and is carried on the platform. The wing assembly support section is carried on such base section.

Abstract: Aircraft mission equipment (e.g., an electrical equipment cabinet) comprising a base plate equipped on a bottom with a plurality of air casters that provide flotation mobility. When the equipment is being loaded in or unloaded from an aircraft, the actuated air casters provide a plurality of air cushions. The total lift force produced by the air cushions is sufficient to float the equipment above and out of contact with the floor, thereby improving ease of handling and reducing point loads on the floor structure. Portions of the air distribution system that provides pressurized air to the air casters on the bottom of the base plate are structurally integrated into the base plate of the mission equipment.

Abstract: The invention relates to a cargo restraint arranged between a passenger compartment and an article storage compartment in a utility vehicle. The cargo restraint comprises a web body, a first elongate supporting bar attached to the upper marginal edge of the web body and being located in an upper section of the storage compartment attached at a pair of opposed, outer ends, and at least a second and a third elongated supporting bar attached to the lower marginal edge of the web body, said second and third elongated supporting bar being located in a lower section of the storage compartment attached at a pair of opposed, outer ends. At least one pair of adjacent, facing end sections of the said second and third elongate supporting bars are arranged separate and movable relative to each other.