Abstract: A cargo guide assembly includes a base which is mountable to the floor of a cargo hold in a transport vehicle such as an aircraft. A guide rail is pivotally attached to the base for swinging movement between a first position in which the guide rail contacts the side of a cargo container in the cargo hold, thereby restraining movement of the cargo and a second position in which the guide rail lies below the cargo floor, thereby permitting cargo to pass over it. A powered actuator is mounted on the base and is coupled to the guide rail by actuation linkage operable to move the guide rail from its first to its second position. Preferably, the assembly includes a latch for latching the guide rail in its second position and a biasing device associated with the base to bias the guide rail toward its first position.

Abstract: A cargo restraint for use in loading and unloading cargo in the hold of an aircraft includes a lip member which extends into the path of cargo entering the aircraft and is yieldably mounted to rotate out of the way of cargo entering the cargo hold. The lip member has stop means associated therewith to prevent rotation of the lip means on engagement by cargo in a direction exiting the cargo hold so as to restrain the cargo from exiting. The lip member is rotatably mounted on a carrier member which in turn is pivotally attached to a base affixed to the floor of the cargo hold. The lip member is movable into a retracted position below the cargo deck to permit passage of cargo out of the hold. A powered actuator is provided which is operable to move the lip member between its extended and retracted positions.