Abstract: A modular cargo loading and unloading system for installation in the lower lobe compartment of an aircraft is disclosed. The system includes a doorway transfer unit (17) and a plurality of longitudinal units (19). Each of the units includes conveyor belts for supporting and moving cargo containers. The doorway transfer unit (19) includes perpendicular conveyor belts (35, 37) that are selectively raised, lowered and powered to change the direction of cargo container movement at the entryway of the lower lobe compartment. The longitudinal units (19) include powered belts (51) that move the cargo containers to and from their destinations in the lower lobe compartment. A quick-change mechanism that attaches the modular units to the cargo tie-down receptacles located in the deck of the lower lobe compartment allows the units to be quickly installed and removed.

Abstract: A mounting assembly for the insulation and interior panels of an aircraft. The mounting assembly includes an upper retainer for securing the upper edge of the cabin panel to the aircraft, and a lower releasable latch assembly which connects the lower end of the cabin panel to the aircraft. The curved aircraft panels, which are made of a resilient bendable material, are installed so that the panels are further resiliently bent into a tensioned state which acts to resiliently engage the panels between the upper retainer and the lower latch assembly. A shock absorber and insulation retainer is attached to the aircraft between the aircraft frame and the cabin panel to prevent vibration of the cabin panel and to secure the insulation between the aircraft panel and the aircraft frame.