5120-14-454-9392

2 | DAC: 4 18 Apr 2002 5120-14-364-8020 Claw Bar 212286RNCC: 3 | RNVC: 2 | DAC: 1 2 Sep 1980 5120-14-454-9392

1560-99-459-8095 1560994598095 994598095 is an item of various configuration that is an integral member of the airframe structure. it is specifically designed for the purpose of maintaining, positioning, joining, and strengthening the aircraft structure. it may include holes for mounting purposes or to form an assembly.

6750-01-016-2180 6750010162180 010162180 is a chemically coated paper which, when exposed to a light source and passed through a liquid, vapor spray, or thermal developing process, reproduces copy from a translucent original.

5340-14-441-8904 5340144418904 144418904 is a forked part, having transverse hole(s) or slot(s) in each arm (prong) to accommodate a bolt, pin, or the like, and having a connection facility opposite the fork. it is designed to be attached to a shaft, rod, turnbuckle or the like by welding, threading, and/or pinning. may include provisions for locking. see also yoke, universal joint and connector, rod end. for items specifically designed for aviation, see clevis, rod end, aviation.

5330-27-016-2180 5330270162180 270162180 is an item fabricated from nonmetallic special shaped section. it may be (1) formed to a specific shape with or without joints, (2) a single piece whose ends have been secured together to form a specific shape, or (3) a straight item fabricated to a specific length for a specific application with end cuts or joints. items, except for molded corners, slot(s), press fit buttons, and the like must be of one continuous cross section. it is specifically designed for use in applications where there is no relative motion between joined parts. excludes bushing, nonmetallic; packing, performed; pad, cushioning;and seal, plain. for straight items with square end cuts and without mounting hole(s), slot(s), or press fit buttons, see nonmetallic special shaped section.