FAA Advisory Circular 43.13-1B
Acceptable Methods, Techniques, and Practices
Aircraft Inspection and Repair
AC 43.13-1B | 7. Aircraft Hardware, Control Cables, and Turnbuckles | 11. Hardware Identification Tables | 7-210. Nuts
9/8/98
TABLE 7-12. (CONTINUED)
Bolt Number
NAS6604-6620
Description
Bolt, hex head,
long thread, alloy steel
AC 43.13-1B
TABLE 7-13. (CONTINUED)
Nut Part Number
Description
AN345
Nut, plain, hex., n-s,
fine thread
NAS6704-6720
Bolt, hex. head,
long thread, cres.
AN350
Nut, plain, wing
TABLE 7-13. TABLE OF NUTS.
Nut Part Number
Description
AN256
Nut, self-lock
right angle plate
AN310
Nuts, castellated
AN315
Nut, plain
AN316
Nut, check
AN320
Nut, castle shear
AN335
AN340
AN341
Nut, plain, hex,
nonstructural
Nut, plain, hex.,
n-s, course thread
Nut, plain, hex.
AN355
AN356
AN360
AN361
AN362
AN363
AN364
AN365
AN366
Nut, engine, slotted
Nut, stamped
Nut, plain, engine
Self-locking nut plate,
countersunk 100°,
550 °F.
Nut, plate, self-locking,
noncounters., 550°F.
Nut, self-locking,
550 °F.
Nut, self-locking,
thin, 250 °F.
Nut, self-locking 250°F.
Nut, plate,
noncounters., 250°F.
Par 7-196
Page 7-63