01-182-5600
Threaded Spacing Standoff
0.106 in. min, 0.113 in. max dia hole through center left internal
01-182-5601
Threaded Spacing Standoff
0.106 in. min, 0.113 in. max dia hole through center left internal
01-182-5602
Threaded Spacing Standoff
0.106 in. min, 0.113 in. max dia hole through center left internal
01-182-5603
Threaded Spacing Standoff
0.106 in. min, 0.113 in. max dia hole through center left internal
01-182-5604
Threaded Spacing Standoff
0.106 in. min, 0.113 in. max dia hole through center left internal
01-182-5693
Drawer Extension Slide Section
Cres qq-s-763 cl 302 or 304 or cl 303 astm A582; passivate ; 11.062 in.o/a lg; 0.625 in.w; 1.391 in.w slide
01-182-5729
Bumper
0.124" overall width furnished w/ pad
01-182-5793
Turnbuckle
Each end contains a hex, 0.492 in. min to 0.502 in. max width across flats, contains left-hand threads on 1 end
01-182-5834
Access Cover
Used on f-16/f-15/f-111. two holes 0.281 in dia drilled thru each flange 3.000 in. from end
01-182-6143
Angle Bracket
Used on fan frame of kc135r f108-cf-100 engine. angle
01-182-6144
Angle Bracket
Angle
01-182-6145
Angle Bracket
2nd leg contains a spacer angle
01-182-6146
Angle Bracket
1st leg contains 2 spacers, 2nd leg contains a nut-plate angle
01-182-6147
Angle Bracket
Angle
01-182-6148
Angle Bracket
Angle
01-182-6150
Double Angle Bracket
2nd leg contains a nut-plate double angle
01-182-6159
Blank Panel
Used on kc-135r acft. 7.000" overall width 0.093" material thickness blank, plain design
01-182-6160
Access Cover
0.218" hole diameter
01-182-6201
Loop Clamp
Saddle mount
01-182-6211
Mounting Bracket
Used on acft eng f100. titanium alloy ams 4928, 3.548 in. lg, 2.766 in. w, 0.250 min 0.253 max in. dia 1 hole, 0.211 min 0.212 max in. dia 4 holes
01-182-6212
Mounting Bracket
Used on acft eng f100. titanium alloy ams 4928, 1.711 in. lg, 0.610 min 0.620 max in. w, 0.211 min 0.212 max in. dia 2 places, 0.250 min in. 0.253 max in. dia 1 place
01-182-6215
Mounting Bracket
Used on acft eng f100. titanium alloy ams 4928, 4.340 in. lg, 0.305 min in. 0.315 max in. dia 1 hole, 0.462 min in. 0.466 max in. dia 1 hole, 0.250 min 0.253 max in. dia 1 hole, 0.249 min 0.250 max in. dia 2 holes
01-182-6217
Mounting Bracket
Used on acft eng f100. titanium alloy ams 4928, 0.740 min 0.760 max in. w, 3.610 in. lg, 0.250 min 0.253 max in. 1 dia, 0.249 min 0.250 max in. 1 dia, 0.305 min 0.315 max in. 1 dia
01-182-6272
Escutcheon Plate
Marked w/this side up per class a on plate face; hole dia 0.296/0.303 in.; o/a lgth 3.480/3.520 in.; c to c distance between holes 2.750/2.770 in.
01-182-6408
Spring Tension Clip
01-182-6490
Access Cover
Used on aero space gearbox r/n 1619118. 0.540" inside diameter 0.857" outside diameter
01-182-6669
Angle Bracket
2nd leg contains a nut-plate angle
01-182-6671
Angle Bracket
1st leg contains a nut-plate angle
01-182-6672
Angle Bracket
2nd leg contains a nut-plate angle
01-182-6673
Angle Bracket
2nd leg contains 2nut-plates angle
01-182-6674
Angle Bracket
Angle
01-182-6675
Angle Bracket
Angle
01-182-6676
Angle Bracket
1st leg contains 2 spacers angle
01-182-6730
Access Cover
Used on f-16c/d usaf aircraft. plies 1-5 fms-3015, plies 1-6 fms-1025, class 4; process, bond
01-182-6732
Access Cover
Used on f-16c/d usaf aircraft. plies 1-5 fms-3015, plies 1-6 fms-1025, class 4; process, bond
01-182-6813
Loop Clamp
Triple hinged clamp, contains 2 holes as loop inside diameter, 0.231 in. min to 0.239 in. max loop inside diameter, F118 engine qualified
01-182-6814
Loop Clamp
0.500" overall width
01-182-7380
Helical Compression Spr Retainer
Irregular
01-182-7381
Nut And Bolt Locking Plate
01-182-7387
Retaining Strap
0.060" material thickness contains 2 mounting slots, 0.210 in. min to 0.230 in. max slot width, center arch contains a nut-plate tapered arch
01-182-7389
Helical Compression Spring Seat
01-182-7390
Helical Compression Spring Seat
01-182-7520
Rod End Clevis
Used on m992,nsn 2350011104660. clevis
01-182-7556
Mending Plate
