00-351-5112
Butt Hinge
2.5000" overall length 0.5000" material thickness
00-351-5166
Angle Bracket
Angle
00-351-5168
Swivel Caster
00-351-5360
Access Cover
Passivate surface treated
00-351-6764
Rod End Connector
Cadmium surface treated connector
00-351-6928
Angle Bracket
Zinc or zinc surface treated angle
00-351-6992
Loop Clamp
1.000" overall width 0.032" material thickness single loop
00-351-7006
Nut And Bolt Retainer
00-351-7390
Mounting Bracket
00-351-7831
Manual Control Lever
Material iron casting malleable grade i or ii spec qq-i-666
00-351-7903
Mounting Bracket
Used on balistics computer. steel; 8.000 in. lg; 6.000 in. w; four 0.250 by 0.531 in. mounting slots
00-351-7934
Rod End Clevis
3a rod connection thread class left-hand rod connection 0.344" rod connection thread length 0.125" hole diameter 0.187" overall width passivate surface treated unf rod connection thread series
00-351-8420
Butt Hinge Leaf
2.125" overall length 0.079" material thickness
00-351-8549
Butt Hinge
0.032" material thickness
00-351-8710
Protective Dust And Moisture Cap
Passivate surface treated
00-351-9756
Loop Clamp
T-bolt
00-352-0252
Key Blank
Steel, hexagon grip; 3 stamped grooves
00-352-0323
Loop Clamp
0.500" overall width 0.020" material thickness offset mount
00-352-0324
Retaining Strap
3.149" overall length 0.620" overall width 0.062" material thickness saddle arch
00-352-0367
Angle Bracket
Nut plate hole in first leg 0.195 in. nom dia distance from edge to center along width 0.500 in. distance from edge to center along length 0.250 in. lacquer surface treated angle
00-352-0553
Threaded Spacing Standoff
Stake 0.030 in. deep TW0 places left internal thread
00-352-0602
Retaining Strap
3.291" overall length 0.500" overall width 0.064" material thickness saddle arch
00-352-0603
Retaining Strap
3.291" overall length 0.500" overall width 0.064" material thickness saddle arch
00-352-1912
Access Cover
0.375" hole diameter one end dimpled
00-352-2267
Mounting Bracket
Used on f-100 aircraft engine. titanium alloy, AMS4928, 0.211 in. min, 0.217 in. max, dia offour mtg holes located on 1.200 in. by 3.500 in. centers
00-352-3200
Helical Compression Spring Seat
0.4570" bore diameter nickel surface treated seat
00-352-3223
Helical Compression Spring Seat
0.4290" bore diameter
00-352-3326
Dirt And Liquid Deflector
00-352-3787
Access Cover
Used on aircraft model c5a.
00-352-3869
Shimmy Damper
00-352-4489
Access Cover
W/bolt
00-352-5507
Helical Compression Spring Seat
Used on f-15 aircraft passivate surface treated
00-352-5765
Rod End Connector
Each enddrilled 0.688 in.
00-352-5853
Rod End Clevis
2b rod connection thread class right-hand rod connection 1.125" rod connection thread length 0.500" hole diameter 1.125" overall width cadmium surface treated clevis unf rod connection thread series
00-352-6619
Resilient General Purpose Mount
00-352-6720
Loop Clamp
1.250" overall width 0.250" material thickness
00-352-7378
Spring Holder
00-352-7480
Helical Compression Spring Seat
00-352-7523
Dirt And Liquid Deflector
2.242" inside diameter 2.995" outside diameter 0.060" material thickness round, flanged
00-352-7541
Rod End Connector
2g rod connection thread class right-hand rod connection 9.500" rod connection thread length copper surface treated connector acme rod connection thread series
00-352-7548
Rod End Connector
2a rod connection thread class right-hand rod connection 4.125" rod connection thread length 12 rod connection thread quantity per inch 1.875 in.min, 1.880 in.max dia by 1.000 in.lg thd relief under tongue section connector un rod connection thread series
00-352-7681
Nut And Bolt Locking Plate
Radius
00-352-7772
Nut And Bolt Locking Plate
Radius
00-352-7779
Loop Clamp
0.875" overall width 0.250" material thickness single loop
00-352-8292
Grooved Clamp Coupling Ferrule
0.750" overall length
00-352-8560
Nut And Bolt Locking Plate
Radius
00-352-8561
Nut And Bolt Locking Plate
Radius
00-352-8584
Loop Clamp
0.781" overall width
00-352-8627
Solid Plain Disk
