00-395-9444
Threaded Spacing Standoff
00-395-9447
Solid Plain Disk
00-395-9457
Retaining Strap
Teletypewriter subassembly one clamp; one plate
00-395-9462
Threaded Spacing Standoff
Undercut, left end projection both ends right external thread
00-395-9483
Spring Holder
00-395-9900
Helical Compression Spring Seat
Used on f-15 aircraft passivate surface treated
00-395-9955
Helical Compression Spring Seat
Used on f-15 aircraft passivate surface treated
00-396-0126
Antipilferage Seal
00-396-2043
Access Door Hinge
Model f-15
00-396-2044
Access Door Hinge
Used on w/s:aircraft, eagle f-15. model f-15
00-396-2045
Access Door Hinge
Model f-15
00-396-2643
Helical Compression Spring Seat
0.5360" bore diameter seat
00-396-3112
Retaining Strap
0.563" overall length 0.313" overall width 0.020" material thickness nickel surface treated j
00-396-3393
Thumb Latch
Material:steel; surface treatment:phosphate;
00-396-3394
Resilient Mount Plate
00-396-3401
Synchro Clamp
0.250" hole diameter
00-396-3404
Flush Lock
Master key provision:not included;
00-396-3441
Catch Strike
0.625" overall length 0.625" overall width 0.062" material thickness chromate surface treated
00-396-3859
Double Angle Bracket
Anodize surface treated double angle
00-396-3911
Angle Bracket
Offset angle
00-396-4282
Mounting Bracket
00-396-4301
Mounting Bracket
0.217 in. dia 4 holes
00-396-4608
Helical Compression Spring Seat
00-396-4612
Helical Compression Spring Seat
0.1250" bore diameter seat
00-396-4635
Angle Bracket
Angle
00-396-4636
Angle Bracket
Angle
00-396-4678
Angle Bracket
Cadmium surface treated angle
00-396-4762
Mounting Plate
Two holes 0.339 in. min cadmium surface treated
00-396-4790
Angle Bracket
Bend r between legs 0.219 in. min 0.281 in. max; second hole in foot of second leg 0.281 in. min 0.344 in. max dia angle
00-396-4802
Loop Clamp
0.550" overall width 0.039" material thickness cadmium band surface treated multiple loop
00-396-4856
Helical Compression Spring Seat
00-396-4910
Angle Bracket
Angle
00-396-4913
Angle Bracket
Used on eng j-57. angle
00-396-4979
Mounting Bracket
00-396-4997
Angle Bracket
Used on engj-57. angle
00-396-5005
Angle Bracket
Used on eng j-57. cadmium surface treated angle
00-396-5248
Angle Bracket
One additonal hole in first leg; rockwell hardness c 25 to c 33 angle
00-396-5376
Grooved Clamp Coupling Ferrule
0.325" overall length
00-396-5381
Angle Bracket
Self-locking feature of nut must meet 2.0 pounds to 13.0 pound per in. toque when tested with 0.190-32 unf-3a bolt; joint of nut must withstand torque of 60.0 pounds per in. cadmium surface treated angle
00-396-5464
Double Angle Bracket
Cadmium surface treated double angle
00-396-5534
Mounting Bracket
Used on j-57 aircraft engine. material ams 6322 steel; 2.850 in. wd between center end holes; 0.745 in. lg between center outside holes
00-396-6919
Protective Dust And Moi Cap-plug
00-396-7624
Manual Control Lever
Used on C-47.
00-396-8475
Loop Clamp
Steel
00-396-8476
Loop Clamp
Used on acft model c118.
00-396-8665
Access Door Hinge
Contains 1 bushing, p/n NAS75-4-031
00-396-8666
Access Door Hinge
00-397-0143
Blank Panel
5.720" overall width 0.064" material thickness chromate zinc surface treated blank, plain design
