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2b all facilities hole
cylindrical frame
0.250in. power takeoff facility hole ⁓1/4"
1.250in.
1.620in.
steel
nickel
1.562in.
0.180in.
0.310in. and 0.405in.
400.0
fully inclosed
1
continuous
circumference
115.0 ac
1 bracket and 3 threaded hole
150.0 milliamperes
40 all facilities hole
pull
6.00 ounces
internal threads
0.150in.
0.112in. all facilities hole ⁓1/8"
isosceles triangle
0.500in.
material document and classification: DAMIL-S-4040, surface treatment document and classification: DAMIL-C-26074
MIL-S-4040 mil spec single material response
MIL-C-26074 mil spec single treatment response
06481-935084 drawing (this is the basic governing drawing, such as a contractor drawing, original equipment manufacturer drawing, etc.; excludes any specification, standard or other document that may be referenced in a basic governing drawing)
unc all facilities hole
2 solderless lug
1EA
Unc all facilities hole
40 all facilities hole
0.250 inches minimum power takeoff facility hole
2b all facilities hole
Schedule B number: 8412909080
nmfc 063100
Parts of engines and motors
FSC 5945 ⁓ Relays and solenoids
Excluding contractors.
unc all facilities hole thread series material document 40 all facilities hole thread quantity per inch 0.250" power takeoff facility hole thread length 2b all facilities hole thread class
1. | 935084-0002 | Cage 06481 |
Nothing similar to this part number was found in our inventory
An item consisting of one or more coils surrounding an iron core. the coil(s) and the core are moveable in relation to each other. the axial or rotary movement is a result of the magnetic flux of the coil. it is designed to convert electrical energy into mechanical energy. it does not include switch contacts. see also relay, electromagnetic, and electromagnetic actuator.