grip length 4.2-4.22 detent to tapered end distance 0.46-0.51 steel material hardness rating 40 rockwell c minimum shank and spindle

accommodated shaft maximum rated speed 1000 feet per minute housing bore diameter 2.375

length: 2.567 width: 1.875 holder

bearing and fulcrum bore for aircraft use

panel accommodation hole diameter 0.312-0.317 length 1.69 diameter 0.37

panel accommodation hole diameter 0.312-0.317

length 0.5 insert size 0.562-12 unc class 2a full internal thread length 0.07

thread size 3-16 screw thread series designator unj

seat angle 8.5 degrees 1st end maximum operating temp 135 degree celsius single response

transistor modified nsn 5961000054427.

circuit card nsn 5998000054369.

length: 1.50 height: 0.50 encased

terminal length 1.5 power dissipation rating in watts 0.062 free air

actuated fuel pump nsn 2910000055059.

gasket nsn 5330000054611.

sectional height cross 0.067-0.073 center hole diameter 5.71-5.73 rubber material

terminal length 1.5 power dissipation rating in watts 0.25 free air

terminal length 1.5 terminal diameter 0.025

terminal length 1.5 electrical resistance 750 kilohms

inside diameter 16.814-16.838 outside diameter 17.006-17.016

inside diameter 1.09-1.25 fastening device type slotted hexagon head screw width 0.5-0.56 steel material

steel 5 teeth 0.25 in. w of teeth corners and edges chamfered 45 deg by 0.062 in. lg grooved booth sides 1.25 in. w o.094 in. long 0.031 in. deep 0.312 in. thk

resistance tolerance in percent -1 to 1 electrical resistance 674 kilohms

door latch used on aircraft model av-8a

retaining ring nsn 5325000054380.

hole diameter 0.167-0.175 inside corner radius 0.03 length 1.625 width 1.625 copper material

control unit nsn 1680003495216.

thread size 0.75 all ends seat angle 37 degrees 1st end and 2nd steel material leg length 1.25 inches 1st end and 2nd