terminal length 1.5 center to center distance between terminals parallel to length 0.962

crank specs bore diameter 0.502 bore length 1.31 titanium material used on aircraft outer wing slat mechanism

semiconductor material silicon

special screw nsn 5305000054412.

special collar nsn 6610000054409.

stabilizer computer nsn 6615000054367.

special seal nsn 5330000054024.

body diameter 0.087 body length 0.25

circuit card specs length 8 height 0.093 width 6.45

terminal length 1.5 insulation resistance at reference temp 100000 megohms body length 0.44 body height 0.16 nonderated operating temp 125 degree celsius maximum

bore diameter 0.439 bore length 0.89 titanium material

integrated circuit nsn 5962000054077.

voltage rating 120 volts cabinet operating temp range +36/+41 degree fahrenheit

motor specs height 5.75 length 10.5 width 5.75

conductor size 10 awg material thickness 0.02 largest width 0.125

coupling nsn 3010000055071.

terminal length 1.25 temp coefficient of capacitance range per section in ppm per degree celsius -0 to 70 single section body length 0.43 body height 0.15 nonderated operating temp 125 degree celsius maximum

cross-sectional shape style 116 irregular shape from old fiig a03200

terminal length 1.5 insulation resistance at reference temp 25000 megohm-microfarads

bore diameter 0.502 bore length 1.31 titanium material

steel ams 6427 rod end titanium alloy ams 4928 rod end vacuum cadmium plated 5.01 in. between bearing centerlines

titanium material

dissipator assembly consists of holder 1 heat dissipator 2 thermistor 1

nonpile-up structural design

electrical coil nsn 5950000054569.

end item identification av-8a aircraft

end item identification aircraft model av-8a

body length 0.188 body width 0.188 body height 0.094