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resistance tolerance in percent -5 to 5 ambient temp in deg celsius at full rated power 70 electrical resistance 91 ohms terminal length 1.5

steel material spring free length 0.63

length of aircraft former series 32-32030 is 32.75 inches. made of aluminum alloy 2024. aircraft mission design series: f-4.

fastener length: 0.359 to 0.391 minimum tensile strength: 125000 pounds per square inch

nut height 0.938 minimum and 1 maximum nominal thread size 1.125 steel material width across flats 1.788 minimum and 1.82 maximum

voltage rating 1000 ac maximum rated working voltage all conductors temp rating 260 degrees celsius

steel material spring free outside diameter 0.93

used to support front inlet fan module during installation or removal from engine positioned in horizontal work stand

steel material

length 1.1 minimum and 1.12 maximum

4.81 in. o/a lg 1.38 in. o/a dia 1.113 in. id

1x and 2x and 3x and 4x and 5x and 6x and 7x magnification vertical body tube position

material thickness: 0.368 to 0.37 material document and classification: aluminum alloy qq-a-200/11 t6 or qq-a-225/9 t6; surface finish: anodized mil-a-8625; fsc application data: handle assembly ejection seat aircraft

transistor nsn 5961000059568.

bracket system consists of 4 spring clips 27 terminals 2 washers

inductance rating 1.4 microhenries minimum single component single winding and 2.3 microhenries maximum single component single winding winding operating current 5.1 amperes ac maximum single component single winding

rubber material peripheral diameter 4.5

aluminum material countersink angle: 99 degrees to 101 degrees

length 1.865 copper material

hole diameter: 0.428 to 0.448 aperture width: 2.99 to 3.01