Model: 1-100-417-02
Tu Axial Compressor Disk And HubSpecial Features:
Titanium alloy, m3400 fscm 91547, rockwell c scale 36 max hardness, painted finish, p6441 fscm 91547, 2.351 in. Nom o/a lg, tapered od disk, 7.274 in. Min, 7.284 in. Max largest od disk, 7.146 in. Min, 7.156 in. Max smallest od disk, 0.677 in. Min, 0.682 in. Max lg disk, 38 blade grooves equally spaced on outer periphery, 2 hubs, 1st end 4.430 in. Min, 4.440 in. Max od hub, 1.202 in. Min, 1.212 in. Max distance from 1st end to disk, 2nd end 4.421 in. Min, 4.422 in. Max od hub, 0.453 in. Min, 0.466 in. Max distance from 2nd end to disk, 4.082 in. Min, 4.087 in. Max diameter bore
Properties:
Inc 61831 cancelled/replaced by ,inc 50561, fiig a10700, app-key f ,inc 50562, fiig a10700, app-key f ,inc 50563, fiig a10700, app-key f ,inc 50564, fiig a10700, app-key f ,inc 50565, fiig a10700, app-key f ,inc 50566, fiig a10700, app-key f ,on 021513 ~(all except usa). A disk having provisions on the outer periphery for attaching compressor blades and an integral hub that provides support and alignment for the compressor rotor. See also disk,axial compressor,turbine engine.
Part 1-100-417-02 NSN 2840-00-979-8432
Material Classification
Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicatorsPackaging & Shipping
Freight Classification
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Schedule B and Export
- Schedule B: 8411997050
- SITC: 71499
- End Use: Engines and turbines for military aircraft
- NAICS: 336412
- USDA: 1
Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft
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