Model: 1-140-590-09
Air Antifriction Bearing HousingSpecial Features:
Surface, phosphate ams 2481; 5.5635 in. O/a lg.; 6.312 in. Min., 6.313 in. Max. O/a dia.; flange located on one end; rockwell c scale 23 max hardness; 1.380 in. Min., 1.390 in. Max. O/a lg.; 6.440 in. O/a dia.; 0.420 in. W of face; 1st step 0.670 in. Min., 0.690 in. Max. Lg.; 3.800 in. Od; 2nd step 0.140 in. Min., 0.150 in. Max. Lg; 4.901 in. Min., 4.903 in. Max. Od; 3rd step 0.140 in. Lg.; 5.000 in. Od; bore, 3.140 in. Id; 0.820 in. Min., 0.830 in. Max. Dp; counterbore, 4.620 in. Id; 0.560 in. Dp; flange located on opposite end; rockwell c scale 23 max. Hardness; 1.430 in. O/a lg; 6.060 in. O/a dia.; 0.320 in. W of face; 1st step 0.780 in. Min., 0.790 in. Max. Lg.; 3.800 in. Od; 2nd step 0.180 in. Min., 0.200 in.Max. Lg.; 4.901 in. Min., 4.903 in. Max. Od; 3rd step 0.130 in. Min., 0.140 in. Max. Lg.; 5.000 in. Od; bore, 3.140 in. Id; 0.780 in. Min., 0.790 in. Max. Dp; counterbor, 4.620 in. Id; 0.460 in. Dp; each flang, 15 holes 0.440 in. Dia.
Properties:
A housing designed to surround, retain, support, and protect an antifriction bearing mounted on a shaft, turbine, aircraft gas turbine engine. it may also act as a sump to collect the lubricant to be pumped back to the tank.
Part 1-140-590-09 NSN 2840-01-011-5045
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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