6022813: COMPRESSOR ROTOR,TURBO SUPERCHAR.
COMPRESSOR ROTOR,TURBO SUPERCHAR. Key specifications include length: 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT, material: ALUMINUM ALLOY 7075, overall_width: 1.250 INCHES NOMINAL IN, heat_treatment: T-6511 SOLUTION HEAT TREATED, first_tip_style: SQUARE END, special_features: ITEM IS A BLOWER,MINIATURE. This part is cataloged in the U.S.
Government catalog under NSN 9540-01-364-1592, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| material | ALUMINUM ALLOY 7075 |
| overall_width | 1.250 INCHES NOMINAL IN |
| heat_treatment | T-6511 SOLUTION HEAT TREATED |
| first_tip_style | SQUARE END |
| special_features | ITEM IS A BLOWER,MINIATURE |
| basic_shape_style | CHANNEL |
| left_inside_angle | 90.0 DEGREES NOMINAL |
| fabrication_method | EXTRUDED |
| right_inside_angle | 90.0 DEGREES NOMINAL |
| base_flange_thickness | 0.080 INCHES NOMINAL IN |
| left_side_flange_height | 0.630 INCHES NOMINAL IN |
| NSN | 9540-01-364-1592 |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| BASE FLANGE THICKNESS | 0.080 INCHES NOMINAL IN |
| LEFT SIDE FLANGE HEIGHT | 0.630 INCHES NOMINAL IN |
| HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| FILLET RADIUS WHERE RIGHT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL IN |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| OVERALL WIDTH | 1.250 INCHES NOMINAL IN |
| LEFT SIDE FLANGE THICKNESS | 0.080 INCHES NOMINAL IN |
| BASIC SHAPE STYLE | CHANNEL |
| RIGHT SIDE FLANGE HEIGHT | 2.000 INCHES NOMINAL IN |