9972M33P05: BEARING,ROLLER,CYLINDRICAL.
The BEARING,ROLLER,CYLINDRICAL is a the manufacturer industrial component. Key specifications include material: STEEL COMP M50 OUTER RING, bore_shape: STRAIGHT, bore_diameter: 1.9683 INCHES MINIMUM AND 1.9685 INCHES MAXIMUM IN, overall_width: 0.7824 INCHES MINIMUM AND 0.7874 INCHES MAXIMUM IN, surface_finish: GROUND, locating_feature: NONLOCATING. This part is cataloged in the U.S.
Government catalog under NSN 3110-01-160-9079, 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.
| material | STEEL COMP M50 OUTER RING |
| bore_shape | STRAIGHT |
| bore_diameter | 1.9683 INCHES MINIMUM AND 1.9685 INCHES MAXIMUM IN |
| overall_width | 0.7824 INCHES MINIMUM AND 0.7874 INCHES MAXIMUM IN |
| surface_finish | GROUND |
| locating_feature | NONLOCATING |
| style_designator | SINGLE ROW, NON-LOCATING, TWO LIP INNER RING, CYLINDRICAL OUTER RING, SEPARABLE |
| internal_clearance | 0.0030 INCHES MINIMUM RADIAL AND 0.0036 INCHES MAXIMUM RADIAL IN |
| end_item_identification | ACFT ENG F101,GE102,F110,GE100 |
| overall_outside_diameter | 3.7399 INCHES MINIMUM AND 3.7402 INCHES MAXIMUM IN |
| retainer_fabrication_method | FORGED |
| criticality_code_justification | FEAT |
| NSN | 3110-01-160-9079 |
| RETAINER FABRICATION METHOD | FORGED |
| INTERNAL CLEARANCE | 0.0030 INCHES MINIMUM RADIAL AND 0.0036 INCHES MAXIMUM RADIAL IN |
| LOCATING FEATURE | NONLOCATING |
| SURFACE FINISH | GROUND |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| STYLE DESIGNATOR | SINGLE ROW, NON-LOCATING, TWO LIP INNER RING, CYLINDRICAL OUTER RING, SEPARABLE |
| OVERALL WIDTH | 0.7824 INCHES MINIMUM AND 0.7874 INCHES MAXIMUM IN |
| OVERALL OUTSIDE DIAMETER | 3.7399 INCHES MINIMUM AND 3.7402 INCHES MAXIMUM IN |
| BORE SHAPE | STRAIGHT |
| SPECIAL FEATURES | SILVER PLATE CAGE 0.0005-0.0015 THK PER AMS 2412;OUTER RING FLANGED ALL THE WAY AROUND AND SPURRED IN 3 PLACES,EQUALLY SPACED,FOR MOUNTING;EACH SPUR HAS 2 DRILLED HOLES,ONE TAPPED 0.190-32UNF-1B THRU PER MIL-S-7742,THE OPPOSITE HOLE BEING 0.284 IN. NOM THRU, THIS ITEM IS USED IN THE F118-101 AND F101-102 ENGINES ON THE INLET GEARBOX. FAILURE OF THIS ITEM CAN RESULT IN AN UNCOMMANDED INFLIGHT SHUTDOWN IN |