3011764: PISTON ASSEMBLY,COMPRESSOR BLEED.
PISTON ASSEMBLY,COMPRESSOR BLEED. Key specifications include material: STEEL ALLOY OVERALL, point_type: SPLIT, point_angle: 135.0 DEGREES NOMINAL, shank_style: STRAIGHT ROUND, flute_length: 1.500 INCHES NOMINAL IN, overall_length: 2.625 INCHES NOMINAL IN. This part is cataloged in the U.S.
Government catalog under NSN 2840-00-587-3978, 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 ALLOY OVERALL |
| point_type | SPLIT |
| point_angle | 135.0 DEGREES NOMINAL |
| shank_style | STRAIGHT ROUND |
| flute_length | 1.500 INCHES NOMINAL IN |
| flute_quantity | 2 |
| overall_length | 2.625 INCHES NOMINAL IN |
| shank_diameter | 0.109 INCHES NOMINAL IN |
| special_features | COBALT/HSS, JOBBERS LG;FRACTIONAL SIZE 7/64 |
| cutting_end_style | GENERAL PURPOSE |
| nominal_cutting_diameter | 0.1094 INCHES IN |
| cutting_rotation_direction | RIGHT-HAND |
| NSN | 2840-00-587-3978 |
| GENERAL CHARACTERISTICS ITEM DESCRIPTION | ASSEMBLY C/O INSERT P/N MS124735 PISTON P/N 3011763 |
| END ITEM IDENTIFICATION | T400-CP-400 GAS TURBINE ENGINE,UH-IN HELICOPTER |
No substitute or cross-reference records for this part.