4083564: CASE,DIFFUSER,AIRCRAFT GAS TURBI.
CASE,DIFFUSER,AIRCRAFT GAS TURBI. Key specifications include diameter: 28.330 INCHES MINIMUM AND 28.350 INCHES MAXIMUM IN, material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 13.940 INCHES MINIMUM AND 13.946 INCHES MAXIMUM IN, hardness_rating: 34.0 ROCKWELL C NOMINAL OVERALL, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-448-0656, 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.
| diameter | 28.330 INCHES MINIMUM AND 28.350 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 13.940 INCHES MINIMUM AND 13.946 INCHES MAXIMUM IN |
| hardness_rating | 34.0 ROCKWELL C NOMINAL OVERALL |
| end_item_identification | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | ABHP AND ABMZ AND CQFM |
| NSN | 2840-01-448-0656 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| HARDNESS RATING | 34.0 ROCKWELL C NOMINAL OVERALL |
| CRITICALITY CODE JUSTIFICATION | ABHP AND ABMZ AND CQFM |
| DIAMETER | 28.330 INCHES MINIMUM AND 28.350 INCHES MAXIMUM IN |
| OVERALL LENGTH | 13.940 INCHES MINIMUM AND 13.946 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.