4084773: CASE,TURBINE,AIRCRAFT GAS TURBIN.
CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include diameter: 30.910 INCHES MINIMUM AND 30.920 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 6.784 INCHES MINIMUM AND 6.790 INCHES MAXIMUM IN, end_item_identification: F100-PW-100 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-448-1008, 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 | 30.910 INCHES MINIMUM AND 30.920 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 6.784 INCHES MINIMUM AND 6.790 INCHES MAXIMUM IN |
| end_item_identification | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | TURBINE |
| criticality_code_justification | ABHP AND ABMZ AND CZBJ |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME CASE,TURBINE REAR |
| NSN | 2840-01-448-1008 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | ABHP AND ABMZ AND CZBJ |
| DIAMETER | 30.910 INCHES MINIMUM AND 30.920 INCHES MAXIMUM IN |
| OVERALL LENGTH | 6.784 INCHES MINIMUM AND 6.790 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME CASE,TURBINE REAR |
| END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.