4059312: CASE,DIFFUSER,AIRCRAFT GAS TURBI.
CASE,DIFFUSER,AIRCRAFT GAS TURBI. Key specifications include diameter: 28.245 INCHES MINIMUM AND 28.265 INCHES MAXIMUM IN, design_type: AXIAL COMPRESSOR, overall_length: 17.818 INCHES MINIMUM AND 17.822 INCHES MAXIMUM IN, hardness_rating: 36.0 ROCKWELL C NOMINAL OUTER CASE, end_item_identification: F100-PW-100/200 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: DIFFUSER. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-130-2407, 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 | 28.245 INCHES MINIMUM AND 28.265 INCHES MAXIMUM IN |
| design_type | AXIAL COMPRESSOR |
| overall_length | 17.818 INCHES MINIMUM AND 17.822 INCHES MAXIMUM IN |
| hardness_rating | 36.0 ROCKWELL C NOMINAL OUTER CASE |
| end_item_identification | F100-PW-100/200 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | DIFFUSER |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME CASE,COMBUSTION CHAMBER,AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-130-2407 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| HARDNESS RATING | 36.0 ROCKWELL C NOMINAL OUTER CASE |
| DIAMETER | 28.245 INCHES MINIMUM AND 28.265 INCHES MAXIMUM IN |
| OVERALL LENGTH | 17.818 INCHES MINIMUM AND 17.822 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | DIFFUSER |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME CASE,COMBUSTION CHAMBER,AIRCRAFT GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | F100-PW-100/200 AIRCRAFT GAS TURBINE ENGINE |
No substitute or cross-reference records for this part.