4075413-01: CASE,COMBUSTION CHAMBER,AIRCRAFT.
CASE,COMBUSTION CHAMBER,AIRCRAFT. Key specifications include material: NICKEL ALLOY OUTER CASE, design_type: COMPRESSOR, overall_length: 17.024 INCHES NOMINAL IN, end_item_identification: F100PW0229 AIRCRAFT ENGINE, engine_section_location: COMPRESSOR, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-310-2458, 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 | NICKEL ALLOY OUTER CASE |
| design_type | COMPRESSOR |
| overall_length | 17.024 INCHES NOMINAL IN |
| special_features | INCLUDES 4-9 STAGES; USE ONLY ON 4077081-08,4077081-07,4079598-01,4079598-04,4080084-03,4080084-04,AND 4080302-02; T.O. 2J-F100-54 |
| end_item_identification | F100PW0229 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-310-2458 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 17.024 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | INCLUDES 4-9 STAGES; USE ONLY ON 4077081-08,4077081-07,4079598-01,4079598-04,4080084-03,4080084-04,AND 4080302-02; T.O. 2J-F100-54 |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE |
| MATERIAL | NICKEL ALLOY OUTER CASE |
No substitute or cross-reference records for this part.