4081554: SHROUD,COMPRESSOR,AIRCRAFT GAS T.
SHROUD,COMPRESSOR,AIRCRAFT GAS T. Key specifications include material: NICKEL ALLOY OVERALL, overall_length: 1.658 INCHES NOMINAL IN, special_features: T.O. 2J-F100-24, FIG 143; USED ONTHE 4000 CYCLE 220E ENGINE CORE ONLY, end_item_identification: F100PW220E AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMPRESSOR, criticality_code_justification: FEAT.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-426-6695, 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 OVERALL |
| stage_number | 4 |
| overall_length | 1.658 INCHES NOMINAL IN |
| special_features | T.O. 2J-F100-24, FIG 143; USED ONTHE 4000 CYCLE 220E ENGINE CORE ONLY |
| end_item_identification | F100PW220E AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | FEAT |
| NSN | 2840-01-426-6695 |
| STAGE NUMBER | 4 |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| OVERALL LENGTH | 1.658 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-24, FIG 143; USED ONTHE 4000 CYCLE 220E ENGINE CORE ONLY |
| END ITEM IDENTIFICATION | F100PW220E AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.