2840PL0697074: SHROUD SEGMENT,TURBINE,AIRCRAFT.
SHROUD SEGMENT,TURBINE,AIRCRAFT. Key specifications include material: NICKEL ALLOY OVERALL, stage_number: 11, overall_length: 17.034 INCHES MINIMUM AND 17.044 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-54, FIG 88 IND 19, end_item_identification: ACFT ENG F100PW0229, engine_section_location: COMPRESSOR.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-356-9500, 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 | 11 |
| overall_length | 17.034 INCHES MINIMUM AND 17.044 INCHES MAXIMUM IN |
| special_features | T.O. 2J-F100-54, FIG 88 IND 19 |
| end_item_identification | ACFT ENG F100PW0229 |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-356-9500 |
| STAGE NUMBER | 11 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 17.034 INCHES MINIMUM AND 17.044 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-F100-54, FIG 88 IND 19 |
| END ITEM IDENTIFICATION | ACFT ENG F100PW0229 |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.