4055257CLC: CASE,TURBINE,AIRCRAFT GAS TURBIN.
CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include material: STEEL OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 5.136 INCHES MINIMUM AND 5.140 INCHES MAXIMUM IN, special_features: T.O. 2J-F100-14, FIG 122, IND 27;1ST STG TURBINE DISK & FRONT CASE, end_item_identification: ACFT ENG F100, engine_section_location: TURBINE.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-101-8701, 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 | STEEL OVERALL |
| design_type | AXIAL COMPRESSOR |
| overall_length | 5.136 INCHES MINIMUM AND 5.140 INCHES MAXIMUM IN |
| special_features | T.O. 2J-F100-14, FIG 122, IND 27;1ST STG TURBINE DISK & FRONT CASE |
| end_item_identification | ACFT ENG F100 |
| engine_section_location | TURBINE |
| criticality_code_justification | APGF AND CZBJ AND FEAT |
| material_document_and_classification | AMS 5663 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | CASC AND DUCT SET, TURBINE |
| NSN | 2840-01-101-8701 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5663 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 5.136 INCHES MINIMUM AND 5.140 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 122, IND 27;1ST STG TURBINE DISK & FRONT CASE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CASC AND DUCT SET, TURBINE |
| END ITEM IDENTIFICATION | ACFT ENG F100 |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.