L4100265-011: CASE,TURBINE,AIRCRAFT GAS TURBIN.
CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include design_type: AXIAL COMPRESSOR, special_features: CONSISTS OF ENGINE SHROUD PANELS AND SUPPORTS, end_item_identification: ACFT ENG F101, engine_section_location: TURBINE, reference_data_and_literature: T.O. 2J-F101-4, FIG 83, IND 12, criticality_code_justification: FEAT AND CZBJ.
This part is cataloged in the U.S. Government catalog under NSN 2840-01-187-8260, 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.
| design_type | AXIAL COMPRESSOR |
| special_features | CONSISTS OF ENGINE SHROUD PANELS AND SUPPORTS |
| end_item_identification | ACFT ENG F101 |
| engine_section_location | TURBINE |
| reference_data_and_literature | T.O. 2J-F101-4, FIG 83, IND 12 |
| criticality_code_justification | FEAT AND CZBJ |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME INSULATION BLANKET,THERMAL,AIRCRAFT GAS TURBINE ENGINE |
| NSN | 2840-01-187-8260 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F101-4, FIG 83, IND 12 |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | CONSISTS OF ENGINE SHROUD PANELS AND SUPPORTS |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME INSULATION BLANKET,THERMAL,AIRCRAFT GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | ACFT ENG F101 |
No substitute or cross-reference records for this part.