4083057: LINER,COMBUSTION CHAMBER,AIRCRAF.
LINER,COMBUSTION CHAMBER,AIRCRAF. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 1.456 INCHES NOMINAL IN, overall_length: 6.157 INCHES MINIMUM AND 6.269 INCHES MAXIMUM IN, special_features: THERMAL BARRIER COATING ADDED PER ECN 95QA006, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMBUSTION CHAMBER. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-421-9737, 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 |
| overall_width | 1.456 INCHES NOMINAL IN |
| overall_length | 6.157 INCHES MINIMUM AND 6.269 INCHES MAXIMUM IN |
| special_features | THERMAL BARRIER COATING ADDED PER ECN 95QA006 |
| end_item_identification | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMBUSTION CHAMBER |
| criticality_code_justification | STDC AND CZBJ AND ABHP AND ABMK AND FEAT |
| material_document_and_classification | PWA1475 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | LINER SEGMENT,COMBUSTION CHAMBER DUCT, 1 OD |
| surface_treatment_document_and_classification | SPEC PWA 265-1 MFR REF SINGLE TREATMENT RESPONSE OVERALL |
| NSN | 2840-01-421-9737 |
| SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | SPEC PWA 265-1 MFR REF SINGLE TREATMENT RESPONSE OVERALL |
| CRITICALITY CODE JUSTIFICATION | STDC AND CZBJ AND ABHP AND ABMK AND FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1475 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 6.157 INCHES MINIMUM AND 6.269 INCHES MAXIMUM IN |
| OVERALL WIDTH | 1.456 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| SPECIAL FEATURES | THERMAL BARRIER COATING ADDED PER ECN 95QA006 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | LINER SEGMENT,COMBUSTION CHAMBER DUCT, 1 OD |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.