2840PL0788967: 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, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE, engine_section_location: COMBUSTION CHAMBER, criticality_code_justification: ABHP AND CZBJ AND FEAT. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-448-7038, 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 | T.O. 2J-F100-54, FIG 100, IND 20; USE ONLY ON P/N 4084089 AND 4083194; 96QA074 IMPROVED DURABILITY LINER SEGMNET THRU NORMAL ATTRITION OF PARTS |
| end_item_identification | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| engine_section_location | COMBUSTION CHAMBER |
| criticality_code_justification | ABHP AND CZBJ AND FEAT |
| material_document_and_classification | PWA1475 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME LINER SEGMENT,COMBUSTION CHAMBER DUCT |
| NSN | 2840-01-448-7038 |
| CRITICALITY CODE JUSTIFICATION | ABHP AND CZBJ 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 | T.O. 2J-F100-54, FIG 100, IND 20; USE ONLY ON P/N 4084089 AND 4083194; 96QA074 IMPROVED DURABILITY LINER SEGMNET THRU NORMAL ATTRITION OF PARTS |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME LINER SEGMENT,COMBUSTION CHAMBER DUCT |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | NICKEL ALLOY OVERALL |