2840PL0864836: SUPPORT,TURBINE COMPONENT,AIRCRA.
SUPPORT,TURBINE COMPONENT,AIRCRA. Key specifications include material: NICKEL ALLOY, overall_length: 3.773 INCHES MINIMUM AND 3.781 INCHES MAXIMUM IN, inside_diameter: 23.962 INCHES MINIMUM AND 23.966 INCHES MAXIMUM IN, outside_diameter: 26.217 INCHES MINIMUM AND 26.221 INCHES MAXIMUM IN, special_features: USE ONLY ON P/NS 4084517-700 AND 4083015-701; LOCATED NEAR REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY, end_item_identification: F100-PW-229 AIRCRAFT GAS TURBINE ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-448-7511, 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_length | 3.773 INCHES MINIMUM AND 3.781 INCHES MAXIMUM IN |
| inside_diameter | 23.962 INCHES MINIMUM AND 23.966 INCHES MAXIMUM IN |
| outside_diameter | 26.217 INCHES MINIMUM AND 26.221 INCHES MAXIMUM IN |
| special_features | USE ONLY ON P/NS 4084517-700 AND 4083015-701; LOCATED NEAR REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY |
| end_item_identification | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| reference_data_and_literature | T.O. 2J-F100-54, FIG 99, IND 34 |
| criticality_code_justification | ABHP AND ABKV AND AARX AND FEAT |
| material_document_and_classification | PWA1198 MFR REF SINGLE MATERIAL RESPONSE |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME SUPPORT TURBINE DUCT AND VANE, ASSEMBLY OF |
| NSN | 2840-01-448-7511 |
| CRITICALITY CODE JUSTIFICATION | ABHP AND ABKV AND AARX AND FEAT |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F100-54, FIG 99, IND 34 |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1198 MFR REF SINGLE MATERIAL RESPONSE |
| OVERALL LENGTH | 3.773 INCHES MINIMUM AND 3.781 INCHES MAXIMUM IN |
| OUTSIDE DIAMETER | 26.217 INCHES MINIMUM AND 26.221 INCHES MAXIMUM IN |
| INSIDE DIAMETER | 23.962 INCHES MINIMUM AND 23.966 INCHES MAXIMUM IN |
| SPECIAL FEATURES | USE ONLY ON P/NS 4084517-700 AND 4083015-701; LOCATED NEAR REAR COMPRESSOR DRIVE TURBINE ROTOR AND STATOR ASSY |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SUPPORT TURBINE DUCT AND VANE, ASSEMBLY OF |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT GAS TURBINE ENGINE |
| MATERIAL | NICKEL ALLOY |