4086505: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 15.795 INCHES MINIMUM AND 15.805 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_width: 2.934 INCHES MINIMUM AND 2.944 INCHES MAXIMUM IN, special_features: SHOT-PEENED IN BORE AREA FOR IMPROVED DURABILITY, end_item_identification: F100PW100/200/220C/220, engine_section_location: LOW PRESSURE TURBINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-469-1113, 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.
| diameter | 15.795 INCHES MINIMUM AND 15.805 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| stage_number | 4 |
| overall_width | 2.934 INCHES MINIMUM AND 2.944 INCHES MAXIMUM IN |
| special_features | SHOT-PEENED IN BORE AREA FOR IMPROVED DURABILITY |
| end_item_identification | F100PW100/200/220C/220 |
| engine_section_location | LOW PRESSURE TURBINE |
| material_document_and_classification | PWA1016 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| part_name_assigned_by_controlling_agency | SEAL-AIR,TURBINE,4TH STAGE |
| NSN | 2840-01-469-1113 |
| STAGE NUMBER | 4 |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1016 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 15.795 INCHES MINIMUM AND 15.805 INCHES MAXIMUM IN |
| OVERALL WIDTH | 2.934 INCHES MINIMUM AND 2.944 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| SPECIAL FEATURES | SHOT-PEENED IN BORE AREA FOR IMPROVED DURABILITY |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | SEAL-AIR,TURBINE,4TH STAGE |
| END ITEM IDENTIFICATION | F100PW100/200/220C/220 |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.