6888722: SEAL,METALLIC,AIRCRAFT GAS TURBI.
SEAL,METALLIC,AIRCRAFT GAS TURBI. Key specifications include diameter: 6.143 INCHES MINIMUM AND 6.155 INCHES MAXIMUM IN, material: STEEL OVERALL, overall_length: 3.230 INCHES MINIMUM AND 3.260 INCHES MAXIMUM IN, special_features: T.O. 2J-TF41-4, FIG 102, IND 1; HIGH PRESSURE COMPRESSOR ROTOR, HP TURBINE SHAFT AND REAR THRUST BEARING, end_item_identification: ACFT ENGINE NO.
TF-41, engine_section_location: HIGH PRESSURE COMPRESSOR. This part is cataloged in the U.S. Government catalog under NSN 2840-01-044-6109, 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 | 6.143 INCHES MINIMUM AND 6.155 INCHES MAXIMUM IN |
| material | STEEL OVERALL |
| overall_length | 3.230 INCHES MINIMUM AND 3.260 INCHES MAXIMUM IN |
| special_features | T.O. 2J-TF41-4, FIG 102, IND 1; HIGH PRESSURE COMPRESSOR ROTOR, HP TURBINE SHAFT AND REAR THRUST BEARING |
| end_item_identification | ACFT ENGINE NO. TF-41 |
| engine_section_location | HIGH PRESSURE COMPRESSOR |
| criticality_code_justification | ABHP AND ABMZ AND FEAT |
| part_name_assigned_by_controlling_agency | ORIGINAL NAME SEAL,SLEEVE,THRUST |
| NSN | 2840-01-044-6109 |
| CRITICALITY CODE JUSTIFICATION | ABHP AND ABMZ AND FEAT |
| DIAMETER | 6.143 INCHES MINIMUM AND 6.155 INCHES MAXIMUM IN |
| OVERALL LENGTH | 3.230 INCHES MINIMUM AND 3.260 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE COMPRESSOR |
| SPECIAL FEATURES | T.O. 2J-TF41-4, FIG 102, IND 1; HIGH PRESSURE COMPRESSOR ROTOR, HP TURBINE SHAFT AND REAR THRUST BEARING |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SEAL,SLEEVE,THRUST |
| END ITEM IDENTIFICATION | ACFT ENGINE NO. TF-41 |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.