9686M61P17: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 18.174 INCHES MINIMUM AND 18.194 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 1.280 INCHES MINIMUM AND 1.300 INCHES MAXIMUM IN, end_item_identification: TF-39ENGINE TO 2J-TF39-4 FIG 51 IND-154, engine_section_location: COMPRESSOR, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-474-1288, 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 | 18.174 INCHES MINIMUM AND 18.194 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| overall_length | 1.280 INCHES MINIMUM AND 1.300 INCHES MAXIMUM IN |
| end_item_identification | TF-39ENGINE TO 2J-TF39-4 FIG 51 IND-154 |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | AGAV |
| NSN | 2840-01-474-1288 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| DIAMETER | 18.174 INCHES MINIMUM AND 18.194 INCHES MAXIMUM IN |
| OVERALL LENGTH | 1.280 INCHES MINIMUM AND 1.300 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| END ITEM IDENTIFICATION | TF-39ENGINE TO 2J-TF39-4 FIG 51 IND-154 |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.