3038M79P02: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include diameter: 18.072 INCHES MINIMUM AND 18.082 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, overall_length: 0.775 INCHES MINIMUM AND 0.795 INCHES MAXIMUM IN, special_features: T.O. 2J-TF39-4;HONEYCOMBED, material_thickness: 0.560 INCHES MINIMUM AND 0.600 INCHES MAXIMUM IN, end_item_identification: ACFT ENG.
TF-39. This part is cataloged in the U.S. Government catalog under NSN 2840-00-009-4084, 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 | 18.072 INCHES MINIMUM AND 18.082 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| overall_length | 0.775 INCHES MINIMUM AND 0.795 INCHES MAXIMUM IN |
| special_features | T.O. 2J-TF39-4;HONEYCOMBED |
| material_thickness | 0.560 INCHES MINIMUM AND 0.600 INCHES MAXIMUM IN |
| end_item_identification | ACFT ENG. TF-39 |
| engine_section_location | TURBINE |
| material_document_and_classification | AMS 5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-00-009-4084 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| DIAMETER | 18.072 INCHES MINIMUM AND 18.082 INCHES MAXIMUM IN |
| OVERALL LENGTH | 0.775 INCHES MINIMUM AND 0.795 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| MATERIAL THICKNESS | 0.560 INCHES MINIMUM AND 0.600 INCHES MAXIMUM IN |
| SPECIAL FEATURES | T.O. 2J-TF39-4;HONEYCOMBED |
| END ITEM IDENTIFICATION | ACFT ENG. TF-39 |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.