2840PL0786534: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include material: NICKEL ALLOY OVERALL, overall_width: 0.245 INCHES MINIMUM AND 0.255 INCHES MAXIMUM IN, overall_length: 1.240 INCHES MINIMUM AND 1.260 INCHES MAXIMUM IN, special_features: T.O. 2J-TF39-4; TURBINE NOZZLE, material_thickness: 0.004 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN, end_item_identification: ACFT ENG TF-39.
This part is cataloged in the U.S. Government catalog under NSN 2840-00-111-1018, 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 |
| stage_number | 2 |
| overall_width | 0.245 INCHES MINIMUM AND 0.255 INCHES MAXIMUM IN |
| overall_length | 1.240 INCHES MINIMUM AND 1.260 INCHES MAXIMUM IN |
| special_features | T.O. 2J-TF39-4; TURBINE NOZZLE |
| material_thickness | 0.004 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN |
| end_item_identification | ACFT ENG TF-39 |
| engine_section_location | HIGH PRESSURE TURBINE |
| material_document_and_classification | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 2840-00-111-1018 |
| STAGE NUMBER | 2 |
| MATERIAL DOCUMENT AND CLASSIFICATION | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| OVERALL LENGTH | 1.240 INCHES MINIMUM AND 1.260 INCHES MAXIMUM IN |
| OVERALL WIDTH | 0.245 INCHES MINIMUM AND 0.255 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| MATERIAL THICKNESS | 0.004 INCHES MINIMUM AND 0.007 INCHES MAXIMUM IN |
| SPECIAL FEATURES | T.O. 2J-TF39-4; TURBINE NOZZLE |
| END ITEM IDENTIFICATION | ACFT ENG TF-39 |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.