9395M65G01: SEAL,AIR,AIRCRAFT GAS TURBINE EN.
SEAL,AIR,AIRCRAFT GAS TURBINE EN. Key specifications include material: STEEL OVERALL, special_features: T.O. 2J-TF39-4; OUTER RADIUS IS 15.237 IN.
FORMED BY ONE PIECE W/45 DEGANGLE; 6 HOLES 0.261-0.267 IN. DIA IN, end_item_identification: ACFT ENG TF39, engine_section_location: LOW PRESSURE TURBINE, criticality_code_justification: AGAV, material_document_and_classification: B50TF25CL-A ASSN STD 5TH MATERIAL RESPONSE OVERALL. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-198-9107, 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 | STEEL OVERALL |
| stage_number | 5 |
| special_features | T.O. 2J-TF39-4; OUTER RADIUS IS 15.237 IN. FORMED BY ONE PIECE W/45 DEGANGLE; 6 HOLES 0.261-0.267 IN. DIA IN |
| end_item_identification | ACFT ENG TF39 |
| engine_section_location | LOW PRESSURE TURBINE |
| criticality_code_justification | AGAV |
| material_document_and_classification | B50TF25CL-A ASSN STD 5TH MATERIAL RESPONSE OVERALL |
| NSN | 2840-01-198-9107 |
| STAGE NUMBER | 5 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| MATERIAL DOCUMENT AND CLASSIFICATION | B50TF25CL-A ASSN STD 5TH MATERIAL RESPONSE OVERALL |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| SPECIAL FEATURES | T.O. 2J-TF39-4; OUTER RADIUS IS 15.237 IN. FORMED BY ONE PIECE W/45 DEGANGLE; 6 HOLES 0.261-0.267 IN. DIA IN |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |
| MATERIAL | STEEL OVERALL |