9139M55: CASE,TURBINE,AIRCRAFT GAS TURBIN.
CASE,TURBINE,AIRCRAFT GAS TURBIN. Key specifications include material: NICKEL ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 46.500 INCHES MINIMUM AND 47.025 INCHES MAXIMUM IN, end_item_identification: ACFT ENG TF39, engine_section_location: TURBINE, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-444-7699, 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 |
| design_type | AXIAL COMPRESSOR |
| overall_length | 46.500 INCHES MINIMUM AND 47.025 INCHES MAXIMUM IN |
| special_features | MATERIAL IS INCONEL 718 WITH A THERMO BARRIER COATING ON INNER DIA. ORIGINAL DRAWING NAME CASE,TURBINE MID FRAME. THIS ITEM IS PART OF THE HT90 MOD FOR THE TF39 ENG |
| end_item_identification | ACFT ENG TF39 |
| engine_section_location | TURBINE |
| criticality_code_justification | AGAV |
| NSN | 2840-01-444-7699 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| OVERALL LENGTH | 46.500 INCHES MINIMUM AND 47.025 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | TURBINE |
| SPECIAL FEATURES | MATERIAL IS INCONEL 718 WITH A THERMO BARRIER COATING ON INNER DIA. ORIGINAL DRAWING NAME CASE,TURBINE MID FRAME. THIS ITEM IS PART OF THE HT90 MOD FOR THE TF39 ENG |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |
| MATERIAL | NICKEL ALLOY OVERALL |
No substitute or cross-reference records for this part.