1807M24: BLADE,TURBINE ROTOR,AIRCRAFT GAS.
BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include material: ALUMINUM BLADE, design_type: AXIAL COMPRESSOR, overall_width: 1.347 INCHES MINIMUM AND 1.352 INCHES MAXIMUM IN, overall_length: 5.388 INCHES MINIMUM AND 5.400 INCHES MAXIMUM IN, blade_attachment_method: FIR TREE, end_item_identification: ACFT ENG TF39. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-444-7701, 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 | ALUMINUM BLADE |
| design_type | AXIAL COMPRESSOR |
| stage_number | 2 |
| overall_width | 1.347 INCHES MINIMUM AND 1.352 INCHES MAXIMUM IN |
| overall_length | 5.388 INCHES MINIMUM AND 5.400 INCHES MAXIMUM IN |
| special_features | THIS ITEM IS PART OF THE HT90 MODFOR THE TF39 ENGINE, EXTERNAL COATING PLATINUM ALUMINIDE, ORIGINAL DRAWING NAME BLADE,HIGH PRESSURE TURBINE ROTOR STAGE 2, LEAD |
| blade_attachment_method | FIR TREE |
| end_item_identification | ACFT ENG TF39 |
| engine_section_location | HIGH PRESSURE TURBINE |
| criticality_code_justification | AGAV |
| NSN | 2840-01-444-7701 |
| STAGE NUMBER | 2 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| BLADE ATTACHMENT METHOD | FIR TREE |
| OVERALL LENGTH | 5.388 INCHES MINIMUM AND 5.400 INCHES MAXIMUM IN |
| OVERALL WIDTH | 1.347 INCHES MINIMUM AND 1.352 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| SPECIAL FEATURES | THIS ITEM IS PART OF THE HT90 MODFOR THE TF39 ENGINE, EXTERNAL COATING PLATINUM ALUMINIDE, ORIGINAL DRAWING NAME BLADE,HIGH PRESSURE TURBINE ROTOR STAGE 2, LEAD |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |
| MATERIAL | ALUMINUM BLADE |
No substitute or cross-reference records for this part.