305-415-804-0: BLADE,TURBINE ROTOR,AIRCRAFT GAS.
BLADE,TURBINE ROTOR,AIRCRAFT GAS. Key specifications include material: NICKEL ALLOY OVERALL, design_type: COMPRESSOR, overall_length: 4.000 INCHES NOMINAL IN, special_features: MATERIAL INCONEL 100, blade_attachment_method: LOCK, end_item_identification: F108 AIRCRAFT ENGINE. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-371-5782, 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 | COMPRESSOR |
| stage_number | 1 |
| overall_length | 4.000 INCHES NOMINAL IN |
| special_features | MATERIAL INCONEL 100 |
| blade_attachment_method | LOCK |
| end_item_identification | F108 AIRCRAFT ENGINE |
| engine_section_location | LOW PRESSURE TURBINE |
| reference_data_and_literature | T.O. 2J-F108-14,FIG FIN 72-54-00-9 IND 525 |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | BLADE ASSY-LPT RTR STG 1 |
| NSN | 2840-01-371-5782 |
| STAGE NUMBER | 1 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-F108-14,FIG FIN 72-54-00-9 IND 525 |
| BLADE ATTACHMENT METHOD | LOCK |
| OVERALL LENGTH | 4.000 INCHES NOMINAL IN |
| ENGINE SECTION LOCATION | LOW PRESSURE TURBINE |
| SPECIAL FEATURES | MATERIAL INCONEL 100 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BLADE ASSY-LPT RTR STG 1 |
| END ITEM IDENTIFICATION | F108 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.