4084233: NOZZLE ASSEMBLY,TURBINE,AIRCRAFT.
NOZZLE ASSEMBLY,TURBINE,AIRCRAFT. Key specifications include material: CHROMIUM ALLOY OVERALL, design_type: AXIAL COMPRESSOR, overall_length: 4.615 INCHES MINIMUM AND 4.639 INCHES MAXIMUM IN, special_features: REF CLASS NO. 26, 4.639-4.664 FLOW AREA, SET UP NO.
76, blade_attachment_method: SLOT, end_item_identification: ACFT ENG F100PW100. This part is cataloged in the U.S. Government catalog under NSN 2840-01-445-6765, 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 | CHROMIUM ALLOY OVERALL |
| design_type | AXIAL COMPRESSOR |
| stage_number | 3 |
| overall_length | 4.615 INCHES MINIMUM AND 4.639 INCHES MAXIMUM IN |
| special_features | REF CLASS NO. 26, 4.639-4.664 FLOW AREA, SET UP NO. 76 |
| blade_attachment_method | SLOT |
| end_item_identification | ACFT ENG F100PW100 |
| engine_section_location | LOW PRESSURE COMPRESSOR |
| criticality_code_justification | AGAV |
| part_name_assigned_by_controlling_agency | VANETURBINE STATOR,3 STAGE,ASSY OF |
| NSN | 2840-01-445-6765 |
| STAGE NUMBER | 3 |
| DESIGN TYPE | AXIAL COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 4.615 INCHES MINIMUM AND 4.639 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | LOW PRESSURE COMPRESSOR |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | VANETURBINE STATOR,3 STAGE,ASSY OF |
| END ITEM IDENTIFICATION | ACFT ENG F100PW100 |
| MATERIAL | CHROMIUM ALLOY OVERALL |
No substitute or cross-reference records for this part.