4047224: HUB,COMPRESSOR,AIRCRAFT GAS TURB.
HUB,COMPRESSOR,AIRCRAFT GAS TURB. Key specifications include diameter: 7.162 INCHES MINIMUM AND 7.166 INCHES MAXIMUM IN, material: NICKEL ALLOY HUB, design_type: COMPRESSOR, overall_length: 4.004 INCHES MINIMUM AND 4.014 INCHES MAXIMUM IN, end_item_identification: F100-PW-100 AIRCRAFT ENGINE, engine_section_location: COMPRESSOR. This part is cataloged in the U.S.
Government catalog under NSN 2840-01-033-9081, 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.
| diameter | 7.162 INCHES MINIMUM AND 7.166 INCHES MAXIMUM IN |
| material | NICKEL ALLOY HUB |
| design_type | COMPRESSOR |
| stage_number | 2 |
| overall_length | 4.004 INCHES MINIMUM AND 4.014 INCHES MAXIMUM IN |
| end_item_identification | F100-PW-100 AIRCRAFT ENGINE |
| engine_section_location | COMPRESSOR |
| criticality_code_justification | FEAT |
| material_document_and_classification | PWA1022 MFR REF SINGLE MATERIAL RESPONSE HUB |
| part_name_assigned_by_controlling_agency | ORIG NAME NUT,PLAIN,ROUND |
| NSN | 2840-01-033-9081 |
| STAGE NUMBER | 2 |
| DESIGN TYPE | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| MATERIAL DOCUMENT AND CLASSIFICATION | PWA1022 MFR REF SINGLE MATERIAL RESPONSE HUB |
| DIAMETER | 7.162 INCHES MINIMUM AND 7.166 INCHES MAXIMUM IN |
| OVERALL LENGTH | 4.004 INCHES MINIMUM AND 4.014 INCHES MAXIMUM IN |
| ENGINE SECTION LOCATION | COMPRESSOR |
| SPECIAL FEATURES | INTL INVOLUTE SPLINE DATA: TEETH 140; PRESSURE ANGLE 30 DEG.; T.O. 2J-F100-4, FIGURE 115, INDEX 3; USED ON THE REAR COMPRESSOR DRIVE; SEE TCTO 2J-F100(II)-509 SUPERSEDES PN 4036639; F100 FRACTURE CRITICAL PART. |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIG NAME NUT,PLAIN,ROUND |
| END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT ENGINE |
No substitute or cross-reference records for this part.