822666: HUB,COMPRESSOR,AIRCRAFT GAS TURB.
HUB,COMPRESSOR,AIRCRAFT GAS TURB. Key specifications include diameter: 4.870 INCHES MINIMUM AND 4.890 INCHES MAXIMUM IN, material: NICKEL ALLOY OVERALL, end_item_identification: TF33-P-7A ACFT ENGINE A, engine_section_location: COMPRESSOR, reference_data_and_literature: 2J-TF33-14 FIGURE 19 INDEX 5A A, criticality_code_justification: AGAV. This part is cataloged in the U.S.
Government catalog under NSN 5360-00-023-1809, 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 | 4.870 INCHES MINIMUM AND 4.890 INCHES MAXIMUM IN |
| material | NICKEL ALLOY OVERALL |
| end_item_identification | TF33-P-7A ACFT ENGINE A |
| engine_section_location | COMPRESSOR |
| reference_data_and_literature | 2J-TF33-14 FIGURE 19 INDEX 5A A |
| criticality_code_justification | AGAV |
| material_document_and_classification | AMS5660 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| NSN | 5360-00-023-1809 |
| SPRING FREE OUTSIDE DIAMETER | 1.312 INCHES NOMINAL IN |
| END STYLE | SPRING END,SQUARED AND GROUND BOTH ENDS |
| STYLE DESIGNATOR | CYLINDRICAL |
| SPRING FREE LENGTH | 5.125 INCHES NOMINAL IN |
| INSIDE DIAMETER | 0.593 INCHES NOMINAL IN |
| COIL QUANTITY | 20 1/2 |
| COIL HELIX DIRECTION | RIGHT-HAND |
| MATERIAL | STEEL OVERALL |
No substitute or cross-reference records for this part.