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| Item Name | Hub Compressor Aircraft Gas Turb |
| Federal Supply Group (FSG) | Engines Turbines and Components |
| Federal Supply Class (FSC) | 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| National Item Identification Number (NIIN) | 01-471-7748 (014717748) |
| NCB Code | USA (01) |
| Manufacturer | United Technologies Corporation |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABMZ | DIAMETER | 4.870 INCHES MINIMUM AND 4.890 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | TF33-P-7A ACFT ENGINE |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| MATT | III MATERIAL | NICKEL ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5660 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| RDAL | REFERENCE DATA AND LITERATURE | 2J-TF33-14 FIGURE 19 INDEX 5A |
| ABMZ | DIAMETER | 4.870 INCHES MINIMUM AND 4.890 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | TF33-P-7A ACFT ENGINE |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| MATT | III MATERIAL | NICKEL ALLOY OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5660 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| RDAL | REFERENCE DATA AND LITERATURE | 2J-TF33-14 FIGURE 19 INDEX 5A |
| Relevant Components for NSN - 2840-01-471-7748, 2840014717748 | ||||
| 2825-00-790-8901 (2825007908901) | 2825-01-010-8535 (2825010108535) | 2825-00-371-7811 (2825003717811) | 2805-01-264-5598 (2805012645598) | |
| 2840-01-375-6452 (2840013756452) | 2805-01-130-2594 (2805011302594) | 2835-01-234-6845 (2835012346845) | 2805-01-714-1073 (2805017141073) | |
| 2840-00-837-2120 (2840008372120) | 2840-01-708-1715 (2840017081715) | 2840-01-200-9553 (2840012009553) | 2805-00-710-5355 (2805007105355) | |
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