AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
| 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) | 01-458-2759 (014582759) |
| NCB Code | USA (01) |
| Manufacturer | United Technologies Corporation |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 12.726 INCHES NOMINAL |
| ABMZ | DIAMETER | 16.741 INCHES MINIMUM AND 16.743 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | TF-33 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT AND ABHP AND ABMZ AND CZBJ |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | P/N NOT TO BE PROCURED; P/N TAKEN OFF ENGINE AND PUT INTO SUPPLY THEN REWORKED UP TO P/N 753538 (01-160-6504); DEPENDING ON REPAIR IT WILL GET ASSIGNED A DIFFERENT P/N; IF THIS P/N HAS CRACKS IN THE TIE ROD HOLES WILL BE ASSIGNED P/N 784473 |
| MATT | III MATERIAL | STEEL OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS6415 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-34, FIG 6, IND 51 |
| Relevant Components for NSN - 2840-01-458-2759, 2840014582759 | ||||
| 2805-00-164-1620 (2805001641620) | 2815-01-207-9726 (2815012079726) | 2825-00-377-3256 (2825003773256) | 2805-01-195-3494 (2805011953494) | |
| 2840-00-966-8075 (2840009668075) | 2840-01-467-5221 (2840014675221) | 2815-99-534-5610 (2815995345610) | 2840-01-657-1001 (2840016571001) | |
| 2840-00-869-7004 (2840008697004) | 2840-01-414-6654 (2840014146654) | 2840-00-704-1319 (2840007041319) | 2840-00-869-9397 (2840008699397) | |
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