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) | 01-216-0526 (012160526) |
| NCB Code | USA (01) |
| Manufacturer | United Technologies Corporation |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 4.004 INCHES MINIMUM AND 4.014 INCHES MAXIMUM |
| ABMZ | DIAMETER | 7.162 INCHES MINIMUM AND 7.166 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT ENGINE |
| APGF | DESIGN TYPE | COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | APGF AND CZBJ AND CZCJ AND ABHP AND ABMZ |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIG NAME NUT,DRIVE SHAFT |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| CZCJ | STAGE NUMBER | 2 |
| FEAT | 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; REIDENTIFIED FROM P/N 4047224 |
| MATT | MATERIAL | NICKEL ALLOY HUB |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1022 MFR REF SINGLE MATERIAL RESPONSE HUB |
| Relevant Components for NSN - 2840-01-216-0526, 2840012160526 | ||||
| 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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