| Part Number: 4047224 | Manufacturer: United Technologies Corp |
| NSN : 2840-01-033-9081 (2840010339081) | Item Name : hub compressor aircraft gas turb |
| CAGE Code: 77445 | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| NIIN : 01-033-9081 (010339081) | FSG : 28 Engines Turbines and Components |
| Country: USA | NCB Code: 01 |
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-033-9081 Item Description: Hub Compressor Aircraft Gas Turb | 2840 | 010339081 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| I | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 4047224 | 3 | 2 | 3 |
| 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 | FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIG NAME NUT,PLAIN,ROUND |
| 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; SEE TCTO 2J-F100(II)-509 SUPERSEDES PN 4036639; F100 FRACTURE CRITICAL PART. |
| MATT | III MATERIAL | NICKEL ALLOY HUB |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | PWA1022 MFR REF SINGLE MATERIAL RESPONSE HUB |
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