| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-363-0850 Item Description: Disk And Hub Compre | 2840 | 013630850 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 854131 | 2 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 6.500 INCHES NOMINAL |
| ABMZ | DIAMETER | 15.000 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | TF33-PW-3/5/9/PW-103 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME HUB,COMPRESSOR,AIRCRAFT GAS TURBINE ENGINE |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | USED ON THE ROTOR FRONT COMPRESSOR; SUPERSEDED P/N 576901, 395001 AND 747231 |
| MATT | III MATERIAL | TITANIUM ALLOY OVERALL |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4, FIG 5, 5B, IND 1, FIG 5C, IND 6 |
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