| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-447-2868 Item Description: Disk And Hub Compre | 2840 | 014472868 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1559m63g04 | 1 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 6.425 INCHES MINIMUM AND 6.455 INCHES MAXIMUM |
| ABMZ | DIAMETER | 17.225 INCHES MINIMUM AND 17.229 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | F110-GE-129 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | ABHP AND ABMZ AND FEAT |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SPOOL, COMPRESSOR ROTOR |
| CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
| FEAT | SPECIAL FEATURES | T.O 2J-F110-14, FIG 67, IND 5; REPL P/N 1559M63G02; HPCR STG 1-2 SPOOL OIL DRAIN HOLES ARE ENLARGED 1.48 LARGER THAN THE CURRENT ELLIPTICAL HOLES TO ALLOW BETTER DRAINAGE |
| MATT | III MATERIAL | TITANIUM ALLOY OVERALL |
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