NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-459-1286 Item Description: Disk And Hub Compre | 2840 | 014591286 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1559m63 | 5 | 9 | D |
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 | F118-GE-100 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 HPC COMPRESSOR SPOOL |
CZBJ | ENGINE SECTION LOCATION | COMPRESSOR |
FEAT | SPECIAL FEATURES | PT.O. 2J-F110-4, FIG 67, IND 5; HPCR STG 1-2, SPOOL OIL DRAIN HOLES ARE ENLARGED 1.48 LARGER THAN THE CURRENT ELLIPTICAL HOLES TO ALLOW BETTER DRAINAGE; CAN ONLY BE USED ON THE F118-GE-100 AIRCRAFT JET TURBINE ENGINE |
MATT | III MATERIAL | TITANIUM ALLOY OVERALL |
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