NSN 2840-01-459-1286 · NIIN 014591286 · FSC 2840
NO DASHES 2840014591286
In Stock
DISK AND HUB,COMPRESSOR,AIRCRAFT
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Application: F118-GE-100 AIRCRAFT GAS TURBINE ENGINE
Technical characteristics
9 rows
Straight from the federal item record. Entries the record leaves empty are shown empty — nothing is filled in on its behalf.
| MRC | Requirement | Value |
|---|---|---|
| ABHP | OVERALL LENGTH | INCHES MINIMUM 6.425 AND INCHES MAXIMUM 6.455 |
| ABMZ | DIAMETER | INCHES MINIMUM 17.225 AND INCHES MAXIMUM 17.229 |
| 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 | T.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 | MATERIAL | OVERALL TITANIUM ALLOY |