AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
| Item Name | Disk And Hub Compressor Aircraft |
| Federal Supply Group (FSG) | Engines Turbines and Components |
| Federal Supply Class (FSC) | 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
| National Item Identification Number (NIIN) | 01-447-2868 (014472868) |
| NCB Code | USA (01) |
| Manufacturer | General Electric Company |
| Part Number | Manufacturer | Item Name | RFQ |
|---|---|---|---|
| 1559M63G04 | general electric company | disk and hub compressor aircraft | RFQ |
| 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 |
| Relevant Components for NSN - 2840-01-447-2868, 2840014472868 | ||||
| 2810-00-215-9725 (2810002159725) | 2810-01-442-8304 (2810014428304) | 2840-00-054-1352 (2840000541352) | 2825-00-147-5817 (2825001475817) | |
| 2840-00-936-0717 (2840009360717) | 2805-01-624-8047 (2805016248047) | 2840-01-680-0148 (2840016800148) | 2815-00-963-3563 (2815009633563) | |
| 2840-00-432-3057 (2840004323057) | 2815-01-609-8784 (2815016098784) | 2835-01-033-7276 (2835010337276) | 2840-01-686-5641 (2840016865641) | |
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