Thank you for your interest in 1559M63 available NSN part on NSN Sphere. Disk And Hub Compre is listed with the part number 1559M63, and its manufacturer is General Electric Inc. This NSN part is currently available for purchase through our website today, and you may begin the process by filling out the following RFQ form. By providing us with information such as what parts you need, when you need them by, and your target price, our team can present you with a personalized quote that has been specifically tailored to fit your individual needs and requirements. Once you have submitted your request, a dedicated account manager will review and reach out to you in 15 minutes or less to continue the purchasing process.
As a leading online distributor of NSN parts like 1559M63, we provide customers access to an expansive database of new, used, and obsolete items that have been sourced from top global manufacturers such as General Electric Inc. If you are facing an AOG situation or time constraint, we provide same-day delivery and expedited shipping on a number of items. Get started on the purchasing process for NSN 2840014591286 under FSC 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components and experience how NSN Sphere can serve as your strategic sourcing partner for all of your operational needs.
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 |
---|---|---|
ABMZ | Diameter | 17.225 INCHES MINIMUM AND 17.229 INCHES MAXIMUM |
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 | Material | TITANIUM ALLOY OVERALL |
MRC | Decoded Requirement | Clear Text Reply |
CXCY | Part Name Assigned By Controlling Agency | ORIGINAL NAME HPC COMPRESSOR SPOOL |
AGAV | End Item Identification | F118-GE-100 AIRCRAFT GAS TURBINE ENGINE |
CZBJ | Engine Section Location | COMPRESSOR |
ABHP | Overall Length | 6.425 INCHES MINIMUM AND 6.455 INCHES MAXIMUM |
APGF | Design Type | AXIAL COMPRESSOR |
CRTL | Criticality Code Justification | ABHP AND ABMZ AND FEAT |
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