We appreciate your interest in the products and services we have to offer at Parts Delivered Today. Part number 1559M63 is one of the many Disk And Hub Compressor Aircraft items tracing back to the manufacturer General Electric Company which is available for purchase at any time on our database. When you have discovered items of interest, be sure to begin the procurement process by requesting a quote for your comparisons through the submission of an RFQ form. Once our team receives your completed form with your various operational needs and restrictions, we can formulate a solution that suits your specifications within 15 minutes or less.
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In addition to products manufactured by General Electric Company like those with the NSN 2840-01-459-1286 and CAGE Code 07482, we also offer countless other components that you can rely on. For example, items belonging to the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, among many more, are available for your immediate purchase on our website. In order to ensure the caliber of our offerings, we source all parts from leading global manufacturers that are on our Approved Vendors List (AVL). Moreover, countless products are subjected to rigorous quality assurance measures to guarantee their fit, form, and function prior to shipment. Through our numerous dedications and practices, we are proud to serve as an AS9120B, ISO 9001:2015, and FAA AC 00-56B accredited distributor. To learn more about our services and products, we encourage you to call or email us at any time; a representative will be more than happy to assist you however we can throughout the procurement process.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-459-1286 Item PartTypeName: DISK AND HUB,COMPRESSOR,AIRCRAFT | 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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