Thank you for choosing to partner with National Stock Number Shop for the Rotor Compressor Aircraft Gas Tu NSN parts you require. On this page, you can submit a quote request for General Electric Company part number 1559M63G02-129, a component that can also be found by inputting NSN 2840014388399 in our search engine. Apart from this item, we also have an array of other in-demand part numbers, all of which can be traced back to a conglomerate of well-known manufacturers that we trust. Explore our expansive part catalogs by scrolling over to our menu and locate products according to manufacturer, NIIN, NSN, and more.
National Stock Number Shop works with numerous government and defense agencies, so we use CAGE Codes like 07482 to uniquely identify items in a standardized manner. Additionally, we utilize Federal Supply Classes (FSCs) to organize our stock, ensuring customers can find General Electric Company parts under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components with ease. With this in mind, we encourage you to complete the RFQ form below for NSN 2840014388399 or any others, and see how we can provide you with a customized sourcing solution. For one-on-one assistance, contact us via phone or email at any time; we are available around the clock for customer inquiries!
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-438-8399 Item PartTypeName: ROTOR,COMPRESSOR,AIRCRAFT GAS TU | 2840 | 014388399 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1559M63G02-129 | 1 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABMZ | Diameter | 17.300 INCHES NOMINAL |
CZCJ | Stage Number | 1 |
FEAT | Special Features | T.O. 2J-F110-14, FIG 67, IND 5 UNDER P/N 1559M63G02; INCLUDES STAGE 2; ALSO CONSISTS NO. 1 DISK AND NO. 2 DISK AND FORWARD SHAFT THAT MAKES A 1 PIECE CONSTRUCTION THAT HOLDS BOTH STGS; WEIGHS 40.3 LBS; BASIC P/N CAN BE USED ON ALL ENGINE TYPES, BUT ONCE USED ON THE F110-GE-129, IT CAN ONLY BE USED ON A F110-GE-129 ENGINE; REIDENTIFICATION WILL CONSIST OF ADDING THE ENGINE TYPE AS A DASH NUMBER FOLLOWING THE P/N |
CXCY | Part Name Assigned By Controlling Agency | ORIGINAL NAME SPOOL,COMPRESSOR ROTOR |
MATT | Material | TITANIUM ALLOY OVERALL |
AGAV | End Item Identification | F110-GE-129 AIRCRAFT GAS TURBINE ENGINE |
CZBJ | Engine Section Location | HIGH PRESSURE COMPRESSOR |
ABHP | Overall Length | 6.143 INCHES MINIMUM AND 6.163 INCHES MAXIMUM |
APGF | Design Type | AXIAL COMPRESSOR |
MRC | Decoded Requirement | Clear Text Reply |
MDCL | Material Document And Classification | TI-17 MFR REF SINGLE MATERIAL RESPONSE OVERALL |
CRTL | Criticality Code Justification | FEAT AND ABHP AND ABMZ AND CZBJ |
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