Mfg Part Number: 1559M63G02-129 | Alternate P/N: 1559M63G02129 |
Manufacturer: General Electric Company | NSN : 2840-01-438-8399 |
NIIN : 014388399 | Item Name : rotor compressor ai |
CAGE Code : 07482 | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
Thank you for your interest in our available 1559M63G02-129 NSN part. This part number 1559M63G02-129 is a Rotor Compressor Ai listed under the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, and it is manufactured by General Electric Company. At Internet of Components, all of our stock and inventory are available for purchase today, ready to ship with short lead times and competitive pricing. Whether you are in need of parts that are new, used, or obsolete, our team of industry experts is readily available 24/7x365 to fulfill all of your operational
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Internet of Components is a premier supplier of 1559M63G02-129 NSN component, and we carry recently requested NSN components such as 2840014388399. We strive to only provide our customers with quality parts, which is why we choose to source our inventory from thousands of global manufacturers such as General Electric Company. If you are interested in this particular item, we invite you to begin the purchasing process for 1559M63G02-129 today by filling out and submitting an Instant RFQ. Once received, a member of our staff will review and reach out to you in 15 minutes or less to provide a personalized quote that caters towards your individual needs. Get started on the purchasing process today and see how we are revolutionizing the purchasing process.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-438-8399 Item Description: Rotor Compressor Ai | 2840 | 014388399 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1559M63G02-129 | 3 | 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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