Thank you for your interest in 1559M63G02-110 available NSN part on NSN Sphere. Rotor Compressor Ai is listed with the part number 1559M63G02-110, 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 1559M63G02-110, 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 2840014388400 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 |
---|---|---|---|---|---|---|
2840-01-438-8400 Item Description: Rotor Compressor Ai | 2840 | 014388400 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
I | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
1559m63g02-110 | 5 | 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, IT CAN ONLY BE USED ON AN F110 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-100 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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