If you are interested in NSN 2840-01-438-8399 with the part number 1559M63G02-129, we have you covered at Part Orbit. This particular item is described as a Rotor Compressor Aircraft Gas Tu, and it was manufactured by General Electric Company. If you would like to purchase this particular part number, or any other NSN part on our website, first begin with a competitive quote which you may receive through the submission of an RFQ form for 1559M63G02-129 part as provided below. With team members readily available for customers 24/7x365, responses to quote requests will be given in as little as 15 minutes or less.
Whether you want NSN 2840-01-438-8399 produced under the CAGE Code 07482 or other General Electric Company parts, we are unmatched in our availability and quality. With our NO CHINA SOURCING pledge, we ensure that all offered NSN parts have come from leading global manufacturers that we trust and have undergone all necessary quality assurance measures. National Stock Numbers, or NSNs, are 13-digit numerical codes that serve to classify all ‘standardized material items of supply’. The NSN system is practiced by all NATO countries, facilitating an ease of trade. As a leading distributor of NSN parts, we invite you to take advantage of our services today and see how we can serve as your strategic sourcing partner.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2840-01-438-8399 Item Description: 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 | 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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