Maintenance Parts Pro is pleased to offer procurement options for General Electric Company part number 1559M63G02-129, a Rotor Compressor Aircraft Gas Tu product we carry that is listed with the NSN 2840-01-438-8399 for seamless identification. As this item is available for purchase today, be sure to fill out and submit the Request for Quote (RFQ) form on this page if you are interested in obtaining pricing information. All that we ask is that you share details like your budget, desired quantity, and expected fulfillment speed so that we can respond with the most fitting solutions for your comparisons.
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Alongside streamlined quotation processes, we aim to support our customers by providing as much relevant listing information and data with product offerings as possible. For example, part number 1559M63G02-129 specifically traces back to General Electric Company through CAGE Code 07482, as well as belongs to the FSC [FSC] as per its NSN of 2840-01-438-8399. Referencing such details, you can locate and procure exact specifications with ease. With our various practices in mind, do not hesitate to request a quote on part number 1559M63G02-129 using our provided form.
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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