Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number 1559M63G02-129, a General Electric Company item with the NSN 2840014388399 that is listed alongside the description “Rotor Compressor Aircraft Gas Tu.” If you are interested in part number 1559M63G02-129 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number 1559M63G02-129 is specifically listed with the NSN 2840-01-438-8399, and this code can be used to determine that it falls under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. Additionally, while tracing back to General Electric Company, this NSN part was specifically produced under CAGE Code 07482. With our services and dedication to simple procurement in mind, get started with us today!
| 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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