When you require Rotor Compressor Aircraft Gas Tu components such as part number 1559M63G02-129 with the NSN 2840014388399 for your operations, Broadline NSN is your best bet. Whether you are searching for parts from manufacturers like General Electric Company or something else, our team is dedicated to helping you acquire what you need with competitive rates and rapid lead times for your benefit. As such, when you have discovered items of interest, we encourage you to take advantage of our rapid RFQ service by filling out and submitting the form featured throughout our website. On this form, be sure to include relevant details such as your desired part quantity and budget parameters so that our dedicated team members can craft a customized solution that suits your particular operational needs.
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At Broadline NSN, we are dedicated to distributing reliable products such as those with the NSN 2840-01-438-8399 or CAGE code 07482. As an AS9120B, ISO 9001:2015, and FAA AC 00-56B accredited parts distributor, you can rely on the caliber of our offerings which feature more than 2 billion new, used, obsolete, and hard-to-find components that are readily available for your purchase at any time. Countless products are subject to rigorous quality control measures to guarantee their fit, form, and function prior to your purchase for your benefit, and all come from leading manufactures like General Electric Company. Those looking for high-quality parts like listings belonging to the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components can count on our team to get them what they need in rapid time. Call or email us with any questions and we will be more than happy to assist you through any stage of the procurement process.
| 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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