Welcome to National Stock Numbers Quotes, your go-to solution for Rotor Compressor Aircraft Gas Tu components by General Electric Company. With over 2 billion ready-to-purchase products in our inventory, customers can easily meet rigid time constraints and inflexible budget parameters. National Stock Numbers Quotes maintains a diverse database of items that suit a myriad of industry verticals, including aerospace, defense, and civil sectors, among others. On this page, you can submit a quote request for part number 1559M63G02-129 with NSN 2840014388399 to receive a customized solution in as little as 15 minutes or less.
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At National Stock Numbers Quotes, we make it a priority to meet our customers’ operational requirements, so we keep catalogs fully stocked with in-demand NSN parts like those with the FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components by General Electric Company. For additional specification regarding your part needs, you can also find a wide range of items by their respective CAGE Code, such as 07482, and many other designations for your ease-of-search. Kick off the procurement process with a competitive quote for NSN 2840-01-438-8399 today and see why customers continuously rely on National Stock Numbers Quotes time and time again. For one-on-one assistance, contact us via phone or email at any time; we are available around the clock!
| 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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