| Mfg Part Number: 1559M63G02-110 | Alternate P/N: 1559M63G02110 | Manufacturer: General Electric Company |
| NSN : 2840-01-438-8400 | Item Name : rotor compressor ai | CAGE Code : 07482 |
| FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
Thank you for your interest in NSN 2840-01-438-8400 manufactured by General Electric Company. The particular NSN product you are looking for is listed alongside the part number 1559M63G02-110, and is described as Rotor Compressor Ai. As we have this item available, we invite you to request a quote for your comparisons by filling out our RFQ form below. Once you have completed our form, we ask that you provide us with details regarding target prices, quantities, and expected shipping time frame. In this way, we can provide you with a quote that meets your specifications and requirements.
Beyond NSN 2840-01-438-8400 manufactured under CAGE Code 07482, and other various General Electric Company parts, Acquire NSN has a stock inventory of over 2 billion new, used, obsolete, and hard-to-find NSN parts 1559M63G02-110 that work to meet the needs of a variety of industry verticals and applications. Acquire NSN operates under AS9120B and ISO 9001:2015 certification and FAA AC 00-56B accreditation to ensure the quality and authenticity of our offerings. We have developed an interface that simplifies the purchasing process with rapid response times for the industries we serve. Get started on the procurement process today and see why customers steadily rely on Acquire NSN for all their operational needs.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-438-8400 Item Description: Rotor Compressor Ai | 2840 | 014388400 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| I | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1559m63g02-110 | 5 | 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, IT CAN ONLY BE USED ON AN F110 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-100 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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