| Mfg Part Number: 1559M63G02-129 | Alternate P/N: 1559M63G02129 | NSN : 2840-01-438-8399 |
| NIIN : 014388399 | CAGE Code : 07482 | Manufacturer: General Electric Co |
| Item Name : Rotor Compressor Ai | FSC : 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
Thank you for your continued interest in the various parts and components currently available on The NSN Mart. Here, our customers will find our NSN RFQ Page for Rotor Compressor Ai parts with the NSN 2840-01-438-8399, among others from the manufacturer General Electric Co. For particular equipment such as part number 1559M63G02-129, the submission of a completed RFQ form will provide customers with a quote on any desired part in just 15 minutes or less. Upon receival, our expert market representatives will use your offered information to construct a quote paramount to your operations with rapid turnaround times and cost savings at our forefront.
As our robust supply chain stretches across the United States, we are able to supply entities facing Aircraft on Ground (AOG) delays, or other unique time constraints, with expedited shipping on select NSN 2840-01-438-8399 items for immediate procurement. Operating as an AS9120B, ISO 9001:2015, and FAA AC 00-56B accredited enterprise, products listed on our database are upheld to rigorous quality assurance testing, inspection, and cross-referencing before shipment. Functioning as the only independent distributor with a NO CHINA SOURCING pledge, you can depend on The NSN Mart for authentic items like those listed alongside the CAGE Code 07482 by General Electric Co.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-438-8399 Item Description: Rotor Compressor Ai | 2840 | 014388399 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| I | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1559m63g02-129 | 3 | 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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