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| Part No. : 701979 | Manufacturer : united technologies corporation | Item Name: case fan aircraft gas turbine en |
| NSN: 2840-00-117-4893 (2840001174893) | CAGE Code: 77445 | FSC: 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
If you require part number 701979 from United Technologies Corporation which is described as a Case Fan Aircraft Gas Turbine En component ASAP Logistic Solutions is your sourcing solution. On this page, you can request a quote on part number 701979 which is listed under the Federal Supply Class 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components. To ensure that you only procure the exact item you need to be sure to note that this particular product is listed with the NSN 2840001174893 and was produced under the CAGE Code 77445. To learn more about this listing or to simply initiate the purchasing process, complete and submit the RFQ form on this page for part 701979 today Within 15 minutes of receiving and reviewing a completed request based on the information you provide a member of our staff will contact you to provide a tailored solution to your comparison needs.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-00-117-4893 Item PartTypeName: CASE,FAN,AIRCRAFT GAS TURBINE EN | 2840 | 001174893 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 618962 | 1 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | TF33-PW-3/5/9/103 AIRCRAFT GAS TURBINE ENGINE |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT AND CZBJ |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME CASE AND VANE ASSEMBLY,COMPRESSOR,STATOR |
| CZBJ | ENGINE SECTION LOCATION | FAN |
| FEAT | SPECIAL FEATURES | USED ON THE FRONT CASE COMPRESSOR ROTOR,FAN SUPERSEDES P/N 433477,506262,618962 SUPERSEDED BY P/N 672345 |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4,FIG 4,IND 3,2J-TF33-34,FIG 4,IND 1 |
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