Aerospace Engineering Solutions is proud to offer immediate purchasing options on Praxair Surface Technologies Inc part number 565720, a Seal Metallic Aircraft Gas Turbi product we carry that is listed with the NSN 2840-01-022-0859 for ease of identification. If you would like to learn more about this item, be sure to complete the Request for Quote (RFQ) form provided on this page. By including essential details like your target price, desired quantity, and expected fulfillment timeline, you are ensured a fully customized quote from our team.
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For your reference, this product is traceable to Praxair Surface Technologies Inc through the CAGE Code 33870, as well as categorized under FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components based on the first four digits of the NSN 2840-01-022-0859. Using such information, you can easily narrow down exact items of need for an ease of procurement. With our quotation service in mind, be sure to submit a completed form when you are ready to begin. Should you wish to speak with one of our representatives to discuss services, you can also give us a call or email at your convenience. With all that we offer, choose Aerospace Engineering Solutions for part number 565720 and other NSN items of need.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-022-0859 Item PartTypeName: SEAL,METALLIC,AIRCRAFT GAS TURBI | 2840 | 010220859 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 565720 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 1.215 INCHES MINIMUM AND 1.225 INCHES MAXIMUM |
| ABMZ | DIAMETER | 6.873 INCHES MINIMUM AND 6.875 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG TF33 |
| APGF | DESIGN TYPE | AXIAL COMPRESSOR |
| CRTL | CRITICALITY CODE JUSTIFICATION | MATT AND CZBJ AND ABHP AND ABMZ |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME CARBON SEAL,ENGINE |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| FEAT | SPECIAL FEATURES | T.O. 2J-TF33-14,FIG 4,IND 41A; USED ON THE NO. 1 BEARING,SUPPORT COMPRESSOR INLET CONE; MATL IS GRAPHITE CARBON |
| MATT | MATERIAL | GRAPHITE OVERALL |
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