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| Part No. : 800220 | Manufacturer : turbine engine components | Item Name: seal air aircraft gas turbine en |
| NSN: 2840-01-168-1327 (2840011681327) | CAGE Code: 02403 | FSC: 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components |
If you require part number 800220 from Turbine Engine Components which is described as a Seal Air Aircraft Gas Turbine En component ASAP Logistic Solutions is your sourcing solution. On this page, you can request a quote on part number 800220 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 2840011681327 and was produced under the CAGE Code 02403. To learn more about this listing or to simply initiate the purchasing process, complete and submit the RFQ form on this page for part 800220 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 |
|---|---|---|---|---|---|---|
| 2840-01-168-1327 Item PartTypeName: SEAL,AIR,AIRCRAFT GAS TURBINE EN | 2840 | 011681327 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 800220 | 1 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 1.505 INCHES MINIMUM AND 1.519 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | ACFT ENG TF33 |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME SEAL AIR,AIRCRAFT GAS TURBINE ENGINE |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| CZCJ | STAGE NUMBER | 3 |
| FEAT | SPECIAL FEATURES | USED ON TF33-P3,P5,P9,PW103 AND P7A ENGINE SERIES SAME AS P/N 617727,REPLACES P/N 390259,390259M80,AND 513540 |
| MATT | MATERIAL | NICKEL ALLOY OVERALL |
| RDAL | REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-14,FIG 30,IND 17,TF33-4,FIG 32,IND 26 |
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