You have reached the quote request page for part number 9502M33P01 of Electro Methods Inc, we have in stock that is listed alongside the description Seal Air Aircraft Gas Turbine En. If you would like to learn more about this NSN part and your purchasing options, please fill out and submit the Request the Quote (RFQ) page presented on this page. By offering us important details like your target price and expected fulfillment time frame, our team can best offer you a tailored solution for your consideration. As we have staff available at all times, responses to any submission will be offered within 15 minutes of our review.
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To make exploring our expansive inventory simple, we have chosen to list all offerings alongside as much information as we can for an ease of identification. For example, part number 9502M33P01 is specifically produced under CAGE Code 33617, denoting the specific Electro Methods Inc facility it traces back to. Furthermore, with the NSN 2840-01-146-5653, this item also belongs to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components, further ensuring that you only purchase your exact needs. If you have any questions or concerns regarding our offerings or service, be sure to call or email us at your convenience. Otherwise, we look forward to serving you as your strategic sourcing partner for part number 9502M33P01 and more.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2840-01-146-5653 Item PartTypeName: SEAL,AIR,AIRCRAFT GAS TURBINE EN | 2840 | 011465653 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 9502M33P01 | 6 | 1 | C | 9 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABHP | OVERALL LENGTH | 0.900 INCHES MINIMUM AND 0.910 INCHES MAXIMUM |
| ABMZ | DIAMETER | 7.545 INCHES MINIMUM AND 7.555 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | F110-GE-110 AIRCRAFT ENGINE |
| CQFM | HARDNESS RATING | 28.0 ROCKWELL C MINIMUM OVERALL AND 37.0 ROCKWELL C MAXIMUM OVERALL |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| CZBJ | ENGINE SECTION LOCATION | TURBINE |
| FEAT | SPECIAL FEATURES | T.O. 2J-F110-14; FAN FRAM ASSY; NO. 3 BEARING; 2ND END DIA. 7.400-7.401 |
| MATT | MATERIAL | STEEL COMP 630 OVERALL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5643 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| SFTT | SURFACE TREATMENT | NICKEL OVERALL |
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