Thank you for taking interest in Aircraft Precision Products Inc part number 9502M33P01, which is listed with the NSN 2840-01-146-5653 and a product description of “Seal Air Aircraft Gas Turbine En.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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Alongside part number 9502M33P01, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Seal Air Aircraft Gas Turbine En part with the NSN 2840-01-146-5653. For example, you can browse other Aircraft Precision Products Inc components that were produced under CAGE Code 97123 or listings that belong to FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number 9502M33P01 and other desired offerings on Aerospace Spare.
| 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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