Thank you for taking interest in the Honeywell International Inc part number 331487, a Plate Thrust Bearing product that we stock that is presented alongside the NSN 2915-00-571-0616 for ease of identification. If you would like to learn more about this component and secure purchasing options for your consideration, please fill out and submit the Request for Quote (RFQ) form that is offered below. All we ask is that you supply us with enough information to best accommodate any particular requirements or restrictions that you may have, and we will respond with a curated quote within 15 minutes of our receipt and review.
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We strive to ensure that customers only receive precise items of need, opting to arrange our collection by diverse, commonly recognized forms of data. For instance, part number 331487 specifically traces back to Honeywell International Inc through the CAGE Code 06848, a distinct identifier for one of their physical locations. Moreover, with the NSN 2915-00-571-0616, this listing falls within Federal Supply Code (FSC) 2915 Engine Fuel System Components Aircraft and Missile Prime Movers, enabling one to figure out its basic application. Keeping this in mind, do not hesitate to obtain a competitive quote for part number 331487 here on Aero OEM Parts at your earliest convenience.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2915-00-571-0616 Item PartTypeName: PLATE,THRUST BEARING | 2915 | 005710616 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 331487 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | TURBINE ENGINE FUEL CONTROL MODEL NO. AJ-H1 |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | SCRES AMS 5610,IMMUNIZE PER BENDIX ES-091,ROCKWELL C 35-45 HARDNESS,0.840 IN. O/A OD,0.240 IN. THK,PLATE HAS 0.085 MIN 0.095 IN. MAX FLANGE THK,FLANGE END HAS 0.3000 IN. MIN 0.3005 IN. MAX ID,OTHER END COUNTERBORED 0.500 IN. ID |
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