Thank you for taking interest in United Technologies Corporation part number 652221, which is listed with the NSN 2915-00-483-9671 and a product description of “Fuel Control Afterburner Turbine Engine.” 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 652221, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Fuel Control Afterburner Turbine Engine part with the NSN 2915-00-483-9671. For example, you can browse other United Technologies Corporation components that were produced under CAGE Code 77445 or listings that belong to FSC 2915 Engine Fuel System Components Aircraft and Missile Prime Movers 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 652221 and other desired offerings on Aerospace Spare.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2915-00-483-9671 Item Description: Fuel Control Afterburner Turbine Engine | 2915 | 004839671 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 652221 | 6 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | FCRES TUBE MATERIAL,SIX PART NO. 652185 TUBES REQUIRED,ROCKWELLC34 MIN,0.372-0.378 IN. TUBE OD,0.025-0.040 IN. TUBE THK AT BENDS,0.030-0.040 IN. TUBE THK AT OTHER THAN BENDS,8.714 IN. TUBE WORKING LG |
| ZZZV | FSC APPLICATION DATA | AIRCRAFT JET ENGINE,TF30 |
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