Thank you for choosing to partner with National Stock Number Shop for the Link Stop Valve Idler NSN parts you require. On this page, you can submit a quote request for Maney Aircraft Inc part number L5873087-001, a component that can also be found by inputting NSN 1650011888671 in our search engine. Apart from this item, we also have an array of other in-demand part numbers, all of which can be traced back to a conglomerate of well-known manufacturers that we trust. Explore our expansive part catalogs by scrolling over to our menu and locate products according to manufacturer, NIIN, NSN, and more.
National Stock Number Shop works with numerous government and defense agencies, so we use CAGE Codes like 10000 to uniquely identify items in a standardized manner. Additionally, we utilize Federal Supply Classes (FSCs) to organize our stock, ensuring customers can find Maney Aircraft Inc parts under the FSC 1650 Aircraft Hydraulic Vacuum and De icing System Components with ease. With this in mind, we encourage you to complete the RFQ form below for NSN 1650011888671 or any others, and see how we can provide you with a customized sourcing solution. For one-on-one assistance, contact us via phone or email at any time; we are available around the clock for customer inquiries!
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| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1650-01-188-8671 Item PartTypeName: LINK STOP,VALVE IDLER | 1650 | 011888671 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| L5873087-001 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | AIRCRAFT B-1B |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | STEEL CRES PLATE ALLOY,PH13-8MO; 4.293 IN. LG; 1ST END 1.853 IN. LG TO CLEVIS; 0.188 IN. THK; OBLONG HOLE 0.250 IN. FROM END; 0.645 IN. LG; 0.376 IN. W; 2ND END CLEVIS 0.938 IN. W ON OUTSIDE TO OUTSIDE; 0.630 IN. INSIDE CLEVIS ARMS; 2 HOLES |
| ZZZV | FSC APPLICATION DATA | AIRCRAFT HYDRAULIC SYSTEM |
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