Rotable Parts Exchange serves as a comprehensive source for military products, aerospace equipment, and Link Stop Valve Idler items. You have expressed particular interest in part number L5873087-001, a Boeing Company The component we offer that is presented with the NSN 1650-01-188-8671 for straightforward identification and procurement. By completing and submitting the Request for Quote form provided on this page, you can obtain pricing details on this NSN part for your comparisons. Once our staff members receive and review your submitted information, a dedicated account manager will directly contact you with a response within 15 minutes or less.
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We strive to streamline the purchasing process and simplify it as much as possible, which includes providing detailed listings for all components to help customers pinpoint their exact needs. For instance, part number L5873087-001 is manufactured by Boeing Company The under the CAGE Code 43999. Additionally, by using the initial digits of the NSN 1650-01-188-8671, you can discover that this component is associated with the FSC 1650 Aircraft Hydraulic Vacuum and De icing System Components. If you have any specific questions about our database, you may always give us a call or email, as we would be delighted to assist you however we can. Otherwise, we encourage you to secure a quote for part number L5873087-001 at your earliest convenience.
| 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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