Buy Mil Spares is your sourcing solution for top-quality military and defense parts, aerospace parts, and other similar products that are necessary for operational fulfillment. You have reached the RFQ page for part number L5873087-001, a Link Stop Valve Idler item that is listed with the NSN 1650-01-188-8671 for an ease of identification. Manufactured by Boeing Company The and readily available for procurement today, you are always welcome to request a quote on this NSN part to receive tailored pricing information and fulfillment options from our team. Simply offer us important information like your desired quantity, price, and fulfillment timeframe, and our team will supply you with a tailored quote on part number L5873087-001 in 15 minutes or less.
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To ensure that customers quickly identify and procure exact items, we list everything with as much relevant information as possible. For example, while part number L5873087-001 is manufactured by Boeing Company The, it is specifically done so under CAGE Code 43999, a unique identifier assigned to a specific facility by the DLA that supplies to various government or defense agencies. Furthermore, using the first digits of the NSN 1650-01-188-8671, one can also determine that this part falls under FSC 1650 Aircraft Hydraulic Vacuum and De icing System Components. With this in mind, continue exploring our website today, and see how we can help you secure competitive pricing and rapid lead times on all desired NSN parts.
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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