NSN Parts Associated with NSN 1650-01-188-8671 (1650011888671) of Link Stop Valve Idler- Submit a Quote

NSN 1650-01-188-8671 is a type of Link Stop Valve Idler component is now available in stock at One Click Purchasing. NSN codes are a unique numeric serial number assigned by the Defense Logistics Agency (DLA) for all items acquired, stocked, and circulated within the federal supply chain. With NSNs, identifying items is made much easier, ensuring simplified purchasing processes where customers can guarantee that they only procure exact items as necessary.

At One Click Purchasing, owned and operated by ASAP Semiconductor LLC, we prioritize the supply of high-quality, authenticated NSN parts with NSN 1650-01-188-8671 at competitive prices. With an extensive supply-chain network, we guarantee the fastest turnaround times in the industry and a 95% on-time delivery track record. If you would like to obtain a rapid quote for parts with the NSN 1650-01-188-8671, please complete the instant RFQ form below, and a dedicated representative will contact you shortly.

Information of NSN 1650-01-188-8671 (1650011888671)

Alternate NSN : 1650-01-188-8671
Manufacturers : maney aircraft inc , kit pack company inc , boeing company the
CAGE Code : 10000 , 30842 , 43999
Item Name : Link Stop Valve Idler
NIIN : 011888671
FSG Name : 16 Aircraft Components and Accessories
FSC Name : 1650 Aircraft Hydraulic Vacuum and De-icing System Components
NCB Code : USA (01)

Part Number's List for NSN 1650-01-188-8671, 1650011888671

Part No Manufacturer Item Name QTY RFQ
L5873087-001 maney aircraft inc link stop valve idler Avl
RFQ
L5873087-001 kit pack company inc link stop valve idler Avl
RFQ
L5873087 001 boeing company the link stop valve idler Avl
RFQ

Product Details of NSN 1650011888671

MRCCriteriaCharacteristic
AGAVEND ITEM IDENTIFICATIONAIRCRAFT B-1B
TEXTGENERAL CHARACTERISTICS ITEM DESCRIPTIONSTEEL 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
ZZZVFSC APPLICATION DATAAIRCRAFT HYDRAULIC SYSTEM

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