To receive competitive purchasing options on part number LE162-0066-0001 by Boeing Company The, look no further than NSN Direct. For your reference, this item has the NSN 1680-01-163-6724 and is listed with the description “Strut Assembly Aircraft Seat.” If this matches your needs, we encourage you to fill out the partially-completed quote request form on this page to kick off procurement. By providing comprehensive information about your requirements, such as your desired quantity, pricing, and fulfillment speed, our experts can formulate the most fitting solutions for you. We want to ensure that this process is quick and effortless, so we routinely respond to requests within 15 minutes of receiving and reviewing them.
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In addition to our streamlined quotation service, we also aim to make the process of finding products simple. As such, if you require other Boeing Company The parts produced under the CAGE Code 43999, you can peruse our manufacturer or CAGE Code catalogs, or use our search engine and filters. Furthermore, if you want to locate items similar to part number LE162-0066-0001, you can glean from the first four digits of its NSN 1680-01-163-6724 that it belongs to the FSC 1680 Miscellaneous Aircraft Accessories Components. This being said, do not hesitate to request quotes on part number LE162-0066-0001 and any other NSN parts that we feature to experience unrivaled procurement.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 1680-01-163-6724 Item PartTypeName: STRUT ASSEMBLY,AIRCRAFT SEAT | 1680 | 011636724 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| 7 | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| LE162-0066-0001 | 2 | 2 | 7 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | B-1B AIRCRAFT |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | MADE FROM 4130 STEEL BAR,MIL-S-6758,CONDITION F4,HEAT 125 KSI MIN;TUBE MATERIAL 2024-T3 WW-T-700/3,WALL THICKNESS AND OUTSIDE DIAMETER AS INDICATED;OVERALL LENGTH 12.63;ROD ASSEMBLY TEST TENSION LOAD OF 1500 POUNDS;A COMPRESSION LOAD OF 460 |
| ZZZV | FSC APPLICATION DATA | SEAT,AIRCRAFT |
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