You are currently exploring our in-stock options for part number S6125-50117 with the NSN 1620007001733. This product is listed with the description “Piston Floating Shock Strut Main” and is manufactured by Yeager Manufacturing Corporation. If you are looking to purchase this part, we encourage you to complete and submit the RFQ form below with as much information as you can provide, such as your desired quantity, budget, shipping time frame, and more. Within 15 minutes of receiving and reviewing your submission, one of our experts will reach out with a quote that is tailored to your needs.
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We supply all relevant information alongside the listings on our website, that way you know you are always getting the exact item you require. For example, part number S6125-50117 is listed alongside the NSN 1620-00-700-1733 and belongs to the FSC 1620 Aircraft Landing Gear Components. Additionally, it is also under the CAGE Code 31788, which is assigned to Yeager Manufacturing Corporation. At Aerospace Procurement, you can trust that each product in our inventory is up to industry standards, as we are committed to various quality assurance practices. For example, we uphold a strict NO CHINA SOURCING pledge to ensure that each part is shipped out alongside its manufacturer trace documentation and qualifying certifications. These practices and more allow us to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. Get in contact with us today to see how we can make the procurement process for part number S6125-50117 seamless.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1620-00-700-1733 Item PartTypeName: PISTON,FLOATING,SHOCK STRUT,MAIN | 1620 | 007001733 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
S6125-50117 | 2 | 2 | 5 |
MRC | Criteria | Characteristic |
---|---|---|
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY,QQ-A-250/12,T73;ANODIZED; 0.25 IN. LG; 3.25 IN W;0.25 IN. RADIAL WALL THICKNESS |
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