You have reached the Request for Quote (RFQ) page for part number F3635565-1, an item sourced from Carleton Technologies Inc (CAGE Code 04577) that is classified with the item name Latch Lever. Here, you can utilize our online form to quickly secure tailored pricing and procurement options from our staff as the first step of procurement. With responses always being quick, be sure to get started as soon as possible if you would like to learn more about this part number.
Important Details for Part Number F3635565-1
The part number F3635565-1 is associated with Carleton Technologies Inc, identified by the CAGE Code 04577, and is typically referenced under the item name Latch Lever. It is categorized under the NSN 1660-00-795-7773, with the NIIN 007957773, INC 77777, and NCB code 00 (USA). Additionally, this part falls under the Federal Supply Group (FSG) 16 and Federal Supply Class (FSC) 1660 Aircraft Air Conditioning Heating and Pressurizing Equipment. For more information, these classifications provide further context about the component.
With the form provided, be sure to present our staff with key details on your needs, such as your target pricing, required quantity, and expected turnaround time. Once we receive and review your request for part F3635565-1, a member of our staff will contact you in 15 minutes or less to present customized solutions for your comparisons. Once you make a purchase with us, you can expect our staff to work closely with you through each step of fulfillment to ensure that all needs are met with care and efficiency.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
1660-00-795-7773 Item PartTypeName: LATCH,LEVER | 1660 | 007957773 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | U | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
F3635565-1 | 6 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | ALUMINUM ALLOY QQ-A-596 356-T6;ANODIZED MIL-A-8625 TY 1;1.062 IN. O/A LG;1.015 IN. W O/A;TWO 0.062 IN. DIA HOLES IN LINE THRU CLEVIS ARMS;0.136 IN. DIA HOLE THRU CAM END;ONE 0.112-40 UNC 3B THD HOLE IN ARM END;0.253 IN. DIA BY 0.242 IN. DEE |
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AS9120B and ISO 9001:2015 |
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Aviation Suppliers Association Member |
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FAA AC 0056B Accredited |
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AS 6081:2012 Certification |
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ESD S20.20-2014 Certification |
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