Thank you for taking interest in Aeronautical Standards Group part number AN520PB0-3, which is listed with the NSN 5305-00-815-8358 and a product description of “Screw Machine.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
5305-00-815-8358 Item PartTypeName: SCREW,MACHINE | 5305 | 008158358 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | |||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
AN520PB0-3 | 2 | 2 | 2 |
MRC | Criteria | Characteristic |
---|---|---|
AAJD | THREAD CLASS | 2A |
AASB | FASTENER LENGTH | 0.156 INCHES MINIMUM AND 0.188 INCHES MAXIMUM |
AHYM | NOMINAL THREAD DIAMETER | 0.060 INCHES |
CQBC | MINIMUM TENSILE STRENGTH | 55000 POUNDS PER SQUARE INCH |
CYAU | SCREW MATERIAL | COPPER ALLOY |
CYBA | SCREW SURFACE TREATMENT | CADMIUM |
THSD | THREAD SERIES DESIGNATOR | UNF |
AAJF | THREAD DIRECTION | RIGHT-HAND |
AASA | THREAD LENGTH | 0.188 INCHES MAXIMUM |
AASK | HEAD STYLE | ROUND |
AASL | HEAD DIAMETER | 0.099 INCHES MINIMUM AND 0.113 INCHES MAXIMUM |
AASU | HEAD HEIGHT | 0.053 INCHES MAXIMUM |
ABQZ | INTERNAL DRIVE STYLE | CROSS RECESS TYPE 1 |
CMLP | THREAD QUANTITY PER INCH | 80 |
CYAW | SCREW MATERIAL DOCUMENT AND CLASSIFICATION | QQ-B-613 FED SPEC SINGLE MATERIAL RESPONSE OR QQ-B-626 FED SPEC SINGLE MATERIAL RESPONSE OR QQ-W-321 FED SPEC SINGLE MATERIAL RESPONSE |
CYBE | SCREW SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-416,TY 2,CL 3 FED SPEC SINGLE TREATMENT RESPONSE |
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