| Distributor | Stock | Pricing | MOQ | PKG | Lead Time | Date Code | On Order Quantity | On Order Delivery | |
|---|---|---|---|---|---|---|---|---|---|
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23 pcs
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23 pcs | On Request | 1 | On Request | On Request | On Request | On Request | On Request |
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| Head Diameter | |
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This NAS1351N4H8 socket head cap screw is manufactured by National Aerospace Standards. It features a nominal thread diameter of 0.250 inches and a thread length between 0.399 and 0.500 inches. The overall fastener length is between 0.470 and 0.500 inches.
The screw has a flat chamfer head style with a diameter between 0.365 and 0.375 inches and a height between 0.244 and 0.250 inches. It includes 6 drilled holes with a diameter between 0.044 and 0.050 inches, arranged in a round internal hexagon configuration. The internal drive style is hexagon.
Constructed from Iron Alloy 660, this fastener meets material specifications AMS5731 or AMS5737. It is treated with a passivate surface finish conforming to QQ-P-35 federal specification. The minimum tensile strength is 160,000 pounds per square inch. The thread class is 3a with a right-hand thread direction and 28 threads per inch.
This part conforms to the 80205-NAS1351 professional/industrial association standard. It is classified under ECCN EAR99 and has an NSN of 5305-01-239-3521.
| Qty | Low | High |
|---|---|---|
| 1+ | $0.25 | $0.25 |
Estimated market price range - modelled values for guidance only, not live distributor offers.
The nominal thread diameter is 0.250 inches.
The fastener length is between 0.470 and 0.500 inches.
The screw is made from Iron Alloy 660.
The minimum tensile strength is 160,000 pounds per square inch.
It conforms to the 80205-NAS1351 professional/industrial association standard.
The RoHS status is RoHS3 Compliant.
The Moisture Sensitivity Level is 1 Unlimited.