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NAS1352C02-2

Socket Head Cap Screw

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Description

Socket Head Screw

Specifications

Country of Origin USA
Drive Style Hexagon
End Application Advanced medium range air-to-air (amraam)/aim120a c-2a (reprocured); missile oh-58d; aircraft mh-53e; helicopter observation (ahip) rh-53; helicopter hawkeye e-2c; helicopter ch-53a/d/e; aircraft stratofortress b-52; helicopter tomcat f-14; aircraft w/s: aircraft
Fastener Length Between 0.109 inches and 0.141 inches
Hardness Rating 80.0 rockwell b
Head Diameter Between 0.134 inches and 0.140 inches
Head Height Between 0.083 inches and 0.086 inches
Head Style Flat chamfer
Internal Drive Style Hexagon
Material CRES
Material Specification 66 federal standard 1st material response or 66 federal standard 2nd material response or 66 federal standard 3rd material response or 66 federal standard 4th material response or 66 federal standard 5th material response or astm-a493 aisi xm-7 assn standard 6th material response
Min. Tensile Strength (psi) 80000 pounds per square inch
Minimum Yield Strength 30000 pounds per square inch
NIIN 00-216-8523
NSN 5305-00-216-8523
Sold In Per Package
Specification Data 80205-nas1352 professional/industrial association standard
Surface Finish 63.0 microinches threads
Surface Treatment Passivate
Surface Treatment Specification Qq-p-35 federal specification single treatment response
Thread Class 3a
Thread Diameter 0.086
Thread Direction Right-hand
Thread Length Between 0.073 inches and 0.141 inches
Thread Qty 56
Thread Qty Per Inch (tpi) 56
Thread Series Designator UNJC
Thread Size 2
Weight 0.0001 lb
Width Across Flats Between 0.078 inches and 0.079 inches

Other sizes

Parts that share this base number, ordered by size. Always verify the full specification before substituting.

Cross-reference

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Catalog data updated 2026-07-05. Report a data error