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MS21921-4D

Military Standard Tube Coupling Nut

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Description

Nut

Specifications

Criticality Code Justification Feat
Diameter C Tolerance -000 in
Dimension A 0.72 in
Dimension A Tolerance +0.010 in
Dimension B 0.18 in
Dimension B Tolerance +0.010 in
Dimension C 0.552 in
Dimension H 0.562 in
End Application E-3a aircraft warning and control system (awacs) starlifter c-141 aircraft f-111. tomcat f-14a delta dart f-106 chinook ch-47 helicopter iroquis uh-1 aircraft application
Industry Standards/Certification MIL-S-8879
Material Aluminum
Material Specification T62 or t851 federal specification single material response t6 t6 federal specification single material response or qq-a-225/6 qq-a-367
NIIN 00-555-8203
NSN 4730-00-555-8203
Nut Height Between 0.710 inches and 0.730 inches
Nut Style Tube coupling
Seat Angle 45.00 degrees
Special Features Grumman aerospace corporation a10 aircraft; weapon system essential
Specification Data 96906-ms21921 government standard
Surface Treatment Anodize
Surface Treatment Specification Class 1 military specification single treatment response type 2 mil-a-8625
Thread Class 3b
Thread Direction Right-hand
Thread Qty 20
Thread Qty Per Inch (tpi) 20
Thread Series Unjf (fine thread with external controlled root radius)
Thread Size 0.438
Thread T (MIL-S-8879) 0.4375-20
Tube Outside Diameter 1/4 in
Weight 0.03 lb
Width Across Flats 0.562

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