SAE AS5587A-2008
Clamp, Loop, Plain, Support, Aircraft

Standard No.
SAE AS5587A-2008
Release Date
2008
Published By
Society of Automotive Engineers (SAE)
Status
 2015-04
Replace By
SAE AS5587B-2009
Latest
SAE AS5587B-2015
Scope
Reinstated tolerances to thickness dimensions listed in table2,corrected typographical error for-37"D" dimension,added default angularity tolerance,added marking methods 2D1 or 2E1 as options, specificed type 6 and type 7 for passivation,included requirement to form aluminum in annealed condition,and updated specification references.

SAE AS5587A-2008 history




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