Description / Abstract:
This alloy is intended for use where high strength is required
and where exfoliation and stresscorrosion resistance superior to
7178-T6 is required in high performance military aircraft.
SAE AMS-QQ-A-250/21 Revision C, February 1, 2014
Aluminum Alloy, 7178-T76, Plate and Sheet Improved Exfoliation Resistant