NAVY MIL-A-8866 C-1987
AIRPLANE STRENGTH AND RIGIDITY RELIABILITY REQUIREMENTS, REPEATED LOADS, FATIGUE AND DAMAGE TOLERANCE

Standard No.

NAVY MIL-A-8866 C-1987

Release Date

1987

Published By

United States Navy

Scope

This specification defines the strength and rigidity requirements for repeated loading condition applicable to Navy procured airplanes.