MIL MIL-A-8870C Notice 1 - Validation

This specification contains the general and detail design|requirements and criteria in the design and construction of airplanes to:|a. Prevent flutter, divergence, and other dynamic and static|aeroelastic instabilities.|b. Control structural vibrations.|c. Prevent fatigue failure of the airframe structure or structural|components induced by vibrations, aeroacoustic and other oscillatory loads for the service life of the airplane.|d. Prescribe structural dynamic analyses, laboratory and ground tests, and structural dynamic flight tests required to demonstrate compliance with design requirements.|e. Apply to airplanes acquired by the Navy for all conditions of flight and surface operations for which the airplanes are required to operate. See more