ASTM F3093/F3093M-15 - 1.5.2015
 
1. Scope

1.1 This specification addresses the aeroelasticity requirements of the airplane.

1.2 The values stated in either SI units or inch-pound units are to be regarded separately as standard. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance with the standard.

1.3 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

 
2. Referenced Documents

F3115

Specification for Structural Durability for Small Airplanes

F3065/F3065M-21a

Standard Specification for Aircraft Propeller System Installation (Includes all amendments and changes 5/17/2021).

F3061

Specification for Systems and Equipment in Small Aircraft

Airframe and Equipment Engineering Report No. 45 (as corrected)

Simplified Flutter Prevention Criteria 1955