AIRCRAFT ROUGH LANDING CRITERIA ARGUMENTATION BASED ON FLIGHT DATA READOUTS FROM MSRP-A-02

Abstract

Article considers methods of formation and argumentation of rough landing criteria based on the on-board MSRP-A-02 recorder data with an example of IL-76TD with PS-90A-76 gas-turbine engines. The volume of reliable information development on aircraft in-flight parameters and its maximum load factors on landing with different degree of roughness has been defined. The results of load quantity simulation have been analyzed.

Keywords

• aircraft
• loading
• landing impact
• rough landing
• statistical model
• rough landing criteria