Overview
About AeroSIFT
Providing structural substantiation support to Part 21J DOAs.
Finite Element analysis for internal and interface loads calculations and detail stressing.
Static analysis to demonstrate compliance to FAR/CS 23,25,27 and 29 regulations.
Fatigue and Damage Tolerance analysis to demonstrate compliance to FAR/CS 23,25,27 and 29 regulations.
Preparation and approval of reports by Structures Compliance Verification Engineer (CVE) both EASA and CAA.
Finite Element analysis for internal and interface loads calculations and detail stressing.
Static analysis to demonstrate compliance to FAR/CS 23,25,27 and 29 regulations.
Fatigue and Damage Tolerance analysis to demonstrate compliance to FAR/CS 23,25,27 and 29 regulations.
Preparation and approval of reports by Structures Compliance Verification Engineer (CVE) both EASA and CAA.