SACAA AME Airframes Practice Questions - SACAA Aircraft Maintenance Engineer Airframes General (CAT A B) Theoretical Knowledge Examination Exam

Remove all damaged core material down to the opposite skin while maintaining a 1:1 bevel ratio on the face sheet. Undercut sound core material by 1.5 times the cell diameter around the perimeter of the damage. Remove damaged core back to sound material, leaving clean vertical edges, and undercut the face sheet to create a mechanical key. Remove only the outer face sheet and inject low-density resin into crushed core cells without removing them.