What was found
RIGHT WING, FUSELAGE CENTER WING BOX, INSPECTION OF REAR SPAR & BOTTOM PANEL HOLE Y FOUND A CRACK. REPAIRED IAW EA 6-5710-T0319444 P 1. MAJOR REPAIR IAW GMM 6-2-100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT WING, FUSELAGE CENTER WING BOX, INSPECTION OF REAR SPAR & BOTTOM PANEL HOLE Y FOUND A CRACK. REPAIRED IAW EA 6-5710-T0319444 P 1. MAJOR REPAIR IAW GMM 6-2-100.