What was found
FUSELAGE WING BOX INSP OF REAR SPAR & BOTTOM PANEL. INSPECTED RT SIDE AND FOUND HOLE"P" WITH A CRACK SIGNAL. COMPLIED WITH EA6-5710-T0331014, P1. MAJOR REPAIR IAW GMM 6-2-100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE WING BOX INSP OF REAR SPAR & BOTTOM PANEL. INSPECTED RT SIDE AND FOUND HOLE"P" WITH A CRACK SIGNAL. COMPLIED WITH EA6-5710-T0331014, P1. MAJOR REPAIR IAW GMM 6-2-100.