What was found
FUSELAGE SKIN DENTED AT BS 330.5, STRINGER 11P. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW 42-2018-055, REV B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN DENTED AT BS 330.5, STRINGER 11P. SUCCESSFULLY REFORMED TO ORIGINAL CONTOUR IAW 42-2018-055, REV B.