What was found
VERTICAL STAB LEADING EDGE, FRONT SPAR CAP DAMAGED. REPAIRED IAW 5530-01044 SECT 02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STAB LEADING EDGE, FRONT SPAR CAP DAMAGED. REPAIRED IAW 5530-01044 SECT 02.