What was found
TEMP REPAIR ON VERTICAL STAB RT SIDE AT FUSELAGE SKIN. REPAIRED AREA PER M/M 55-30-0 FIG 801.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TEMP REPAIR ON VERTICAL STAB RT SIDE AT FUSELAGE SKIN. REPAIRED AREA PER M/M 55-30-0 FIG 801.