What was found
UPPER FUSELAGE SKIN HAS A GOUGE FROM BS 1100 TO 1120, BETWEEN STRINGERS 5L AND 6L. BLENDED THE DAMAGED AREA AND FOUND TO BE OUT OF LIMITS. ACCOMPLISHED A PERMANENT REPAIR IAW EC/RA 53 30-06270.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER FUSELAGE SKIN HAS A GOUGE FROM BS 1100 TO 1120, BETWEEN STRINGERS 5L AND 6L. BLENDED THE DAMAGED AREA AND FOUND TO BE OUT OF LIMITS. ACCOMPLISHED A PERMANENT REPAIR IAW EC/RA 53 30-06270.