What was found
UPPER FUSELAGE SKIN HAS A GOUGE FROM BS 1139.819 TO 1160, BETWEEN STRINGERS 5L AND 6L. BLENDED THE DAMAGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101. REPAIRED IAW EC/RA 5330-06260.
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 1139.819 TO 1160, BETWEEN STRINGERS 5L AND 6L. BLENDED THE DAMAGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101. REPAIRED IAW EC/RA 5330-06260.