What was found
ACFT FUSELAGE SKIN IS GOUGED ON LT SIDE AT 409.00 + 64 ABOVE 4TH LT PAX WINDOW BETWEEN STR 13L & 10L. REPAIRED FUSELAGE SKIN BETWEEN FS 409.00 +57 AND FS 409.00 +67 BETWEEN STR4 AND STR BL IAW SRM 53-00-31 REPAIR NR 8.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ACFT FUSELAGE SKIN IS GOUGED ON LT SIDE AT 409.00 + 64 ABOVE 4TH LT PAX WINDOW BETWEEN STR 13L & 10L. REPAIRED FUSELAGE SKIN BETWEEN FS 409.00 +57 AND FS 409.00 +67 BETWEEN STR4 AND STR BL IAW SRM 53-00-31 REPAIR NR 8.