What was found
AT C CHECK, LT WING COVE PANEL SUPPORT ROD ATTACH ANGLES CRACKED STA 568 OUTBD NR 2 SPOILER ACT. REPLACED LT WING COVE PANEL SUPPORT BRKT AT STA 568 O/B OF NR 2 SPOILER ACT PER B727 SRM 51-30-2 N/R 1464.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C CHECK, LT WING COVE PANEL SUPPORT ROD ATTACH ANGLES CRACKED STA 568 OUTBD NR 2 SPOILER ACT. REPLACED LT WING COVE PANEL SUPPORT BRKT AT STA 568 O/B OF NR 2 SPOILER ACT PER B727 SRM 51-30-2 N/R 1464.