What was found
LEFT WING INBOARD TRAILING EDGE MIDFLAP HAS BLIND FASTENER INSTALLED IN STRESS PANEL. REMOVED AND REPAIRED FASTENER IAW SRM 51-30-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING INBOARD TRAILING EDGE MIDFLAP HAS BLIND FASTENER INSTALLED IN STRESS PANEL. REMOVED AND REPAIRED FASTENER IAW SRM 51-30-02.