What was found
DURING INSPECTION, FOUND LT WING UPPER T/E PANEL BY DEFLECTOR RIB CENTER ANGLE CRACKED. MX R & R LT WING DEFLECTION RIB UPPER PANEL CENTER ATTACH ANGLE IAW SRM 51-40-02, PG 1-4 AND IPC 57-50-00-25.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND LT WING UPPER T/E PANEL BY DEFLECTOR RIB CENTER ANGLE CRACKED. MX R & R LT WING DEFLECTION RIB UPPER PANEL CENTER ATTACH ANGLE IAW SRM 51-40-02, PG 1-4 AND IPC 57-50-00-25.