What was found
DURING C CHECK INSPECTION FOUND CHAFE DAMAGE TO STRINGER 19L EXTERNAL REINFORCEMENT TEE WEB BETWEEN FRAME 52 AND 53. CHAFE CAUSED BY WING TO FUSELAGE FAIRING. MAINTENANCE REPAIRED STRINGER 19L (ONE ANGLE REPAIR) I/A/W SRM 53-24-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C CHECK INSPECTION FOUND CHAFE DAMAGE TO STRINGER 19L EXTERNAL REINFORCEMENT TEE WEB BETWEEN FRAME 52 AND 53. CHAFE CAUSED BY WING TO FUSELAGE FAIRING. MAINTENANCE REPAIRED STRINGER 19L (ONE ANGLE REPAIR) I/A/W SRM 53-24-02.