What was found
AT C-CHECK, R/W LEADING EDGE INTERNAL STRUCTURE UPPER SURFACE RIB AT STA 246 HAS LOWER CHORD ANGLE CORRODED AT APPROX 8 FWD OF WING FRONT SPAR. REMOVED AND REINSTALLED LOWER CHORD ANGLE PER SRM 51-30-2, 23 INCHES LONG. N/R 2118
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AT C-CHECK, R/W LEADING EDGE INTERNAL STRUCTURE UPPER SURFACE RIB AT STA 246 HAS LOWER CHORD ANGLE CORRODED AT APPROX 8 FWD OF WING FRONT SPAR. REMOVED AND REINSTALLED LOWER CHORD ANGLE PER SRM 51-30-2, 23 INCHES LONG. N/R 2118