As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PHX - DURING C-CHECK INSPECTION REPORTED A 1.25 INCH CRACK ON LEFT WING TRAILING EDGE INBOARD MIDFLAP INBOARD EDGE FLAP REAR SPAR T-CHORD. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-40-4, FIG 1 51-40-3 AND 51-30-02. (M)