What was found
DURING REGULAR INSPECTION, LT WING OB MID FLAP COVE PANEL DISCOVERED CRACKED ON UNDERSIDE APPROX 22 IN ADJACENT TO SUPPORT ARMS LOCATED AT STA 1100/1122. REPAIRED IAW SRM 51-40-12 AND EO 4757A301.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING REGULAR INSPECTION, LT WING OB MID FLAP COVE PANEL DISCOVERED CRACKED ON UNDERSIDE APPROX 22 IN ADJACENT TO SUPPORT ARMS LOCATED AT STA 1100/1122. REPAIRED IAW SRM 51-40-12 AND EO 4757A301.