What was found
LT WING O/B FLAP HAS CRACK ON STRUCTURE AT STOP BOLT. LT WING O/B FLAP CRACKED STOP FITTING REMOVED. NEW FITTING HOLES TRANSFERRED AND INSTALLED AS PER SRM 51-33-01 AND 51-31-01 VOL II. MAJOR CLASSIFICATION AS PER GMM 6-2-100.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING O/B FLAP HAS CRACK ON STRUCTURE AT STOP BOLT. LT WING O/B FLAP CRACKED STOP FITTING REMOVED. NEW FITTING HOLES TRANSFERRED AND INSTALLED AS PER SRM 51-33-01 AND 51-31-01 VOL II. MAJOR CLASSIFICATION AS PER GMM 6-2-100.