What was found
DURING 1A INSPECTION, THE RT FWD DRAG ANGLE, PROFILE, WAS FOUND TO BE CRACKED AT FRAME 76. MAINTENANCE R & R THE AFFECTED DRAG ANGLE, PROFILE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING 1A INSPECTION, THE RT FWD DRAG ANGLE, PROFILE, WAS FOUND TO BE CRACKED AT FRAME 76. MAINTENANCE R & R THE AFFECTED DRAG ANGLE, PROFILE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.