What was found
WHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT FLAP OUTBOARD HINGE FITTING, INBOARD ATTACH ANGLE CRACKED. REPLACED ATTACH ANGLE IAW DC9 SRM CHAPTERS 51-30-1, 51-30-2, AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
WHILE COMPLYING WITH C-INSPECTION, FOUND THE RIGHT FLAP OUTBOARD HINGE FITTING, INBOARD ATTACH ANGLE CRACKED. REPLACED ATTACH ANGLE IAW DC9 SRM CHAPTERS 51-30-1, 51-30-2, AND 51-30-5.