What was found
DURING C-2 CHECK, INSPECTION REPORTED RT AFT WING TO BODY FAIRING SUPPORT ANGLE CRACKED AT STRINGER 20, BS 727-727B. FABRICATED AND INSTALLED REPLACEMENT SUPPORT ANGLE PER SRM 51-10-02, SRM 51-30-00 AND BOEING DRAWING 65-48657.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-2 CHECK, INSPECTION REPORTED RT AFT WING TO BODY FAIRING SUPPORT ANGLE CRACKED AT STRINGER 20, BS 727-727B. FABRICATED AND INSTALLED REPLACEMENT SUPPORT ANGLE PER SRM 51-10-02, SRM 51-30-00 AND BOEING DRAWING 65-48657.