What was found
DURING C-7 CHECK, INSPECTION FOUND RIGHT EXTERIOR FUSELAGE ANGLE AT BS 540, STRINGER 7R, CRACKED AT POINT FAIRING SUPPORTS ATTACH. MAINTENANCE REPAIRED DAMGED ANGLE PE SRM 51-40-3. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-7 CHECK, INSPECTION FOUND RIGHT EXTERIOR FUSELAGE ANGLE AT BS 540, STRINGER 7R, CRACKED AT POINT FAIRING SUPPORTS ATTACH. MAINTENANCE REPAIRED DAMGED ANGLE PE SRM 51-40-3. (M)