What was found
FORWARD INTERIOR FUSELAGE, AFT SIDE OF FRAME WEB CRACKED AT BS 277, STRINGER 5L. R & R WEB IAW DWG & SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FORWARD INTERIOR FUSELAGE, AFT SIDE OF FRAME WEB CRACKED AT BS 277, STRINGER 5L. R & R WEB IAW DWG & SRM.