What was found
FOUND FUSELAGE INTERIOR AT BS 351.2 RBL 48, CORROSION DAMAGE TO UPPER END OF ANGLE BETWEEN SKIN AND FRAME, JUST ABOVE WALKWAY WEB PANEL, STRINGER 22 AREA. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND FUSELAGE INTERIOR AT BS 351.2 RBL 48, CORROSION DAMAGE TO UPPER END OF ANGLE BETWEEN SKIN AND FRAME, JUST ABOVE WALKWAY WEB PANEL, STRINGER 22 AREA. (M)