What was found
TUL - 2 INCH AREA OF CORROSION ON STA 740 FRAME AT ATTACH POINT TO FUSELAGE BELLY SKIN BL ZERO TO LBL 2. REPLACED T-ANGLE AT 740 28L-28R PER SRM 51-10-01, PAGE 04. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TUL - 2 INCH AREA OF CORROSION ON STA 740 FRAME AT ATTACH POINT TO FUSELAGE BELLY SKIN BL ZERO TO LBL 2. REPLACED T-ANGLE AT 740 28L-28R PER SRM 51-10-01, PAGE 04. (X)