What was found
LOWER HALF OF FUSELAGE TEE ANGLE BETWEEN BS 1040 & 1060, AROUND STRINGER 25R HAD CORROSION. INSTALLED A NEW TEE ANGLE BTWN BS 1040 - 1060, STRINGER 25R IAW SRM 51-40-02-0G-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LOWER HALF OF FUSELAGE TEE ANGLE BETWEEN BS 1040 & 1060, AROUND STRINGER 25R HAD CORROSION. INSTALLED A NEW TEE ANGLE BTWN BS 1040 - 1060, STRINGER 25R IAW SRM 51-40-02-0G-0.