What was found
DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 25R BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 25R FROM BS 720D PLUS 5.00 TO BS 740 IAW SRM 53-10-3 FIG 3. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION, FOUND LEVEL 2 CORROSION ON STRINGER 25R BETWEEN BS 720F AND BS 740. REPAIRED FUSELAGE STRINGER 25R FROM BS 720D PLUS 5.00 TO BS 740 IAW SRM 53-10-3 FIG 3. (M)