What was found
DURING C-CHECK INSPECTION, FOUND EXT FUSELAGE BETWEEN BS 440 AND BS 450 AT STRINGER 23R SKIN BULGED. REPAIRED STRINGER 23R FROM BS 440 TO BS 473 DUE TO LEVEL 2 CORROSION IAW SRM 53-10-3 FIG 1. FUSELAGE SKIN FOUND SATISFACTORY. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION, FOUND EXT FUSELAGE BETWEEN BS 440 AND BS 450 AT STRINGER 23R SKIN BULGED. REPAIRED STRINGER 23R FROM BS 440 TO BS 473 DUE TO LEVEL 2 CORROSION IAW SRM 53-10-3 FIG 1. FUSELAGE SKIN FOUND SATISFACTORY. (M)