What was found
LEVEL 1 CORROSION ON LEFT WING FRONT SPAR BETWEEN WS 938.45 AND 964.56 BESIDE VERTICAL STIFFENER. BLENDED CORROSION FOUND WITHIN LIMITS PER BOEING SRM 57-10-01 FIG. 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEVEL 1 CORROSION ON LEFT WING FRONT SPAR BETWEEN WS 938.45 AND 964.56 BESIDE VERTICAL STIFFENER. BLENDED CORROSION FOUND WITHIN LIMITS PER BOEING SRM 57-10-01 FIG. 1.