What was found
LEVEL 1 CORROSION LEFT WING FRONT SPAR MID-SECTION ON WEB BY VERTICAL STIFFENER LES 732.56. 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 LEFT WING FRONT SPAR MID-SECTION ON WEB BY VERTICAL STIFFENER LES 732.56. BLENDED CORROSION FOUND WITHIN LIMITS PER BOEING SRM 57-10-01 FIG. 1.