As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON ANGLE (2EAS) ON BTW WS=0.00 AND WS=29.00 AT LH/RH WING AUXILIARY INTERNAL REAR SPAR. CORROSION ON ANGLE ON BTW WS=0.00 AND WS=29.00 AT RH WING AUXILIARY INTERNAL REAR SPAR WAS REMOVED AND EVALUATED WITHIN OF LIMITS PER SRM 51-21-06-001-001-A01 AND SRM 53-00-00-101-001-A01. ANGLE ON BTW WS=0.00 AND WS=29.00 AT LH WING AUXILIARY INTERNAL REAR SPAR WAS REPLACED PER SRM 51-42-21-001-001-A01