What was found
LEFT WING REAR SPAR HAS CORROSION. BLEND LIMIT TOLERENCES HAVE BEEN EXCEEDED IAW EA F-2822-7-5009, PT3, STEP B1 ACCOMPLISHED EA F-5710-156998 STEPS 1 THRU 5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING REAR SPAR HAS CORROSION. BLEND LIMIT TOLERENCES HAVE BEEN EXCEEDED IAW EA F-2822-7-5009, PT3, STEP B1 ACCOMPLISHED EA F-5710-156998 STEPS 1 THRU 5.