What was found
DURING INSPECTION AND REPAIR PER AD 94-01-04, FOUND SEVERAL AREAS OF CORROSION IN THE UPPER AND LOWER LAP JOINTS AT STRINGER 4L. REMOVED LIGHT SURFACE CORROSION WITHIN LIMITS PER BOEING SRM 53-30-01 FIG 1 DETAIL 2, LEVEL 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION AND REPAIR PER AD 94-01-04, FOUND SEVERAL AREAS OF CORROSION IN THE UPPER AND LOWER LAP JOINTS AT STRINGER 4L. REMOVED LIGHT SURFACE CORROSION WITHIN LIMITS PER BOEING SRM 53-30-01 FIG 1 DETAIL 2, LEVEL 1.