What was found
THERE IS EVIDENCE OF CORROSION ON S42L BETWEEN FRAMES 56 & 57, REMOVED CORROSION IAW SRM CH 51-74-00, REMAINING MATERIAL IS .095, REPAIR STRINGER 43L IAW SRM 53-00-13 FIG 201, SRI 53-00-13-2-001-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THERE IS EVIDENCE OF CORROSION ON S42L BETWEEN FRAMES 56 & 57, REMOVED CORROSION IAW SRM CH 51-74-00, REMAINING MATERIAL IS .095, REPAIR STRINGER 43L IAW SRM 53-00-13 FIG 201, SRI 53-00-13-2-001-00.