What was found
DURING INSPECTION, FOUND CORROSION ON STRINGER 44 LOCATED BETWEEN FRAMES 33-34. REPAIRED STRINGER IAW SRM 53-00-39, PARA 4A, FIG 201, PAGES 201-212 AND DWG D532-10093.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND CORROSION ON STRINGER 44 LOCATED BETWEEN FRAMES 33-34. REPAIRED STRINGER IAW SRM 53-00-39, PARA 4A, FIG 201, PAGES 201-212 AND DWG D532-10093.