What was found
FOUND ON CV 2 CHECK, CORROSION AT NUT CLIP HOLES TOP AND UNDERSIDES OF FLOOR BEAM STA 344 BETWEEN LBL 10 AND 60. REPAIRED PER SRM 53-10-8, FIG 10. INSTALL DOUBLER AND TRIPLER ON CRACKED LEG ONLY PER ENGINEER D.S.W.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND ON CV 2 CHECK, CORROSION AT NUT CLIP HOLES TOP AND UNDERSIDES OF FLOOR BEAM STA 344 BETWEEN LBL 10 AND 60. REPAIRED PER SRM 53-10-8, FIG 10. INSTALL DOUBLER AND TRIPLER ON CRACKED LEG ONLY PER ENGINEER D.S.W.