What was found
A 1.5 INCH CRACK IN SKIN AND HOLE IN STRINGER 22R AT STA 727E, STR 22R. INSTALLED DOUBLER ON SKIN AND STRINGER PER SRM 53-00-01 FIG 229, DET 19 AND 53-00-03 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 1.5 INCH CRACK IN SKIN AND HOLE IN STRINGER 22R AT STA 727E, STR 22R. INSTALLED DOUBLER ON SKIN AND STRINGER PER SRM 53-00-01 FIG 229, DET 19 AND 53-00-03 FIG 201.