What was found
TAIL INTERIOR, CANTED FRAME RT WEB INBD EDGE HAS 1" CRACK AT OVERHEAD HORIZONTAL STIFFENER, CBS 1485. NR FOR ADDITIONAL INFORMATION 001-0392:5300-2551/027, 00161 CMOR; REPAIRED. REF; SRM 53-03, FIG 49.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TAIL INTERIOR, CANTED FRAME RT WEB INBD EDGE HAS 1" CRACK AT OVERHEAD HORIZONTAL STIFFENER, CBS 1485. NR FOR ADDITIONAL INFORMATION 001-0392:5300-2551/027, 00161 CMOR; REPAIRED. REF; SRM 53-03, FIG 49.