What was found
TAIL INTERIOR, CANTED FRAME LT WEB INBD EDGE HAS 3" CRACK AT OVERHEAD HORIZONTAL STIFFENER, CBS 1485. REPAIRED IAW SRM 53-03, FIG 48.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TAIL INTERIOR, CANTED FRAME LT WEB INBD EDGE HAS 3" CRACK AT OVERHEAD HORIZONTAL STIFFENER, CBS 1485. REPAIRED IAW SRM 53-03, FIG 48.