What was found
TAIL INTERIOR CRACKED BS 1485 CANTED FRAME WEB. CONFIRMED WITH HFEC. TREATED, PRIMED AND INSTALLED REPAIR IAW SRM 53-03D, FIG 48.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TAIL INTERIOR CRACKED BS 1485 CANTED FRAME WEB. CONFIRMED WITH HFEC. TREATED, PRIMED AND INSTALLED REPAIR IAW SRM 53-03D, FIG 48.