What was found
TAIL INTERIOR CANTED FRAME WEB AT BS 1485 HAS 1/2 INCH CRACK. INSTALLED REPAIR IAW SRM 51-70-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TAIL INTERIOR CANTED FRAME WEB AT BS 1485 HAS 1/2 INCH CRACK. INSTALLED REPAIR IAW SRM 51-70-5.