What was found
TAIL INTERIOR CANTED FRAME AFT WEB HAS A CRACK, BS 1520, 18 INCHES INBD OF L10 END FITTING. FABRICATED DOUBLER AND INSTALLED IAW SRM 51-11-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TAIL INTERIOR CANTED FRAME AFT WEB HAS A CRACK, BS 1520, 18 INCHES INBD OF L10 END FITTING. FABRICATED DOUBLER AND INSTALLED IAW SRM 51-11-01.