What was found
CRACK ON FRAME WEB BS 1485 BELOW VENTRAL ACTUATOR FITTING. FRAME WEB WAS REPAIRED IAW SRM 51-01, PAR 21, 53-03 FIG 43, 51-30-2 AND 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON FRAME WEB BS 1485 BELOW VENTRAL ACTUATOR FITTING. FRAME WEB WAS REPAIRED IAW SRM 51-01, PAR 21, 53-03 FIG 43, 51-30-2 AND 51-30-5.