What was found
CRACKED SUPPORT Y=37 AND X=10. SUPPORT WAS REMOVED IAW SRM 51-30-2, REPAIRED IAW SRM 53-01, FIG 2 AND INSTALLED IAW SRM 51-30-2 CRACK LENGTH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED SUPPORT Y=37 AND X=10. SUPPORT WAS REMOVED IAW SRM 51-30-2, REPAIRED IAW SRM 53-01, FIG 2 AND INSTALLED IAW SRM 51-30-2 CRACK LENGTH.