What was found
DURING HMV, A CRACK WAS FOUND ON PAN FWD EDGE OF C3 AT BEAM NR 2 PAN WAS REPAIRED IAW SRM 52-05D FIG 50.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV, A CRACK WAS FOUND ON PAN FWD EDGE OF C3 AT BEAM NR 2 PAN WAS REPAIRED IAW SRM 52-05D FIG 50.