What was found
DURING CHECK-C MAINT, THE FWD UPPER CORNER OF THE LEFT FORWARD CABIN DOOR OPENING HAD ONE INCH CRACK IN THE INNER SKIN AND TITANIUM DOUBLER. REPAIRED CRACK PER SRM 53-05, FIG 25A AND EMLR 69463.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CHECK-C MAINT, THE FWD UPPER CORNER OF THE LEFT FORWARD CABIN DOOR OPENING HAD ONE INCH CRACK IN THE INNER SKIN AND TITANIUM DOUBLER. REPAIRED CRACK PER SRM 53-05, FIG 25A AND EMLR 69463.