What was found
DURING OP 16 MAINT CHECK, THE LT FWD ENTRY DOOR INTERIOR ANGLE WAS CRACKED IN RADIUS, SECOND FROM TOP PRESSURE STOP FITTING. CONFIRMED BY NDT. STOP DRILLED CRACK AND REPAIRED PER SRM 52-05, FIG 31.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OP 16 MAINT CHECK, THE LT FWD ENTRY DOOR INTERIOR ANGLE WAS CRACKED IN RADIUS, SECOND FROM TOP PRESSURE STOP FITTING. CONFIRMED BY NDT. STOP DRILLED CRACK AND REPAIRED PER SRM 52-05, FIG 31.