What was found
DURING SCHEDULED S/B 88/704A INSPECTION, FOUND FWD CABIN DOOR, FWD FUS FRAME CRACKED AT DOOR STOP FITTING, FS 333 AT STR 58. REPAIRED PER SRM 53-2-3, FIG 4 SHEET 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED S/B 88/704A INSPECTION, FOUND FWD CABIN DOOR, FWD FUS FRAME CRACKED AT DOOR STOP FITTING, FS 333 AT STR 58. REPAIRED PER SRM 53-2-3, FIG 4 SHEET 1.