What was found
CRACK ON ATTACH ANGLE INNER SKIN-TO-AFT SIDE PANEL AT PASSENGER DOOR EXTERNAL STRUCTURE. ATTACH ANGLE WAS REPAIRED PER SRM 52-11-04-201-002-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON ATTACH ANGLE INNER SKIN-TO-AFT SIDE PANEL AT PASSENGER DOOR EXTERNAL STRUCTURE. ATTACH ANGLE WAS REPAIRED PER SRM 52-11-04-201-002-A01.