What was found
AFTER REMOVAL OF ACCESS PANEL 621AT CRACK WAS FOUND ON SUPPORT BRACKET CRACK ON STIFFENER SS 21.50 WAS REPAIRED PER CRJ 900 SRM 51-71-59-001-001-A01
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER REMOVAL OF ACCESS PANEL 621AT CRACK WAS FOUND ON SUPPORT BRACKET CRACK ON STIFFENER SS 21.50 WAS REPAIRED PER CRJ 900 SRM 51-71-59-001-001-A01