What was found
AFTER REMOVING CORROSION, A CRACK WAS FOUND ON THE CAP ANGLE ATTACHED TO STAIRWAY FRAME, BETWEEN BS 1401 - 1405, LT SIDE. THE CAP ANGLE WAS REPLACED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFTER REMOVING CORROSION, A CRACK WAS FOUND ON THE CAP ANGLE ATTACHED TO STAIRWAY FRAME, BETWEEN BS 1401 - 1405, LT SIDE. THE CAP ANGLE WAS REPLACED IAW SRM 51-30-2.