What was found
INSPECTION FOUND A 2.2 INCH CRACK IN THE FUSELAGE SKIN AT THE AFT LOWER CORNER OF THE R-1 DOOR. REPAIRED IAW SRM 53-10-01, REPAIR 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2.2 INCH CRACK IN THE FUSELAGE SKIN AT THE AFT LOWER CORNER OF THE R-1 DOOR. REPAIRED IAW SRM 53-10-01, REPAIR 2.