What was found
APPROXIMATE 1.5 INCH CRACK IN FUSELAGE AT LOWER AFT RADIUS OF DOOR 1R. REPAIRED DOOR 1R LOWER AFT CORNER REF SRM 53-10-01 PAGE 207.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
APPROXIMATE 1.5 INCH CRACK IN FUSELAGE AT LOWER AFT RADIUS OF DOOR 1R. REPAIRED DOOR 1R LOWER AFT CORNER REF SRM 53-10-01 PAGE 207.