What was found
THERE IS A 2.5 INCH CRACK IN FUSELAGE AT LOWER AFT RADIUS OF DOOR 1R OPENING. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE INSTALLED. VERIFIED CRACK FREE AFTER DAMAGE REMOVED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
THERE IS A 2.5 INCH CRACK IN FUSELAGE AT LOWER AFT RADIUS OF DOOR 1R OPENING. MAJOR REPAIR ACCOMPLISHED. REPAIR ANGLE INSTALLED. VERIFIED CRACK FREE AFTER DAMAGE REMOVED.