What was found
FOUND CRACK IN FUSELAGE, FORWARD SERVICE DOOR CUTOUT AT UPPER FWD. INSTALLED NEW FRAME IAW SRM 51-10-02, DEFECT SIZE: .25".
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND CRACK IN FUSELAGE, FORWARD SERVICE DOOR CUTOUT AT UPPER FWD. INSTALLED NEW FRAME IAW SRM 51-10-02, DEFECT SIZE: .25".