What was found
CRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF FORWARD SERVICE DOOR (R1). NDT CONFIRMED ADDITIONAL CRACK IN BONDED DOUBLER. REPAIRED AREA IAW SRM 53-00-01 FIG. 201 REPAIR 32 AND EA NR 53-265.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN FUSELAGE SKIN AT AFT LOWER CORNER OF FORWARD SERVICE DOOR (R1). NDT CONFIRMED ADDITIONAL CRACK IN BONDED DOUBLER. REPAIRED AREA IAW SRM 53-00-01 FIG. 201 REPAIR 32 AND EA NR 53-265.