What was found
A .375 INCH CRACK MAIN CABIN DOOR OUTER SKIN AT UPPER AFT CORNER BELOW GATE HINGE. INSTALLED DOUBLER PER M/M 52-11-01 FIG 804.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A .375 INCH CRACK MAIN CABIN DOOR OUTER SKIN AT UPPER AFT CORNER BELOW GATE HINGE. INSTALLED DOUBLER PER M/M 52-11-01 FIG 804.