As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN HAS A BURN HOLE AT B STA 462 APPROX 2" ABOVE S-8R MEASURING 0.011" DEEP AND 0.060" IN DIAMETER. UPON FURTHER INSPECTION FOUND DAMAGE TO WITHIN LIMITS FOR ALLOWABLE DAMAGE IAW SRM 53-30-01. BLENDED OUT DAMAGE AND REFINISHED SURFACE IAW SRM 51-10-02.