What was found
INSPECTION FOUND A BURN SPOT ON FUSELAGE SKIN 2.25 INCHES AFT OF STA 727 AND 2.25 INCHES ABOVE S23L. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201, REPAIR 31, PAGE 231.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A BURN SPOT ON FUSELAGE SKIN 2.25 INCHES AFT OF STA 727 AND 2.25 INCHES ABOVE S23L. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201, REPAIR 31, PAGE 231.