What was found
CRACK IN FUSELAGE SKIN AT FS 1153 RIGHT SIDE 12 INCHES ABOVE THE HORIZONTAL STABILIZER. REMOVED DAMAGED AREA AND INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 53-30-03 FIG 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN FUSELAGE SKIN AT FS 1153 RIGHT SIDE 12 INCHES ABOVE THE HORIZONTAL STABILIZER. REMOVED DAMAGED AREA AND INSTALLED A REPAIR DOUBLER AND FILLER IAW SRM 53-30-03 FIG 2.