What was found
INSPECTION FOUND FUSELAGE SKIN GOUGED BELOW FORWARD END OF DORSAL FIN ON R/H SIDE AT STA 876-885, RBL 5, S1-S2R. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN GOUGED BELOW FORWARD END OF DORSAL FIN ON R/H SIDE AT STA 876-885, RBL 5, S1-S2R. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.