What was found
FWD WEAR ON THE FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FROM BS 2280 THROUGH 2416 RT SIDE. REMOVED DAMAGED AREA AND CHECK REWORKED AREA IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FWD WEAR ON THE FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FROM BS 2280 THROUGH 2416 RT SIDE. REMOVED DAMAGED AREA AND CHECK REWORKED AREA IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.