What was found
WEAR FOUND ON THE FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FORM BS 2280 THROUGH 2416 LT 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.
WEAR FOUND ON THE FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FORM BS 2280 THROUGH 2416 LT SIDE. REMOVED DAMAGED AREA AND CHECK REWORKED AREA IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.