What was found
FOUND WEAR ON FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FROM BS 2517 THROUGH 2628 LT SIDE. REMOVED DAMAGED AREA AND CHECKED 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.
FOUND WEAR ON FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FROM BS 2517 THROUGH 2628 LT SIDE. REMOVED DAMAGED AREA AND CHECKED REWORKED AREA IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.