What was found
DORSAL FIN, RT SIDE SUPPORT SPLICE ANGLE IS CORRODED. R & R SPLICE ANGLE PN A5398192920100 IAW SRM 51-74-10, AND 51-40-21, FIG 9, PARA 7, PG 24.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DORSAL FIN, RT SIDE SUPPORT SPLICE ANGLE IS CORRODED. R & R SPLICE ANGLE PN A5398192920100 IAW SRM 51-74-10, AND 51-40-21, FIG 9, PARA 7, PG 24.