What was found
DURING SCHEDULED NR 2 CHECK, FOUND FUSELAGE SKIN CORRODED AT FS 490 TO 502 AND STRINGER 39 TO 40. REMOVED AND REPLACED DOUBLER AND SKIN PANEL FS 464-530 AND STRINGER 36 TO 42 PER SRM 53-2-1, FIG 2. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED NR 2 CHECK, FOUND FUSELAGE SKIN CORRODED AT FS 490 TO 502 AND STRINGER 39 TO 40. REMOVED AND REPLACED DOUBLER AND SKIN PANEL FS 464-530 AND STRINGER 36 TO 42 PER SRM 53-2-1, FIG 2. (M)