What was found
FUSELAGE SKIN CORRODED AT FUSELAGE FRAME STATION 22 BETWEEN STRINGERS 21.5R TO 21.5L. (DISCOVERED DURING C-CHECK INSPECTION)NEW SKIN INSTALLED IAW SRM 51-10-02 PG. 3 SECT 3A AND RII CARD 53-800-1000.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CORRODED AT FUSELAGE FRAME STATION 22 BETWEEN STRINGERS 21.5R TO 21.5L. (DISCOVERED DURING C-CHECK INSPECTION)NEW SKIN INSTALLED IAW SRM 51-10-02 PG. 3 SECT 3A AND RII CARD 53-800-1000.