What was found
DURING ACCOMPLISHMENT OF NR:1896678 WAS FOUND CORROSION IN THE INTERNAL FUSELAGE SKIN PANEL LOCATED BTW STA. 1562/1582 AND STGR 24/25 LH SIDE. FOR REFERENCE SEE: SRM 53-60-01-0I-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ACCOMPLISHMENT OF NR:1896678 WAS FOUND CORROSION IN THE INTERNAL FUSELAGE SKIN PANEL LOCATED BTW STA. 1562/1582 AND STGR 24/25 LH SIDE. FOR REFERENCE SEE: SRM 53-60-01-0I-1.