What was found
DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FUSELAGE FRAME AT STA 8080 BETWEEN LONGERONS 30LT TO 28RT. REPAIRED I/A/W YS-11 SRM 53-3-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK INSPECTION, CORROSION WAS FOUND ON A FUSELAGE FRAME AT STA 8080 BETWEEN LONGERONS 30LT TO 28RT. REPAIRED I/A/W YS-11 SRM 53-3-2.