What was found
DURING A (C) CHECK, CORROSION WAS NOTED ON FUSELAGE BILDGE INTERIOR SKIN AND N/PS UNDER SUPPORT FRAME AT STA 660-680, LBL13.5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A (C) CHECK, CORROSION WAS NOTED ON FUSELAGE BILDGE INTERIOR SKIN AND N/PS UNDER SUPPORT FRAME AT STA 660-680, LBL13.5.