What was found
DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN INTERNAL DOUBLE AT STA Y=244 BTW LONGERON 16L TO 17L. DOUBLER WAS REPLACED IAW MD88 SRM 53-04D FIG 12B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN INTERNAL DOUBLE AT STA Y=244 BTW LONGERON 16L TO 17L. DOUBLER WAS REPLACED IAW MD88 SRM 53-04D FIG 12B.