As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HMV CORROSION WAS FOUND ON OUTER FUSELAGE SKIN AT RUBSTRIP AREA FROM STA Y=728 BTW LONGS 23RT TO 24RT AND STA Y=757-826 LONG 27RT TO 30 REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA WITHIN LIMITS, IAW SG 09530014 PAR 5A AND SRM 5-04 PAR 57.