What was found
DURING HMV CORROSION WAS FOUND ON EXTERNAL FUSELAGE SKIN FROM STA Y=1060 TO Y=1131 BETWEEN LONGS 18LT AND 30 REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA, WITHIN LIMITS IAW DC9/MD80 SRM 53-04 PAR 57.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HMV CORROSION WAS FOUND ON EXTERNAL FUSELAGE SKIN FROM STA Y=1060 TO Y=1131 BETWEEN LONGS 18LT AND 30 REF MD88 SRM 53-04D PARA 57 FOR REPAIR. BLENDED AREA, WITHIN LIMITS IAW DC9/MD80 SRM 53-04 PAR 57.