What was found
DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN STA Y=773 BTW LONGERON 27 TO 28RT. FUSELAGE SKIN WAS BLENDED AND DOUBLER INSTALLED PER REPAIR IAW MD88 SRM 53-04D PARA 57.
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 STA Y=773 BTW LONGERON 27 TO 28RT. FUSELAGE SKIN WAS BLENDED AND DOUBLER INSTALLED PER REPAIR IAW MD88 SRM 53-04D PARA 57.