What was found
DURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN PREVIOUS REPAIR TRIPLER AT WING FILLET PANELS RUBSTRIP SETTLEMENT AREA STA Y=757-775 BETWEEN LONGERON 26RT-23RT. REF SRM 53-04D FIG 53 FOR REPAIR.
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 PREVIOUS REPAIR TRIPLER AT WING FILLET PANELS RUBSTRIP SETTLEMENT AREA STA Y=757-775 BETWEEN LONGERON 26RT-23RT. REF SRM 53-04D FIG 53 FOR REPAIR.