What was found
FUSELAGE SKIN BULGING AT FASTENER, AT APPROXIMATELY FS 205, LONGERON 31 LEFT. REMOVED CORROSION. REPLACED FINGER DOUBLER AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-21, 53-2-0, 51-1-8, 51-1-11, AND REA D853-40861MR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN BULGING AT FASTENER, AT APPROXIMATELY FS 205, LONGERON 31 LEFT. REMOVED CORROSION. REPLACED FINGER DOUBLER AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-21, 53-2-0, 51-1-8, 51-1-11, AND REA D853-40861MR.