What was found
DURING OP 15 MAINT CHECK, FOUND ON FUSELAGE, 7 RIVET HEADS STRESSED AND CRACKED AT STA 256, 10 TO 14 INCHES BELOW CUSP LINE ON LT SIDE. REMOVED CORROSION PER SPM 6-80-01. SEALED AND REPLACED FASTENERS PER DRAWING 5911410.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OP 15 MAINT CHECK, FOUND ON FUSELAGE, 7 RIVET HEADS STRESSED AND CRACKED AT STA 256, 10 TO 14 INCHES BELOW CUSP LINE ON LT SIDE. REMOVED CORROSION PER SPM 6-80-01. SEALED AND REPLACED FASTENERS PER DRAWING 5911410.