What was found
OVERSIZE RIVET HOLE IN FUSELAGE SKIN. HOLE IS LOCATED 4 INCHES AFT OF STA 500A AND 1.5 INCH INBOARD OF STR 28L. FABRICATED A COUNTERSUNK FREEZE PLUG AND INSTALLED PER ECRA 5331-01457 PART 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
OVERSIZE RIVET HOLE IN FUSELAGE SKIN. HOLE IS LOCATED 4 INCHES AFT OF STA 500A AND 1.5 INCH INBOARD OF STR 28L. FABRICATED A COUNTERSUNK FREEZE PLUG AND INSTALLED PER ECRA 5331-01457 PART 1.