What was found
FUSELAGE SKIN HAS A 2.5 BY 2.5 INCH HOLE BETWEEN BS 807 AND 827 APPROX 5 INCHES BELOW STR 18 LT. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW ECRA 5331-01645.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN HAS A 2.5 BY 2.5 INCH HOLE BETWEEN BS 807 AND 827 APPROX 5 INCHES BELOW STR 18 LT. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW ECRA 5331-01645.