What was found
DURING NON ROUTINE CHECK, HOLE IN FUSELAGE AT BS 330, STRINGER 25 LT. DAMAGE FOUND DURING WALK AROUND, APPLIED TEMPORARY REPAIR IAW SRM 53-10, FIG 10.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING NON ROUTINE CHECK, HOLE IN FUSELAGE AT BS 330, STRINGER 25 LT. DAMAGE FOUND DURING WALK AROUND, APPLIED TEMPORARY REPAIR IAW SRM 53-10, FIG 10.