What was found
TUL - FOUND 15-18 INCH HOLE THROUGH FUSELAGE SKIN ABOVE FORWARD STRAKE ON LEFT SIDE OF AC. REPAIRED FUSELAGE DAMAGE PER SRM 53-04 FIG 1213 SHT 1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TUL - FOUND 15-18 INCH HOLE THROUGH FUSELAGE SKIN ABOVE FORWARD STRAKE ON LEFT SIDE OF AC. REPAIRED FUSELAGE DAMAGE PER SRM 53-04 FIG 1213 SHT 1. (M)