What was found
DURING A LTC INSPECTION, A DENT WAS DISCOVERED ON FUSELAGE SKIN AT BS 244, 1 INCH UNDER STRINGER 17L. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 244, 1 INCH BELOW STRINGER 17L IAW SRM 51-40-2 FIG 1. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A LTC INSPECTION, A DENT WAS DISCOVERED ON FUSELAGE SKIN AT BS 244, 1 INCH UNDER STRINGER 17L. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 244, 1 INCH BELOW STRINGER 17L IAW SRM 51-40-2 FIG 1. (M)