What was found
DURING A LTC INSPECTION, CORROSION AND GOUGES WERE DISCOVERED ON THE FUSELAGE SKIN AT BS 366-370, STRINGER 17-18 LEFT. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 366-370, BETWEEN STRINGER 17-18 LEFT IAW B727 SRM 53-30-3 FIG 3. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A LTC INSPECTION, CORROSION AND GOUGES WERE DISCOVERED ON THE FUSELAGE SKIN AT BS 366-370, STRINGER 17-18 LEFT. ACCOMPLISHED FUSELAGE SKIN REPAIR BS 366-370, BETWEEN STRINGER 17-18 LEFT IAW B727 SRM 53-30-3 FIG 3. (M)