What was found
LEFT FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 2L. CRACK FOUND DURING NDT INSPECTION. LEFT FUSELAGE SKIN REPAIRED WITH DOUBLER (11" X 9") IAW SRM 53-31-01, ITEM 11, FIG 219, SHEET 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 2L. CRACK FOUND DURING NDT INSPECTION. LEFT FUSELAGE SKIN REPAIRED WITH DOUBLER (11" X 9") IAW SRM 53-31-01, ITEM 11, FIG 219, SHEET 1.