What was found
RIGHT FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 2R. DAMAGE FOUND BY NDT INSPECTION. FUSELAGE SKIN REPAIRED WITH DOUBLER INSTSALLATION (9" X 10") IAW SRM 53-31-01 ITEM 11 DETAIL B
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FUSELAGE SKIN CRACKED AT FRAME 75, STRINGER 2R. DAMAGE FOUND BY NDT INSPECTION. FUSELAGE SKIN REPAIRED WITH DOUBLER INSTSALLATION (9" X 10") IAW SRM 53-31-01 ITEM 11 DETAIL B