What was found
RIGHT FUSELAGE SKIN CRACKED AT FRAME 75, NEAR STRINGER 2R. THE SKIN WAS REPAIRED IAW SRM 53-31-01, PARA II, FIG 219, SHEET 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FUSELAGE SKIN CRACKED AT FRAME 75, NEAR STRINGER 2R. THE SKIN WAS REPAIRED IAW SRM 53-31-01, PARA II, FIG 219, SHEET 1.