What was found
RIGHT FUSELAGE SKIN HAS TWO CRACKS AT FRAME 75 AND STRINGER 2R. PERFORMED A PERMANENT REPAIR IAW SRM 53-31-01 FIG 219.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT FUSELAGE SKIN HAS TWO CRACKS AT FRAME 75 AND STRINGER 2R. PERFORMED A PERMANENT REPAIR IAW SRM 53-31-01 FIG 219.