What was found
RT FUSELAGE SKIN AT FRAME 35 AT STRINGER 30 HOLE 2 CRACKED IN SIDE SHELL (DOWNWARD AND AFT). ACP REPAIR OF FR 35R STR 30 AS PER ECRA 5320-02797 PART 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RT FUSELAGE SKIN AT FRAME 35 AT STRINGER 30 HOLE 2 CRACKED IN SIDE SHELL (DOWNWARD AND AFT). ACP REPAIR OF FR 35R STR 30 AS PER ECRA 5320-02797 PART 1.