What was found
LT FUSELAGE SKIN AT FRAME 35 AT STRINGER 30 HOLE 2 CRACKED (DOWNWARD/AFT) IN SIDE SHELL. ACP REPAIR OF FR 35L 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.
LT FUSELAGE SKIN AT FRAME 35 AT STRINGER 30 HOLE 2 CRACKED (DOWNWARD/AFT) IN SIDE SHELL. ACP REPAIR OF FR 35L STR 30 AS PER ECRA 5320-02797 PART 1.