What was found
FUSELAGE SKIN CRACK AT STA 870 STRINGER 23RT. REPAIRED IAW SRM 53-00-01 FIG 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACK AT STA 870 STRINGER 23RT. REPAIRED IAW SRM 53-00-01 FIG 201.