What was found
CRACK IN FUSELAGE SKIN AT BS 530, S16R. INSTALLED REPAIR IAW SRM 5-30-3, FIG 48, DETAIL VII.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IN FUSELAGE SKIN AT BS 530, S16R. INSTALLED REPAIR IAW SRM 5-30-3, FIG 48, DETAIL VII.