As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
IDENTIFIED A CRACK AT 2 PLACES ON THE RIGHT SIDE OF BS 1156 CHORD BETWEEN WL 281-269. STOP DRILLED ENDS OF CRACKS, REMOVED FASTENERS ON AFFECTED CHORD ASSEMBLY AND INSTALLED REPAIR STIFFENER ANGLE IAW ECO 1822. APPLIED ALODINE AND PRIMER BMS 10-11 TYPE 1 PRIMER TO ALL BARE SURFACES AND CORROSION INHIBITING COMPOUND. AIRCRAFT OK FOR SERVICE. (M)