What was found
DURING A C-CHECK INSPECTION, IT WAS DISCOVERED DISHED FASTENERS ON FUSELAGE SKIN AT BS 351, BELOW STRINGER 26R. ACCOMPLISHED SKIN PANEL AND T-CHORD REPLACEMENT IAW B727 SRM 53-30-2, FIG 2 AND SRM 51-30-2. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A C-CHECK INSPECTION, IT WAS DISCOVERED DISHED FASTENERS ON FUSELAGE SKIN AT BS 351, BELOW STRINGER 26R. ACCOMPLISHED SKIN PANEL AND T-CHORD REPLACEMENT IAW B727 SRM 53-30-2, FIG 2 AND SRM 51-30-2. (M)