What was found
PDX- STRESS PANEL 622CT HAS SPINNING SCREW AND NUTPLATE AT AFT ROW, SIX FASTENERS INBOARD FROM AFT OUTBOARD CORNER. REPAIRED IAW DHC-8 Q400 SRM 51-42-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PDX- STRESS PANEL 622CT HAS SPINNING SCREW AND NUTPLATE AT AFT ROW, SIX FASTENERS INBOARD FROM AFT OUTBOARD CORNER. REPAIRED IAW DHC-8 Q400 SRM 51-42-05.