What was found
YYC - C4 FUSELAGE INTERIOR, RIGHT SIDE SUPPORT CHANNEL X240, STRINGER 22S HAS CORROSION ON END. REPAIRED IAW CORROSION PREVENTION CONTROL MANUAL, CHAPTER, PART 1, DHC-8-200 SRM 51-40-11, PAGES 1-4 AND 51-40-00, PAGES 1-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
YYC - C4 FUSELAGE INTERIOR, RIGHT SIDE SUPPORT CHANNEL X240, STRINGER 22S HAS CORROSION ON END. REPAIRED IAW CORROSION PREVENTION CONTROL MANUAL, CHAPTER, PART 1, DHC-8-200 SRM 51-40-11, PAGES 1-4 AND 51-40-00, PAGES 1-5.