What was found
PDX - CRACK IN WEB STIFFENER FOR AFT CONE. STIFFENER IS AT 12 O'CLOCK POSITION ON CONE NR 1 LOWER ENGINE COWL. COMPLETED INSTALLATION OF FASTENER AS PER Q400 SRM 51-42-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
PDX - CRACK IN WEB STIFFENER FOR AFT CONE. STIFFENER IS AT 12 O'CLOCK POSITION ON CONE NR 1 LOWER ENGINE COWL. COMPLETED INSTALLATION OF FASTENER AS PER Q400 SRM 51-42-03.