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WestJet Encore WEN3532

Printed page 21. PDF page 21.

(e.g., to climb) or during engine start-ups and shutdowns. Therefore, it is likely that the main fatigue crack (rotor blade No. 1) developed over more than 1 flight. The fracture surfaces on both rotor blades showed very similar fractographic features

Open official document at PDF page 21Air Transportation Safety Investigation Report A23P0020: Engine compressor failure and fire