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Old 30th Nov 2018, 12:41
  #74 (permalink)  
Join Date: Feb 2017
Location: Isla Grande
Posts: 825
Concerning MCAS on the accident flight.

In the tech log no report of SS on previous flight...!?

Anyhow "the DFDR showed the stick shaker activated during the rotation and remained active throughout the flight."

So the first activation of SS was after replacement of LH AoA sensor.
Is it possible to install a RH AoA sensor in the LH position?

Part number confusion...?

Just asking.
gearlever is offline