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Printed page 26. PDF page 26.
replied "yes yes do it". The stab trim cut-out switches were most likely put in the cut-out positionat about 5 h 40 min 38 s(point G Figure 3). At this time: - the stabilizer position was at 2.3 units, -Open final report at PDF page 26Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 225. PDF page 225.
starts during manual flight, he should immediately put the stab- trim cut-out switches to cut-out position in order to avoid further mistrim. Further trimming and bringing the aircraft to neutral would then be accomplished by the use of a manualOpen final report at PDF page 225Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 232. PDF page 232.
the miss trim level they have on the event flight where the stab trim switches were in cut-out position was unsuccessful. 2.4FCTR Evaluation The Boeing constructed FCTR is designed to replicate the forces needed to move the trim wheel inOpen final report at PDF page 232Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Official web page.
During the 9 seconds of electric trimming, the stab trim cut-out switches were put in the cut-out position. At that moment, the stabilizer was at 2.3 units of trim and the Captain was pulling on the control column with aOpen the official web pageBEA published observations on the Ethiopian report
Printed page 29. PDF page 29.
CUTOUT SWITCHES WERE IN THE CUTOUT POSITION 8A click similar to the Stabilizer trim cut-out switches being put back on was heard on the CVR. 29Open final report at PDF page 29Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 138. PDF page 138.
min 37 s, the Captain expressed "yes, do it", followed by the F/O answer "Stab trim cut-out". Note: the investigation concluded that the F/O most likely moved the stab trim switches into the CUTOUT position at 5 h 40 minOpen final report at PDF page 138Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ