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Printed page 27. PDF page 27.
electrical trim up inputs, a third automatic nose-down trim (MCAS) triggered. There was no corresponding motion of the stabilizer, which is consistent with the stabilizer trim cutout switches beingin the `'cutout'' position At the beginning of this phase, the captainOpen final report at PDF page 27Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 225. PDF page 225.
Captain's electric trim-up inputs, a third automatic nose-down trim was triggered. There was no corresponding motion of the stabilizer since the stab trim cut-out switches were in cut-out position. At that moment, IAS was 327Kt, and on the F/O's speedOpen final report at PDF page 225Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 249. PDF page 249.
activated for the third time, an automatic nose-down trimwas commanded by the FCC.There was no corresponding motion of the stabilizer, which is consistent with the stabilizer trim cutout switches being in the `'cutout'' position; 32. The captain repeatedly requested theOpen final report at PDF page 249Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ