Search report text, read a short matching passage, then open the source page.
Exact phrases match first; otherwise all words must occur close together. Six excerpts maximum. Text extraction cannot search image-only charts. Warsaw uses a report transcription with missing figures and appendices.
8 matching PDF pages. Showing 6 short source excerpts. Open the document for full context.
Printed page 25. PDF page 25.
Phase 3: From A/P disconnect to stabilizer trim cutout (from 5h 39 min 56s until 5h 40 min 38s) At the time A/P disconnected, LH pitch F/D bar disappeared due to the same logic conditions that caused the APdisconnection. TheOpen final report at PDF page 25Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 26. PDF page 26.
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, - The Airplane was 1,500 ft aboveOpen final report at PDF page 26Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 27. PDF page 27.
Phase 4: flight while the stab trim cutout switches were in the cutout position (from 5h 40 min 38 s until 5h 43 min 11 s) At 05:40:43: approximately five seconds after the end of crew manual electrical trim upOpen final report at PDF page 27Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 138. PDF page 138.
h 40 min 37s, the move of the switches into the CUTOUT position occurred between 5 h 40 min 38 s and 5 h 40 min 43 s. According to the CVR transcript, the crew exchanged about the use ofOpen final report at PDF page 138Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 126. PDF page 126.
22.5 revolutions; but to resolve a mistrim of -2.7� it would have to be rotated through 40.5 revolutions, i.e., 80% more. 1.16.3 Angle of Attack, AOA Values At 5 h 38 min 44 s, the LH AOA recorded values beganOpen final report at PDF page 126Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 137. PDF page 137.
disengaged, one single sample of FCC trim UP was recorded (Speed Trim activation). At 5 h 40 min 00 s, MCAS function triggered for the first time. At the end of the MCAS activation, the stabilizer position was 2.1 units.Open final report at PDF page 137Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ