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Printed page iv. PDF page 4.
................................................................................................................................. 56 1.6.5.6 Autopilot................................................................................................................................................................................Open final report at PDF page 4Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page ix. PDF page 9.
System AD Air Data Computer ADR Air Data System ADC Automatic Flight Control System ADS Autopilot Flight Director System AFCS Accessory Gear Box AFDS Above Ground Level AGB Airplane Flight manual. AGL Accident Investigation Bureau AFM Angle of Attack VaneOpen final report at PDF page 9Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 20. PDF page 20.
forces recorded in the DFDR, the captain was the pilot flying. Phase1:From takeoff to Autopilot engagement (from 5h 36 min 12 s until 5h 39 min 23 s) At 5:36:12 the Airplane lined up on runway 07R at field elevationOpen final report at PDF page 20Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 22. PDF page 22.
dangerously too high speed). At 05:38:56, the captain stated "command" to engage the autopilot (A/P). A/P disconnect warning sounded for 2 seconds. At 5:38:59, as the Airplane crossed 400ft Radio Altitude, VNAV mode engaged. From that time, the F/D TOOpen final report at PDF page 22Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 23. PDF page 23.
Investigation Report B737- MAX 8, ET-AVJ December 2022 FIGURE 1: PHASE1 FROM TAKEOFF TO AUTOPILOT ENGAGEMENT Phase 2: Under Autopilot engagement (from 5h 39 min 23 s until 5h 39 min 56s) At 05:39:23, at about 1,000 feet Radio Altitude,Open final report at PDF page 23Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ
Printed page 24. PDF page 24.
Report B737- MAX 8, ET-AVJ December 2022 minimum operational speed as target speed) and autopilot commanded a pitch down to accelerate towards the erroneous minimum operating speed. At 05:39:30, the radar controller identified ET-302 and cleared the flight to climbOpen final report at PDF page 24Aircraft Accident Investigation Report B737 MAX 8, ET-AVJ