Ethiopian 737 MAX 8 crash
#472
In a land of unicorns
Joined APC: Apr 2014
Position: Whale FO
Posts: 6,465
I noticed a sentence about the N1 stabilized at 94% (during takeoff roll). From this point for most of the flight the N1 reference remained there and the throttles didn’t move.
I don’t see any specific mention of the auto throttles being used or if/when they disengaged. I would expect some movement if they were engaged, but if not did the crew forget that they needed to control thrust on their own?
Sent from my iPhone using Tapatalk
I don’t see any specific mention of the auto throttles being used or if/when they disengaged. I would expect some movement if they were engaged, but if not did the crew forget that they needed to control thrust on their own?
Sent from my iPhone using Tapatalk
#473
Gets Weekends Off
Joined APC: Feb 2015
Posts: 983
Why were there electric trim inputs before placing the switches in cutout so short and so few? If you have pressure on the flight controls trim the pressure off. Hold the trim. They used small quick inputs then quit. All the time the throttles are at T/O Trust.
They sure had time to talk on the radio a lot during this but not to trim?
#474
Gets Weekends Off
Joined APC: Dec 2018
Posts: 165
Seems to be the case after moving the cutout switches back to normal as well. Only two quick clicks and then nothing, even after the last MCAS command. I also notice that their altitude appears to be under control, even slowly increasing, until they turned the electricity back on.
#475
In a land of unicorns
Joined APC: Apr 2014
Position: Whale FO
Posts: 6,465
2.3 to 2.1 is measurable. .2 to be exact.
Why were there electric trim inputs before placing the switches in cutout so short and so few? If you have pressure on the flight controls trim the pressure off. Hold the trim. They used small quick inputs then quit. All the time the throttles are at T/O Trust.
They sure had time to talk on the radio a lot during this but not to trim?
Why were there electric trim inputs before placing the switches in cutout so short and so few? If you have pressure on the flight controls trim the pressure off. Hold the trim. They used small quick inputs then quit. All the time the throttles are at T/O Trust.
They sure had time to talk on the radio a lot during this but not to trim?
Main reason will be pilot error - they let the trim run away a bit too far, and they let their speed climb way too high. But the fact is - Boeing's design allowed a single failure degrade the handling to a point where it clearly was very, very difficult to keep the plane under control. Under Part 25, this should be "extremely improbable" - defined as 1 event in 1 billion flight hours, or never in the expected life of the whole fleet. Clearly that requirement is not fulfilled with the 737 MAX.
To slightly adjust an old saying, Boeing put the pilots in a position, where only superior skills could have saved them.
#476
Gets Weekends Off
Joined APC: Jun 2014
Posts: 924
#477
2.3 to 2.1 is measurable. .2 to be exact.
Why were there electric trim inputs before placing the switches in cutout so short and so few? If you have pressure on the flight controls trim the pressure off. Hold the trim. They used small quick inputs then quit. All the time the throttles are at T/O Trust.
They sure had time to talk on the radio a lot during this but not to trim?
Why were there electric trim inputs before placing the switches in cutout so short and so few? If you have pressure on the flight controls trim the pressure off. Hold the trim. They used small quick inputs then quit. All the time the throttles are at T/O Trust.
They sure had time to talk on the radio a lot during this but not to trim?
Checking your history seems you and your family have quite a vested interest in Boeing, that explains why you're slamming and slandering these dead pilots. Really in poor taste and lacks any kind of professional character.
#478
Gets Weekends Off
Joined APC: Dec 2018
Posts: 165
Proactively trimming off control forces and basic power/airspeed management don't sound like advanced level skills.
It sounds like these guys were in over their heads from the start. They activated the autopilot even with the stick shaker active. The overspeed clackers start going off and they're still messing with the guidance panel and talking to ATC. Timid to non-existent effort to keep the trim under control. Zero power management...
#479
:-)
Joined APC: Feb 2007
Posts: 7,339
Proactively trimming off control forces and basic power/airspeed management don't sound like advanced level skills.
It sounds like these guys were in over their heads from the start. They activated the autopilot even with the stick shaker active. The overspeed clackers start going off and they're still messing with the guidance panel and talking to ATC. Timid to non-existent effort to keep the trim under control. Zero power management...
It sounds like these guys were in over their heads from the start. They activated the autopilot even with the stick shaker active. The overspeed clackers start going off and they're still messing with the guidance panel and talking to ATC. Timid to non-existent effort to keep the trim under control. Zero power management...
#480
Gets Weekends Off
Joined APC: Mar 2013
Position: 737 FO
Posts: 269
I’m not sure what you mean by speed on elevator thrust mode. The report says at 1,000 feet the autopilot was engaged (on the 3rd attempt) and 20 seconds later level change at 238kts was selected. This climb mode the auto throttle will hold the N1 limit and the auto pilot will pitch to maintain airspeed. 18 seconds later the autopilot is off and MCAS is engaged.
But yes good point that it will overspeed the aircraft with the nose now coming down. But that still doesn’t relieve the crew from being pilots and not dangerously letting the speed run away.
Sent from my iPhone using Tapatalk
Thread
Thread Starter
Forum
Replies
Last Post