3DDave
Aerospace
- May 23, 2013
- 10,689
"That might well be true, but how many other airlines actually did do that?"
It's an EMERGENCY AD and a Memory Item update to the FCOM.
If they chose to ignore it in spite of the relation to a recent fatal accident it does not fall on Boeing.
All the airlines looked at it and all of them accepted it as did all the pilots and all the CAAs - because it had worked. Demonstrably. In recent memory, so one would think they would examine it carefully.
The reason these instructions don't tell them that pulling back may not stop the trim (aside from it being plainly obvious when it does stop trim, and only works -during- some particular trim event and ) is that this is not a procedure solely for MCAS. It why it refers to "relaxing the column" and not puling back.
This is a procedure for the control fault of runaway stabilizer - which could be caused by a wire breakthrough or switch failure providing unexpected power or control signal that would also not respond to pulling back, or a melted relay or a software fault other than MCAS; maybe due to a dead transistor in a memory chip. There would be no "5 seconds" for a mechanical or electrical fault, so no need to mention it. It might be intermittent or it might be continuous.
The pilots are there to deal with symptoms - the symptom is "runaway stabilizer" not "MCAS due to SMYD/..."
The pilots, the airlines, the CAAs also did not push back on the term "runaway stabilizer" but I've seen too many who claim it cannot be "runaway" if it stops after some interval. "That's not runaway, it stops after a while" they write, as if it matters. Since there is a stop at the end of the jackscrew, by that definition, there can never be trim runaway.
Maybe it should have been called "excess trim force on the control wheel"
Do pilots need a kindergarten class on how to trim a plane? Maybe they do, as the Captain in ET-302 did apply the electric trim but did not trim the plane. Should it be explained as if to a five year old instead of a multi-thousand hour Captain?
"Initially, higher control forces may be needed to overcome any stabilizer nose down trim already applied.
Electric trim can be used to neutralize control column pitch forces before moving the STAB TRIM CUTOUT switches to CUTOUT"
Does that not say what is to be done? It said "Electric trim can be used to neutralize control column pitch forces" and that was true - electric trim continued to function. "neutralize control column pitch forces" is that unclear as the reason to use the electric trim? "neutralize control column pitch forces before moving the STAB TRIM CUTOUT" is what is to be done "before" cutout.
When the Captain read these new instructions what did the Captain think it meant? We don't know because his airline never asked him or the FO (first officer.) We also don't know because there is no record his Chief pilot or the CAA had talked to them either.
From the FDR it is clear this crew was beyond desperate to get the autopilot running even during the non-MCAS related event for which they are trained and given clear instructions to disable the autopilot and autothrottle. ET-302 was gaining altitude and was in a stable climb, when they decided to try to re-engage the autopilot. They turn on the thing they are told to turn off and keep off to try the autopilot and, when that failed, they left turned on the thing they are told to turn off and keep off.
It was that experimentation that lost them all control of the plane. Per the FDR, until they tweaked the trim switch to see if the trim motor worked, MCAS had issued no recent trim commands and MCAS stopped moving the stab the instant any electric trim command was used.
It is more imperative to find out why the training failed so miserably and why their airline and CAA failed to ensure they were capable of handling what is a trivial physical action. Planes can be examined to see if the software is good, but what of the thousands of pilots who may be just as poorly trained?
It's an EMERGENCY AD and a Memory Item update to the FCOM.
If they chose to ignore it in spite of the relation to a recent fatal accident it does not fall on Boeing.
All the airlines looked at it and all of them accepted it as did all the pilots and all the CAAs - because it had worked. Demonstrably. In recent memory, so one would think they would examine it carefully.
The reason these instructions don't tell them that pulling back may not stop the trim (aside from it being plainly obvious when it does stop trim, and only works -during- some particular trim event and ) is that this is not a procedure solely for MCAS. It why it refers to "relaxing the column" and not puling back.
This is a procedure for the control fault of runaway stabilizer - which could be caused by a wire breakthrough or switch failure providing unexpected power or control signal that would also not respond to pulling back, or a melted relay or a software fault other than MCAS; maybe due to a dead transistor in a memory chip. There would be no "5 seconds" for a mechanical or electrical fault, so no need to mention it. It might be intermittent or it might be continuous.
The pilots are there to deal with symptoms - the symptom is "runaway stabilizer" not "MCAS due to SMYD/..."
The pilots, the airlines, the CAAs also did not push back on the term "runaway stabilizer" but I've seen too many who claim it cannot be "runaway" if it stops after some interval. "That's not runaway, it stops after a while" they write, as if it matters. Since there is a stop at the end of the jackscrew, by that definition, there can never be trim runaway.
Maybe it should have been called "excess trim force on the control wheel"
Do pilots need a kindergarten class on how to trim a plane? Maybe they do, as the Captain in ET-302 did apply the electric trim but did not trim the plane. Should it be explained as if to a five year old instead of a multi-thousand hour Captain?
"Initially, higher control forces may be needed to overcome any stabilizer nose down trim already applied.
Electric trim can be used to neutralize control column pitch forces before moving the STAB TRIM CUTOUT switches to CUTOUT"
Does that not say what is to be done? It said "Electric trim can be used to neutralize control column pitch forces" and that was true - electric trim continued to function. "neutralize control column pitch forces" is that unclear as the reason to use the electric trim? "neutralize control column pitch forces before moving the STAB TRIM CUTOUT" is what is to be done "before" cutout.
When the Captain read these new instructions what did the Captain think it meant? We don't know because his airline never asked him or the FO (first officer.) We also don't know because there is no record his Chief pilot or the CAA had talked to them either.
From the FDR it is clear this crew was beyond desperate to get the autopilot running even during the non-MCAS related event for which they are trained and given clear instructions to disable the autopilot and autothrottle. ET-302 was gaining altitude and was in a stable climb, when they decided to try to re-engage the autopilot. They turn on the thing they are told to turn off and keep off to try the autopilot and, when that failed, they left turned on the thing they are told to turn off and keep off.
It was that experimentation that lost them all control of the plane. Per the FDR, until they tweaked the trim switch to see if the trim motor worked, MCAS had issued no recent trim commands and MCAS stopped moving the stab the instant any electric trim command was used.
It is more imperative to find out why the training failed so miserably and why their airline and CAA failed to ensure they were capable of handling what is a trivial physical action. Planes can be examined to see if the software is good, but what of the thousands of pilots who may be just as poorly trained?