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enter image description here
A pop-up rod on a the FO's control column on a DC-9 that shows the Mach trim position. (YouTube)

Regarding the title, I'm not sure if it's just some or all jetliners (I tried to research it). On the DC-9, MD-80, and 737NG,* it is stated clearly in the FCOMs that the Mach trim moves the elevator to counter the Mach tuck. On the 737 the system starts operating above Mach 0.615 (See FCOM 9.20). And below is part of the text from the MD-80 FCOM:

Operating on a Mach schedule, the Mach trim compensator pulls the First Officer’s control column aft as Mach number increases. As the control column moves aft, an indicator rod on the left side of the First Officer’s control column extends, giving visual indication of Mach trim operation.

Why don't the mentioned Mach trimmers use the stabilizer? I always thought the stabilizer had more fine control, not to mention the drag penalty of an offset elevator. There must be a reason for moving the control column aft and not just trim the stabilizer.

Update

It is not an era's technology limitation. The Boeing 707 moved the stabilizer for its Mach trim according to both an accident investigation report and a Cambridge University book. And like the DC-9, the 707 did not have hydraulics for its elevators.

* The MD-90** and B717 move their stabilizer according to their FCOMs.
** Unlike the rest of the DC-9 family, the MD-90 uses a powered-elevator.

My current working hypothesis is that the answer relates to stick forces, but I can't find any reliable sources on the design reasoning.

I checked these posts where Mach tuck was discussed:

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  • $\begingroup$ The comment on the answer on the second question you linked mentions that deflecting elevator produces more force, though with more drag. So maybe the stabiliser range wasn't enough. $\endgroup$
    – Jan Hudec
    Sep 14 '18 at 18:29
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I think it's because the 9 uses free floating elevators with servo tabs to move them. The columns just move the servo tabs which means the actual input forces are really low and there is feel spring unit in the system. For mach trim they just have a servo motor that applies a little pull to the column via the feel spring unit, and the rod extends to tell you the motor is pulling on the column.

There is a trimmable stab for pitch trim, but it will have a fairly primitive controller (figuring pre-microprocessor 1965 electronics) and to incorporate a mach trim mode into the stab control system was probably much more expensive than the simple setup they came up with.

The more modern setup, with hydraulic elevators that are always faired with the stab when not displaced by a control input, and a stab controller that is fully integrated into the autopilot and air data systems is way less drag.

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    $\begingroup$ Did the trimmable stab had a controller at all? It might have been completely manual (it is actuated with electric motor and jackscrew and controlled with a set of switches). $\endgroup$
    – Jan Hudec
    Sep 14 '18 at 18:33
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    $\begingroup$ Not sure exactly what it uses, but when I say "controller" it could just be a relay box and maybe some analog electronics using pots and such, like you might have if there was a flap compensation feature. Or you could see a controller with some basic logic circuits using Integrated Circuit chips, which were the newest thing at the time, but the microprocessor was still another 8-10 years away when the 9 was designed. $\endgroup$
    – John K
    Sep 14 '18 at 19:35
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    $\begingroup$ I actually think it was really just a switch box. Further I suspect there was no position sensor, so the mach trim wouldn't have a reference for introducing specific bias. $\endgroup$
    – Jan Hudec
    Sep 14 '18 at 19:48

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