Manifold pressure is the absolute pressure at the intake manifold and increases as throttle is increased and vice versa. However, when the engines are shutoff, the manifold reads ambient pressure. My question is, why does it read ambient pressure when engines are shut off when the throttles at closed?


The intake manifold is where the air flows from outside into the engine, so obviously it must be open to the outside. So when everything is calm, the pressure quickly equalizes and the manifold pressure is equal to the ambient pressure.

The non-obvious thing is actually why it differs when the engine is running.

When the engine is running, it sucks air in. The volume of air per unit of time is proportional to its rotational speed: higher RPM means more strokes per minute and each stroke has the same displacement.

Now without any restriction in the intake manifold, the air would still enter at the ambient pressure (speaking of normally aspirated engine). And with fully open throttle, the restriction is small enough that the manifold pressure is indeed only a little below ambient.

It is only as you close the throttle that you create significant restriction, which reduces the manifold pressure.

But the reduction is still proportional to the engine RPM. With engine not running there is no suction, so the pressure can't decrease and the gauge still shows ambient pressure.

This dependence on the RPM also means that it is not actually good indicator of the power the engine produces. When you increase RPM by adjusting the mixture, the engine power will increase—because it takes more power to sustain higher RPM—but the manifold pressure will decrease—because there is more suction. The same also happens when you increase RPM by advancing propeller pitch selector.

What manifold pressure is good indicator of though, and the reason it exists, is the engine wear. The amount of air, and fuel, are proportional to the manifold pressure, and therefore so is the peek pressure when the air is compressed and the fuel burnt. And the higher the peek pressure, the more wear on the components. That is why there is absolute maximum you should never exceed and continuous power limit that you should only exceed for limited time on take-off or in emergency.

Note that the relations are further complicated in turbocharged engines where higher engine RPM also mean higher turbocharger RPM and that increases the pressure gain on the turbocharger that adds to the manifold pressure.


Scenario 1: engine running slow

Since there is always at least one piston going down and its valve open, this increases the volume of the manifold and reduces the pressure. Since the throttle is almost closed, the pressure remains low and near vacuum (low MAP), i.e., outside air is not allowed to rush in freely.

Scenario 2: engine shut down

With the engine shutdown, there is no piston action and the pressure can stabilize with the ambient (the throttle valve is not air tight, that's why you can have the engine running with the throttle pulled all the way back, different story for the mixture control).


enter image description hereImage source

Because the manifold is connected to the ambient air via the air intake. The throttle does not hermetically seal against ambient pressure differential when closed, there is no design requirement for this condition.

The transducer measures pressure, not pressure differential.

  • $\begingroup$ @Koyovia Does the MP gauge read the uncorrected barometric pressure or the ATIS altimeter setting pressure? I’m guessing uncorrected. $\endgroup$ – JScarry Sep 17 '17 at 15:01
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    $\begingroup$ @JScarry The altimeter setting reported by the ATIS is QNH (Pressure at sea level calculated from QFE (Pressure at field elevation) using the ISA (International Standard Atmosphere)-model). The MAP would indicate QFE (or at least close to) - to the extent that it is calibrated. $\endgroup$ – Waked Sep 17 '17 at 21:56

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