MAP sensor in Ranger 2006 Argentine engine

Good morning, I hope someone from the community can solve this doubt, what happens is that I have a 2006 Ford Ranger with Argentine type engine with a problem, it happens that when I turn on it, the machine is unstable, it has no power when the ring, only in high speed, I already wash the acceleration body and the injectors, change the spark plugs, but it remains the same.

A mechanic suggested that the MAP sensor changed, I prepared to make the change, but I don't know where it is located, or in the Ford agency I knew how to say. . Can anyone tell me if this Ranger model uses it?

By the way, when I changed the spark plugs, I notice that they are wet as oil.

Thank you.

By the way, in the Ford they told me that the system is marked near the acceleration body, but there where to go it only carries a plastic plaque screwed, suppose they omitted it, because the truck had already been in a workshop, if so, where the harness was? ... I hope they help me

The MAP sensor in constant volume (gasoline) engines are always located in the admission multiple and on constant pressure engines (diesel) is located inside the EDC (Diesel electronic control) in your case it would be to be in the multiple of admission and be 3 -way if it is only MAP, and if it brings included the IAT sensor to be 5 roads. Please specify the motor code, which comes out under the hood or vehicle documents

now regarding your problem,

the MAP sensor is a sensor that measures the absolute pressure in the admission multiple. MAP is abbreviation of manifestation pressure. The MAP sensor measures the void generated in the admission multiple through a hose that connects both components.
When there is a condition of low motor load and a high vacuum, the command unit is responsible for impoverishing the combustible air mixture and the ignition progresses in order to achieve a greater fuel economy.
On the contrary, when a high load and a low vacuum is generated, the command unit enriches the mixture and delays ignition synchronization to avoid the phenomenon of the detonation.

It is very likely that it is the MAP sensor but, I recommend that you make a flight record with a SCAner or a resistance measurement with a multimeter between the sensor pins with the engine in Relay and verify it with a database of the sensor parameters according to the brand.