Ever wanted to run your Carbon Cub on 3 cylinders versus 4? Did you now that every Carbon Cub has a control on the instrument panel to allow you to selectively "turn off" combustion in the #4 cylinder?
During a ground run up of my new Carbon Cub about after about 2 minutes at idle, the engine began to run rough. I had just installed Dynon Skyview Touch and the Engine Management System was working great. Just as the engine began to run rough I noticed that #4 CHT and EGT was falling off rapidly while #1, #2 and #3 CHT and EGT's were normal.
So #4 combustion had stopped at idle. If I increased RPM the CHT and EGT would rise slightly to about half the values of the other cylinders and the engine would run very rough.
That started a day of troubleshooting. Compression was normal, valves where moving, cylinder head looked fine and the LightSpeed ignition system tested normal. Induction system looked good. Change the spark plugs, no change.
After several calls to CubCrafters. Stan asked if the primer was closed. Coincidently I had checked the primer control just before the call and fount it fully in the "closed" position but it was not locked over the detent. So visually it looked like the primer was in the closed position but by pressing on the primer and rotating it, the control was on the wrong side of the detent in the "unlocked" position.
After properly "locking" the primer, I started the engine and all was normal. So the primer fully closed but "unlocked" will stop combustion in the #4 cylinder. The capillary tube from the primer control empties into the top of cylinder head on #4.
I have now confirmed that others have discovered this "undocumented feature". At least one person discovered the feature in flight. Had this happened to me in flight I would be looking for the first safe place to land.
Why did this start after a few minutes of a ground run? I am guessing when I attempted to close the primer originally I did not rotate the control far enough to get past the detent. So at some point during the engine run the control popped off the detent to the "open" position causing additional fuel to be introduced down the tube to #4 cylinder. It is amazing to me that such a small "leak" in the cylinder can kill combustion. My speculation, but I would guess since the primer sources fuel from the top of the fuel strainer when the primer is unlocked the lower manifold pressure in #4 pulls fuel from the strainer through the primer then out to the cylinder head of #4 causing an excessively rich mixture. When I pulled #4 spark plugs they had black soot suggesting a rich mixture.
The "Starting Engine" checklist has the following warning about the use of the Engine Primer.
But I can find no warning about what will happen if the control is not "Closed and Locked" versus just closed. The "Locked" part was very important in my situation as I confirmed the primer was fully closed, it just was not locked.
I consider this "feature" to be a safety of flight issue. Loss of combustion in one cylinder will persuade most of us to get on the ground as soon as possible, possibly making a decision to land in an off airport location.
I have never used the primer in a Carbon Cub. I am considering deactivating the primer control. It is also a source of nuisance fuel leaks in the cockpit. The system could be easily deactivated by capping the line at the primer and #4 cylinder head. Certainly deactivating the priming system for summer operation would make sense.