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High EGT on one cylinder on Lycoming or Continental aircraft engine

Poor mixture distribution
1. Partially plugged fuel nozzle. A partially plugged nozzle will allow enough fuel to flow at idle for combustion. As power is increased, cylinder gradually leans out until detonation or lean mis-fire occurs. Exhaust gas temperature will rise and not respond to mixture control until idle cut off is reached. The reason for this is that the blockage now becomes the primary restriction and is independent of mixture control position. Nozzles can be flow-checked by comparing their outputs in containers of equal size to locate plugged or partially plugged nozzle.

2. Damaged nozzle. A nozzle damaged from over torque will not meter fuel properly. Damage caused by over torque usually effects the air-bleed at idle.

3. Air leak into induction system.

4. Burned (leaking) exhaust valve.

5. Probe problem.

6. Inside diameter of fuel lines too small (Lycoming engines). Lines must be between 0.85 and .090 inches I.D. Use of primer line instead of fuel injector line. The only exception to this rule is the IO540 -E1B5 used in the Aero Commander 500S. Fuel lines on Lycoming engines should have an inside diameter of .085 inch to .090 inch. 

EGT Probe

(Westach Probes at 1,200 degrees F.- 26.03 millivolt, at 1600 degrees F. 35.24 millvolt)

 

 

 

 

 

 


 

 


 

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Disclaimer: sacskyranch.com contains abundant information relating to aircraft maintenance. The information provided  is not intended to supercede or supplement the F.A.A. approved  maintenance and/or operator’s manuals. Those F.A.A. approved manuals must be utilized when performing maintenance and/or operating aircraft.