Why would you NOT lean on takeoff with a Lycoming engine?











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There is an excellent question/answer on leaning here. However what I have not yet understood is why one would NOT lean for takeoff below 3000 feet? Why does the Lycoming Service Directive 1497A/B still say to use Full Rich on takeoff?



Is it not right that a leaned engine is producing its highest power output and would you not want the highest power output on takeoff?










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  • The air is dense below 3000. You won't gain much by leaning that low. It's much better to trade a few HP for better cooling. Note that the SB specifies DENSITY altitude, not just indicated. A hot day in Phoenix will push you well above 3000' DA despite being only 1500' MSL. In this case, leaning before takeoff is appropriate.
    – acpilot
    9 hours ago

















up vote
5
down vote

favorite












There is an excellent question/answer on leaning here. However what I have not yet understood is why one would NOT lean for takeoff below 3000 feet? Why does the Lycoming Service Directive 1497A/B still say to use Full Rich on takeoff?



Is it not right that a leaned engine is producing its highest power output and would you not want the highest power output on takeoff?










share|improve this question









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user2325243 is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
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  • The air is dense below 3000. You won't gain much by leaning that low. It's much better to trade a few HP for better cooling. Note that the SB specifies DENSITY altitude, not just indicated. A hot day in Phoenix will push you well above 3000' DA despite being only 1500' MSL. In this case, leaning before takeoff is appropriate.
    – acpilot
    9 hours ago















up vote
5
down vote

favorite









up vote
5
down vote

favorite











There is an excellent question/answer on leaning here. However what I have not yet understood is why one would NOT lean for takeoff below 3000 feet? Why does the Lycoming Service Directive 1497A/B still say to use Full Rich on takeoff?



Is it not right that a leaned engine is producing its highest power output and would you not want the highest power output on takeoff?










share|improve this question









New contributor




user2325243 is a new contributor to this site. Take care in asking for clarification, commenting, and answering.
Check out our Code of Conduct.











There is an excellent question/answer on leaning here. However what I have not yet understood is why one would NOT lean for takeoff below 3000 feet? Why does the Lycoming Service Directive 1497A/B still say to use Full Rich on takeoff?



Is it not right that a leaned engine is producing its highest power output and would you not want the highest power output on takeoff?







aircraft-performance piston-engine






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edited 25 mins ago









Pondlife

50.1k8135276




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  • The air is dense below 3000. You won't gain much by leaning that low. It's much better to trade a few HP for better cooling. Note that the SB specifies DENSITY altitude, not just indicated. A hot day in Phoenix will push you well above 3000' DA despite being only 1500' MSL. In this case, leaning before takeoff is appropriate.
    – acpilot
    9 hours ago




















  • The air is dense below 3000. You won't gain much by leaning that low. It's much better to trade a few HP for better cooling. Note that the SB specifies DENSITY altitude, not just indicated. A hot day in Phoenix will push you well above 3000' DA despite being only 1500' MSL. In this case, leaning before takeoff is appropriate.
    – acpilot
    9 hours ago


















The air is dense below 3000. You won't gain much by leaning that low. It's much better to trade a few HP for better cooling. Note that the SB specifies DENSITY altitude, not just indicated. A hot day in Phoenix will push you well above 3000' DA despite being only 1500' MSL. In this case, leaning before takeoff is appropriate.
– acpilot
9 hours ago






The air is dense below 3000. You won't gain much by leaning that low. It's much better to trade a few HP for better cooling. Note that the SB specifies DENSITY altitude, not just indicated. A hot day in Phoenix will push you well above 3000' DA despite being only 1500' MSL. In this case, leaning before takeoff is appropriate.
– acpilot
9 hours ago












2 Answers
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8
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You are correct - you do want highest power. But you also want an engine that doesn't overheat and destroy itself.



Your initial climb-out is at an airspeed considerably less than cruising speed so you have less air flowing through the cylinder cooling fins. To compensate for this, flying full rich keep the combustion gasses cooler during the climb-out.



When you reach cruising altitude and level off, you may lean it out in accordance with the engine manufacturer's recommendations.



This "full rich on takeoff" procedure is not limited to Lycoming engines, either. TCM Continental and even the older Pratt and Whitney radials also go full rich on takeoff. It is close to a universal procedure for piston powered aircraft engines.



-Skip






share|edit























  • Another great plus about this is that it means that you can lean for more power should you ever discover that you don't have quite enough power to complete the takeoff safely. If you screw up calculating the weight, density, or distance, if you realize it soon enough, you can lean the engine and live to talk about it.
    – David Schwartz
    8 hours ago


















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2
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Full rich for max cooling when making high power. At higher altitude airports, air is thinner so you lean for the max power you can get at that altitude to be able to make it out.






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    2 Answers
    2






    active

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    2 Answers
    2






    active

    oldest

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    active

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    active

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    up vote
    8
    down vote













    You are correct - you do want highest power. But you also want an engine that doesn't overheat and destroy itself.



    Your initial climb-out is at an airspeed considerably less than cruising speed so you have less air flowing through the cylinder cooling fins. To compensate for this, flying full rich keep the combustion gasses cooler during the climb-out.



    When you reach cruising altitude and level off, you may lean it out in accordance with the engine manufacturer's recommendations.



    This "full rich on takeoff" procedure is not limited to Lycoming engines, either. TCM Continental and even the older Pratt and Whitney radials also go full rich on takeoff. It is close to a universal procedure for piston powered aircraft engines.



    -Skip






    share|edit























    • Another great plus about this is that it means that you can lean for more power should you ever discover that you don't have quite enough power to complete the takeoff safely. If you screw up calculating the weight, density, or distance, if you realize it soon enough, you can lean the engine and live to talk about it.
      – David Schwartz
      8 hours ago















    up vote
    8
    down vote













    You are correct - you do want highest power. But you also want an engine that doesn't overheat and destroy itself.



    Your initial climb-out is at an airspeed considerably less than cruising speed so you have less air flowing through the cylinder cooling fins. To compensate for this, flying full rich keep the combustion gasses cooler during the climb-out.



    When you reach cruising altitude and level off, you may lean it out in accordance with the engine manufacturer's recommendations.



    This "full rich on takeoff" procedure is not limited to Lycoming engines, either. TCM Continental and even the older Pratt and Whitney radials also go full rich on takeoff. It is close to a universal procedure for piston powered aircraft engines.



    -Skip






    share|edit























    • Another great plus about this is that it means that you can lean for more power should you ever discover that you don't have quite enough power to complete the takeoff safely. If you screw up calculating the weight, density, or distance, if you realize it soon enough, you can lean the engine and live to talk about it.
      – David Schwartz
      8 hours ago













    up vote
    8
    down vote










    up vote
    8
    down vote









    You are correct - you do want highest power. But you also want an engine that doesn't overheat and destroy itself.



    Your initial climb-out is at an airspeed considerably less than cruising speed so you have less air flowing through the cylinder cooling fins. To compensate for this, flying full rich keep the combustion gasses cooler during the climb-out.



    When you reach cruising altitude and level off, you may lean it out in accordance with the engine manufacturer's recommendations.



    This "full rich on takeoff" procedure is not limited to Lycoming engines, either. TCM Continental and even the older Pratt and Whitney radials also go full rich on takeoff. It is close to a universal procedure for piston powered aircraft engines.



    -Skip






    share|edit














    You are correct - you do want highest power. But you also want an engine that doesn't overheat and destroy itself.



    Your initial climb-out is at an airspeed considerably less than cruising speed so you have less air flowing through the cylinder cooling fins. To compensate for this, flying full rich keep the combustion gasses cooler during the climb-out.



    When you reach cruising altitude and level off, you may lean it out in accordance with the engine manufacturer's recommendations.



    This "full rich on takeoff" procedure is not limited to Lycoming engines, either. TCM Continental and even the older Pratt and Whitney radials also go full rich on takeoff. It is close to a universal procedure for piston powered aircraft engines.



    -Skip







    share|edit














    share|edit



    share|edit








    edited 11 hours ago

























    answered 11 hours ago









    Skip Miller

    8,4531942




    8,4531942












    • Another great plus about this is that it means that you can lean for more power should you ever discover that you don't have quite enough power to complete the takeoff safely. If you screw up calculating the weight, density, or distance, if you realize it soon enough, you can lean the engine and live to talk about it.
      – David Schwartz
      8 hours ago


















    • Another great plus about this is that it means that you can lean for more power should you ever discover that you don't have quite enough power to complete the takeoff safely. If you screw up calculating the weight, density, or distance, if you realize it soon enough, you can lean the engine and live to talk about it.
      – David Schwartz
      8 hours ago
















    Another great plus about this is that it means that you can lean for more power should you ever discover that you don't have quite enough power to complete the takeoff safely. If you screw up calculating the weight, density, or distance, if you realize it soon enough, you can lean the engine and live to talk about it.
    – David Schwartz
    8 hours ago




    Another great plus about this is that it means that you can lean for more power should you ever discover that you don't have quite enough power to complete the takeoff safely. If you screw up calculating the weight, density, or distance, if you realize it soon enough, you can lean the engine and live to talk about it.
    – David Schwartz
    8 hours ago










    up vote
    2
    down vote













    Full rich for max cooling when making high power. At higher altitude airports, air is thinner so you lean for the max power you can get at that altitude to be able to make it out.






    share|improve this answer



























      up vote
      2
      down vote













      Full rich for max cooling when making high power. At higher altitude airports, air is thinner so you lean for the max power you can get at that altitude to be able to make it out.






      share|improve this answer

























        up vote
        2
        down vote










        up vote
        2
        down vote









        Full rich for max cooling when making high power. At higher altitude airports, air is thinner so you lean for the max power you can get at that altitude to be able to make it out.






        share|improve this answer














        Full rich for max cooling when making high power. At higher altitude airports, air is thinner so you lean for the max power you can get at that altitude to be able to make it out.







        share|improve this answer














        share|improve this answer



        share|improve this answer








        edited 12 hours ago

























        answered 12 hours ago









        CrossRoads

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