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












8















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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  • 1





    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
    Dec 18 '18 at 19:22


















8















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




















  • 1





    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
    Dec 18 '18 at 19:22
















8












8








8








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
















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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share|improve this question













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edited Dec 19 '18 at 4:10









Pondlife

50.5k8135279




50.5k8135279










asked Dec 18 '18 at 15:33









user2325243user2325243

413




413








  • 1





    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
    Dec 18 '18 at 19:22
















  • 1





    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
    Dec 18 '18 at 19:22










1




1





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
Dec 18 '18 at 19:22







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
Dec 18 '18 at 19:22












2 Answers
2






active

oldest

votes


















14














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.






share|improve this answer





















  • 1





    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
    Dec 18 '18 at 20:00



















3














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

    oldest

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    2 Answers
    2






    active

    oldest

    votes









    active

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    active

    oldest

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    14














    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.






    share|improve this answer





















    • 1





      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
      Dec 18 '18 at 20:00
















    14














    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.






    share|improve this answer





















    • 1





      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
      Dec 18 '18 at 20:00














    14












    14








    14







    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.






    share|improve this answer















    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.







    share|improve this answer














    share|improve this answer



    share|improve this answer








    edited Dec 19 '18 at 9:10









    T.J.L.

    307515




    307515










    answered Dec 18 '18 at 16:39









    Skip MillerSkip Miller

    8,6532044




    8,6532044








    • 1





      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
      Dec 18 '18 at 20:00














    • 1





      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
      Dec 18 '18 at 20:00








    1




    1





    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
    Dec 18 '18 at 20:00





    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
    Dec 18 '18 at 20:00











    3














    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






























      3














      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




























        3












        3








        3







        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 Dec 18 '18 at 16:26

























        answered Dec 18 '18 at 15:52









        CrossRoadsCrossRoads

        4,0741517




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