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kostya074

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About kostya074

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    Russia
  1. Hello. Yes, example: arpt UUWW alt 690ft QNH 1007 take CORRECTION TO ELEVATION FOR PRESS ALT from the table; 200 ft 690+200=890ft In my calculation, I chose the worst height value of 2000 feet (so as not to engage in interpolation) Pressure altitude = 890ft Regards Konstantin
  2. Hi, thanks for the work done! Version 1.5.5 of the B737CL calculator is incorrect for me, for example: B737-500 engines rating 20K arpt UUWW wind 190/8 OAT + 15 * C QNH 1007 flaps 5 A / C ON A / I OFF TOW 52300 kg a message appears that max TOW = 51700 kg, although using FCOM we get max TOW = 55100 and is it possible to add intersections manually? I apologize for machine translation Regards Konstantin
  3. Hi, thanks for the work done! Version 1.5.5 of the B737CL calculator is incorrect for me, for example: B737-500 engines rating 20K arpt UUWW wind 190/8 OAT + 15 * C QNH 1007 flaps 5 A / C ON A / I OFF TOW 52300 kg a message appears that max TOW = 51700 kg, although using FCOM we get max TOW = 55100 and is it possible to add intersections manually? I apologize for machine translation Regards Konstantin
  4. Hello! How can I get the latest update? The link to 1.5.5 (1.6.2 ?) message about the deleted file ...
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