March 26, 20206 yr My current IAS at FL200 is 159kts | 183mph; 206kts GS Head wind 14kts. Aircraft at MTOW. manifold pressure: 30.2 in Hg | 1703 RPM| Throttle at 77% | Props at 52% | Mixture at 30% Using Bernt’s FDE. Running very smooth but certainly cannot get max cruising speed. How are the results above? Regards, Fred Fleuren
March 26, 20206 yr 12 minutes ago, Fearless said: Running very smooth but certainly cannot get max cruising speed. Which speed are you looking to max during cruise? You appeared to refer to three. Indicated, true, or ground speed? What is your TAT/OAT? Do you have a valid reference chart for FL 200 at various TAT/OAT? Edited March 26, 20206 yr by fppilot Frank Patton Corsair 5000D Airflow Case; MSI B650 Tomahawk MOB; Ryzen 7 7800 X3D CPU; ASUS RTX 4080 Super; NZXT 360mm liquid cooler; Corsair Vengeance 64GB DDR5 4800 MHz RAM; RMX850X Gold PSU;; ASUS VG289 4K 27" Display; Honeycomb Alpha & Bravo, Crosswind 3's w/dampener. Former USAF meteorologist & ground weather school instructor. AOPA Member #07379126 "I will never put my name on a product that does not have in it the best that is in me." - John Deere
March 26, 20206 yr Author Greetings Frank, Thanks for that. Found the performance tables from the C421C POH and the current IAS is pretty close. OAT is 20F Edited March 26, 20206 yr by Fearless Regards, Fred Fleuren
March 26, 20206 yr Just checked the RW POH values at MTOW at FL200. 1700RPM, 30.0MP = 205ktas. edit. Temp is lower than standard but not much. Since you departed at MTOW I assume you've got a bit lighter at FL200. At FL200 159kias = 216ktas but the IAS/TAS ratio in FSX/P3D doesn't exactly match RW data and deviates even more if temp differs from ISA. Edited March 26, 20206 yr by FDEdev
March 26, 20206 yr No. Just edited my above post. Btw, you will not get max cruise performance with such low RPM and MP settings. For max cruise you need 1900RPM and 32.5MP (225ktas at ISA) Edited March 26, 20206 yr by FDEdev
March 26, 20206 yr Author Much appreciated all. I did make a slight adjustment in the aircraft.cfg file prior to listing the results above namely increased the prop diameter from 7 to 7.6 as per POH and prop thrust scalar to 1.17 as well as engine power scalar to 1.1 Edited March 26, 20206 yr by Fearless Regards, Fred Fleuren
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