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March, 2018 Meeting Handouts & Presentation materials http://eaa21.org/viewtopic.php?f=2&t=372 |
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Author: | rhino [ Thu Mar 15, 2018 4:48 am ] |
Post subject: | March, 2018 Meeting Handouts & Presentation materials |
Here are the presentation materials discussed last night: AC 90-109.pdf [269.28 KiB] Downloaded 823 times AC 90-89A.pdf [567.14 KiB] Downloaded 805 times AC_90-116.pdf [1.14 MiB] Downloaded 744 times Chapter 10 (Weight & Balance) of the Pilots Handbook of Aeronautical Knowledge (PHAK) may be found here: 12_phak_ch10.pdf [5.08 MiB] Downloaded 778 times And the presentation slides here: march, 2018 eaa 21 meeting.pptx [198.25 KiB] Downloaded 788 times |
Author: | Vaughn DeCoster [ Thu Mar 15, 2018 7:07 am ] | ||
Post subject: | Re: March, 2018 Meeting Handouts & Presentation materials | ||
Thanks Bill, great job last night. I wanted to share more accurate Cirrus performance figures. In my few hours in the SR20 I see a little less airspeed but also less fuel burn running LOP. I’m still learning so I’ll post new data next month. Here’s the SR20 POH: http://www.cospilot.com/files/SR20_POH.pdf
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Author: | rhino [ Fri Mar 16, 2018 5:38 am ] |
Post subject: | Re: March, 2018 Meeting Handouts & Presentation materials |
Here are the March, 2018 meeting slides in PDF format: march, 2018 eaa 21 meeting.pdf [353.08 KiB] Downloaded 808 times |
Author: | rhino [ Fri Mar 16, 2018 6:10 am ] |
Post subject: | DA40-180 Mean Aerodynamic Chord calculation per POH |
OK, so Zeller was correct (though don't tell him I said so...). Herein is the POH data on the DA40-180 tapered wing and the APPROX MAC in feet. The inch conversion and W&B tolerance I calculated to be respectively: MAC (inches) 45.72 and, W&B tolerance for AC less than 5,000 lb. gross (see AC 43.13-1) is: 0.05 x MAC = 0.05 x 45.72 = 2.3 inches; wt. <=1.0 US pound Note: these are estimates. Please check with your A&P for the actual requirements. These are considered "negligible weight and CG changes". Reference FAA W&B Handbook and AC 43.13-1/2B for additional information (too big to attach here). DA 40-180 Wing data from the POH: Wing Airfoil Wortmann FX 63-137/20- W4 Wing Area appr. 13.54 m2 appr. 145.7 sq.ft. Mean aerodynamic chord (MAC) appr. 1.121 m appr. 3ft 8.1 in Aspect ratio appr. 10.53 Dihedral appr. 5° ) Leading edge sweep appr. 1° |
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