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Aircraft Performance

Aircraft Performance. This does not supercede ANY official document. Graph Method. With a CG of 36 inches and a weight of 2200 pounds, the CG is in limits. 34” and 2400 pounds won’t work. OAT: 19 C Pressure Alt: 7,000 Density Alt: Approx. 8,800.

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Aircraft Performance

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  1. Aircraft Performance This does not supercede ANY official document.

  2. Graph Method With a CG of 36 inches and a weight of 2200 pounds, the CG is in limits 34” and 2400 pounds won’t work

  3. OAT: 19 C Pressure Alt: 7,000 Density Alt: Approx. 8,800 This is a simple chart to understand. First, locate the temperature at the bottom of the graph. Next, find the pressure alt. (the slanted line), 7000 in this case. Draw a line up form the temp., and then another along the pressure altitude gradient.

  4. Table Method

  5. A BETTER EXAMPLE For the TBM 700 http://www.socataaircraft.com/homepage/english/menu_indexenglish.htm

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