I would like to know the rate of climb at gross weight for various altitudes such as 3,000; 5,000; etc.
I can either use density altitude to determine the planes actual climb rate using these numbers or if there is some other rate of climb correction based on temperature different from standard (like in the Cessna manuals) that would work okay too. I don't have the book yet, so for my preliminary x-c planning to bring the plane from Ohio to California, I need to know what kind of density altitude my Mooney M10 cadet can handle with gross weight. I have a fax if you would like to fax the info. Fax # 916-322-0868, but call me first at 916-445-4966 x1407. Any information would be appreciated. Thanks, Susan
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