Cirrus Design SR22
Section 9 Supplements
10. Record the new weight and C.G. values on the Weight and Balance Record. The above procedure determines the airplane Basic Empty Weight, moment, and center of gravity in inches aft of datum. C.G. can also be expressed in terms of its location as a percentage of the airplane Mean Aerodynamic Cord (MAC) using the following formula: C.G. % MAC = 100 x (C.G. Inches – LEMAC) ÷ MAC Where: LEMAC = 133.1 MAC = 47.7
13772-130 Original: 03-27-07
43 of 58
飞行翻译公司 www.aviation.cn 本文链接地址：西瑞22飞机信息手册 AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22_split_9.pdf
Section 9 Supplements
10. Record the new weight and C.G. values on the Weight and Balance Record. The above procedure determines the airplane Basic Empty Weight, moment, and center of gravity in inches aft of datum. C.G. can also be expressed in terms of its location as a percentage of the airplane Mean Aerodynamic Cord (MAC) using the following formula: C.G. % MAC = 100 x (C.G. Inches – LEMAC) ÷ MAC Where: LEMAC = 133.1 MAC = 47.7
13772-130 Original: 03-27-07
43 of 58
飞行翻译公司 www.aviation.cn 本文链接地址：西瑞22飞机信息手册 AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22_split_9.pdf
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