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Gwidon

CoG in 737-200 by tinmouse

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Hello,I just read the 737-200 Maximum t/o EPR reference (included in file b737-200adv by Gustavo Omykron, thanks Gustavo ;-) ). In this table we have got stablizer trim settings (initial position during t/o) depend on CoG value and flaps position. I wonder, in which way can we calculated CoG value in 737-200 by tinmouse ?RegardsGwidon

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Hello Mike,"Hi Gwidon,long time no speak"To long ... very sad :-((( Dear Mike thank you for your quick and useful respond. You are, like allways, simply the best ;-)))Thanks my friendGwidon

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