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Chris wrote in message .. .
How do aircraft manufactures determine the maximum gross weight for a given plane? I know I've come across articles that mention on a cool day you can go over the max. gross weight by a percentage, I think 20% was thrown out there but not sure. Then again, on a hot day you might not get any where near that. Is it determined by a standard temp? You dont´t know what is the reason for the maximum gross weight (unless you know the designers). It is dangerous to assume that take-off performance defines MTOW. MTOW is also the weight that has been used as the "most critical weight" during the whole design. It means that MTOW is there when you calculate the structural loads. There is a reason why it is called _maximum_ take-off weight. |
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![]() "Chris" wrote in message ... How do aircraft manufactures determine the maximum gross weight for a given plane? They pick a number and then verify that it is OK through a number of tests. There are a lot of requirements for aircraft to do "this or that" at various weights up to gross. For example, the Navion can be approved for various gross weights, some of it is climb horsepower related. If you have the stronger gear and a bigger engine you get a 100 lb increase, etc... Some of it is structural in cruise. Some of it involves sturctures for landing. etc... I know I've come across articles that mention on a cool day you can go over the max. gross weight by a percentage, I think 20% was thrown out there but not sure Burn whatever said that. If it were purely a performance issue, that would be true. But that's not necessarily the case. Note that in the above example, the two limiting factors on the Navion are performance AND the landing gear. A cold day might give you a bit more performance but it isn't going to make the landing gear any stronger. |
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