Ok I've probably left the OP thoroughly confused. My BC12D empty wieght cofg is within the range so I haven't had to think about landing cofg which is what this is all about.
Assuming your BC12D has the A65 you have two ranges to concider:
empty: 14.8 - 17.9
Loaded: 14.2 -...
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Well the Tcraft is not that simple.
If the empty c of g as weighed ends up toward the aft limit of the range, the gross c of g range is different... the aft loaded limit is further forward to ensure the aft limit is not exceeded during flight.
So, for the OP, as my memory...
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Huh?
the cofg moves aft as you burn fuel from the main tank. It is a mathematical certainty and has nothing to do with aerodynamics.
S
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I seem to recall that if your empty C of G is toward the aft limit, the gross C of G range is different. This is because the C of G always moves aft as you burn fuel so if the empty CofG is already aft, a restriction is needed on the loaded Cof G....
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Most likely single point of failure is the magnezium as Hank says. The belcrank is visable through the false spar/aileron cove....
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