How Do You Calculate Lift Force on a Banked Airplane?

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Visual1Up
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Need some suggestions...

I have a banked airplane at theta degrees, with a radius, and velocity. What is the formula for finding lift force. Fc = Fn sin theta I believe, but that's the only formula I am aware of. Thanks!,
-Mike
 
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Visual1Up said:
Need some suggestions...

I have a banked airplane at theta degrees, with a radius, and velocity. What is the formula for finding lift force. Fc = Fn sin theta I believe, but that's the only formula I am aware of. Thanks!,
-Mike
The plane has centripetal acceleration in the horizontal direction. The pilot keeps the plane banked at just the right angle to keep the plane from slipping and maintain a steady altitude. Which forces, and which components of those forces, are keeping the plane from moving up or down?