Good Morning,
I looked for a "Stupid questions from beginners" section, and this seemed to be the most appropriate place... so here goes:
I am getting ready to start building rib blank forms and flange forms and researching the different methods that others use. I notice that on a number of other aircraft the forward and rear flanges are built into the ribs. Is there any reason this couldn't be done on the Bearhawk?
I looked for a "Stupid questions from beginners" section, and this seemed to be the most appropriate place... so here goes:
I am getting ready to start building rib blank forms and flange forms and researching the different methods that others use. I notice that on a number of other aircraft the forward and rear flanges are built into the ribs. Is there any reason this couldn't be done on the Bearhawk?
- The biggest issue I can think of is that a number of ribs have varied lengths, which would mean making the biggest first, then cutting down the template, to the next... and so on.
- A second issue might be alignment at assembly, if the flange is built in, you won't have the "wiggle-room" to shift the rib fore/aft before riveting the rib to the spars.
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