mototopo
Well Known Member
I'm going to rivet the center fuselage section and I have a doubt about the F-705 bulkhead assembly.
In detail, I noticed that the lower flange of the F-705A rear spar is square to its web. During a trial fit with the bottom skin, I noticed that this flange doesn't follow the slightly curved shape of the assembly (if looked from the side). Am I supposed to bend this flange up to let it follow the shape and be in-line with the cabin and baggage ribs or is to be left as is? (I'm sure I already know the answer.. just hope I don't need extra work... )
I didn't find any direction in the instructions or in the plans but, probably, this is just one of those "routine" tasks that have to be performed and, for this reason, omitted.
Thanks
In detail, I noticed that the lower flange of the F-705A rear spar is square to its web. During a trial fit with the bottom skin, I noticed that this flange doesn't follow the slightly curved shape of the assembly (if looked from the side). Am I supposed to bend this flange up to let it follow the shape and be in-line with the cabin and baggage ribs or is to be left as is? (I'm sure I already know the answer.. just hope I don't need extra work... )
I didn't find any direction in the instructions or in the plans but, probably, this is just one of those "routine" tasks that have to be performed and, for this reason, omitted.
Thanks