Randy Miller
Member
Being fairly new at actually posting information and questions on this website please bear with me if some of these questions seem foolish or maybe posted somewhere and I have not been able to find them.
In the process of analyzing and going over all of the work that was done on the quick build fuselage from the factory and a couple of small projects previously started I am a little less overwhelmed thanks for the encouragement. In the process here are a few things I have found and need clarification on.
1. The three rivets that go into the side skins on the very front of the top aft skin and rivet through the longeron, do not appear to have enough room to apply a bucking bar of any size due to the clearance of the F705G angle under the F757 gusset piece/bracket that had to be manufactured and is underneath of the gusset, that is fabricated for the tip up canopy. In the instructions it says to rivet the top rivets through and are unclear as to whether or not this angle bracket is riveted at this time or if the side rivets will clear once the top rivets are riveted down. I have a picture if it helps not sure how to post it.
2. Is it a fairly common practice for the rear baggage floor plates to be bolted down versus riveted down to allow access for additional wires as opposed to running all of the wires in the center tunnel next to the elevator push tube?
3. Likewise can you bolt the rear baggage side plates on the rear next to the front plates that are bolted, versus riveting as per the instructions to allow access to the steps if there is a problem with them in the future?
Sorry to be so wordy but trying to work out some of things I've noticed. Thanks,
Randy
In the process of analyzing and going over all of the work that was done on the quick build fuselage from the factory and a couple of small projects previously started I am a little less overwhelmed thanks for the encouragement. In the process here are a few things I have found and need clarification on.
1. The three rivets that go into the side skins on the very front of the top aft skin and rivet through the longeron, do not appear to have enough room to apply a bucking bar of any size due to the clearance of the F705G angle under the F757 gusset piece/bracket that had to be manufactured and is underneath of the gusset, that is fabricated for the tip up canopy. In the instructions it says to rivet the top rivets through and are unclear as to whether or not this angle bracket is riveted at this time or if the side rivets will clear once the top rivets are riveted down. I have a picture if it helps not sure how to post it.
2. Is it a fairly common practice for the rear baggage floor plates to be bolted down versus riveted down to allow access for additional wires as opposed to running all of the wires in the center tunnel next to the elevator push tube?
3. Likewise can you bolt the rear baggage side plates on the rear next to the front plates that are bolted, versus riveting as per the instructions to allow access to the steps if there is a problem with them in the future?
Sorry to be so wordy but trying to work out some of things I've noticed. Thanks,
Randy
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