Gents,
I am working on my RV-7A fuselage and I keep running across serious assembly order issues. I am currently getting ready to fit my canopy frame but here is where the problem is.
First I must give you the current status of my fuselage.
1. Canopy Cabin Frame completed and fitted.
2. Instrument panel frame and forward fitted.
3. Aft Canopy Decks (F-721B) fitted but not riveted.
4. 3/16" angle (F-705G) under seat back frame (F-705) not riveted.
5. Aft top skin fitted but not riveted.
Here is the issue. If I want to start fitting the canopy frame, I need to rivet the Canopy Decks (F-721B) in position (I am not interested in temporally riveting these in place) because the clecos will prevent proper positioning of the Canopy Frame. But if I rivet the side rails in place then I do not have access to riveting the 3/16" angle (F-705G) on the seat back frame completely. If I rivet the 3/16" angle (F-705G) before the side rails, then I can?t rivet the 3 forward rivets on the aft top skin. I can?t rivet these before the 3/16" angle (F-705G) because I need to remove the skin so that I can fit the canopy.
If you follow the directions (checked with Van's on this) the order of assembly is to install the aft top skin and then rivet the 3/16" angle (F-705G)in position and then install the canopy roll frame. It may sound a bit confusing but it just doesn?t add up.
For those who are beyond this step, you probably know what I am talking about. The solution I have seen is to use pop rivets in the forward 3 holes in the top side skins the pass through the longeron. This makes some sense since it will allow a much more orderly assembly, not to mention riveting access.
However before I commit to this I want to get some input from others who have passed beyond this.
I know Dan C is lurking out there and he used the pop rivet solution.
Any help would be appreciated.
Paul M.
I am working on my RV-7A fuselage and I keep running across serious assembly order issues. I am currently getting ready to fit my canopy frame but here is where the problem is.
First I must give you the current status of my fuselage.
1. Canopy Cabin Frame completed and fitted.
2. Instrument panel frame and forward fitted.
3. Aft Canopy Decks (F-721B) fitted but not riveted.
4. 3/16" angle (F-705G) under seat back frame (F-705) not riveted.
5. Aft top skin fitted but not riveted.
Here is the issue. If I want to start fitting the canopy frame, I need to rivet the Canopy Decks (F-721B) in position (I am not interested in temporally riveting these in place) because the clecos will prevent proper positioning of the Canopy Frame. But if I rivet the side rails in place then I do not have access to riveting the 3/16" angle (F-705G) on the seat back frame completely. If I rivet the 3/16" angle (F-705G) before the side rails, then I can?t rivet the 3 forward rivets on the aft top skin. I can?t rivet these before the 3/16" angle (F-705G) because I need to remove the skin so that I can fit the canopy.
If you follow the directions (checked with Van's on this) the order of assembly is to install the aft top skin and then rivet the 3/16" angle (F-705G)in position and then install the canopy roll frame. It may sound a bit confusing but it just doesn?t add up.
For those who are beyond this step, you probably know what I am talking about. The solution I have seen is to use pop rivets in the forward 3 holes in the top side skins the pass through the longeron. This makes some sense since it will allow a much more orderly assembly, not to mention riveting access.
However before I commit to this I want to get some input from others who have passed beyond this.
I know Dan C is lurking out there and he used the pop rivet solution.
Any help would be appreciated.
Paul M.