Here are a couple of photos showing how a previous builder has "amended" the structure at rear of the aircraft
. The rear deck was not riveted in place along the longerons but held in place with 4x3/16bolts on each side, which in turn held a big chunk of angle which was bolted to the "ears" via the rear spar on the empennage.
http://i229.photobucket.com/albums/ee72/chrism741/SDC10365.jpg
Part of the rear top skin was cut away - presumably to give access for the bolts that hold the front of the empennage - and and additional former was riveted to the top skin just in front of the aperture. The bottom edge of the former was riveted to some angle which was again bolted to the longerons.
http://i229.photobucket.com/albums/ee72/chrism741/SDC10363.jpg
I am planning to remove the extra former and replace the top skin, and will fill the holes with a 6-32 rivet. The rear deck I will rivet in place as per plans but substitute some 6-32 rivets on each side again to fill the holes in the longerons. I'm just wondering if I should a strip of aluminum thing to the underside of the longerons or not? Any other thoughts?
Thanks
Chris
http://i229.photobucket.com/albums/ee72/chrism741/SDC10365.jpg
Part of the rear top skin was cut away - presumably to give access for the bolts that hold the front of the empennage - and and additional former was riveted to the top skin just in front of the aperture. The bottom edge of the former was riveted to some angle which was again bolted to the longerons.
http://i229.photobucket.com/albums/ee72/chrism741/SDC10363.jpg
I am planning to remove the extra former and replace the top skin, and will fill the holes with a 6-32 rivet. The rear deck I will rivet in place as per plans but substitute some 6-32 rivets on each side again to fill the holes in the longerons. I'm just wondering if I should a strip of aluminum thing to the underside of the longerons or not? Any other thoughts?
Thanks
Chris