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Ron Lendon's Aircraft Mfg.
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Date:  4-3-2010
Number of Hours:  5.50
Manual Reference:  
Brief Description:  Near the end of the metal work

Riveted fuselage doubler on both sides using exsisting holes in the upper longeron, no need to weaken that.

Cut and installed the diagonal Z-angles on both sides.

Bolted and riveted right rear spar attach plate.

Tried to do the same on the left and have this view, stopped for the night and may have to remove the flap motor and limit switch to get the riveting done.
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