Ivan Kristensen
Well Known Member
I just finished joining the tail cone to the QB mid section fuselage. This process requires the floor panels being removed in the baggage compartment.
Van's web site states that they use Sherwin Williams corrosion inhibitor on their quick build kits so you can imagine my disappointment when I found that this had not been done in the area between the belly skin and the floor panels.
I looks to me like the whole thing was riveted together, assembled for shipping and then corrosion proofed last before crated up. In my mind this defeats the purpose on using a corrosion inhibitor as it ought to be applied before that parts are assembled so it is applied in areas where it is needed most, ie between rib flanges and the skin!
I wonder if anyone else have found this to be so and what they did about it.
Van's web site states that they use Sherwin Williams corrosion inhibitor on their quick build kits so you can imagine my disappointment when I found that this had not been done in the area between the belly skin and the floor panels.
I looks to me like the whole thing was riveted together, assembled for shipping and then corrosion proofed last before crated up. In my mind this defeats the purpose on using a corrosion inhibitor as it ought to be applied before that parts are assembled so it is applied in areas where it is needed most, ie between rib flanges and the skin!
I wonder if anyone else have found this to be so and what they did about it.