Fellow builders,
Now that I have mostly completed the costruction of the fuselage, I found the measurement of the gap between the spar carry through is about .020 LESS than the thickness of the wing spar. Van's instructions are to bevel the wing spar to ease insertion into the carry through. However my question is, will the carry through flex enough to allow the spar to be insearted?
Has anyone else been faces with this possable delima? Thanks in advance for your inputs.
Now that I have mostly completed the costruction of the fuselage, I found the measurement of the gap between the spar carry through is about .020 LESS than the thickness of the wing spar. Van's instructions are to bevel the wing spar to ease insertion into the carry through. However my question is, will the carry through flex enough to allow the spar to be insearted?
Has anyone else been faces with this possable delima? Thanks in advance for your inputs.