Saville
Well Known Member
As I read and re-read the description on Van's QB page, a few questions arise. It says:
"The builder must drill and rivet the one remaining skin, install the control pushrods and blind rivet the composite wingtips to the outboard end. The ailerons and flaps are assembled and attach to the wing with a few bolts and a hingepin. "
Question 1:
What is meant by ailerons and flaps "assembled"? Meaning they are built for you? Or does it mean: "The builder than assembles the ailerons and flaps and attach them to the wing with a few bolts and hinge pin"?
It goes on to say:
"We estimate that a builder working two hours an evening and a long Saturday can complete a wing to flight status in a week."
Question 2:
Does this "flight status" include landing light(s) and wing tip lights? Or do they mean absolute minimum flight status?
Question 3:
If the latter, then I assume one has to cut the hole(s) for any leading edge landing light(s); cut holes in the wingtips for running lights; and thread the wiring for all that inside a QB wing which does not have the final skin panel on, yes?
Question 4:
How hard is it to thread the said wire through the QB wing and provide it with a solid anchoring throughout the run as well as chafing protection?
Thanks!
"The builder must drill and rivet the one remaining skin, install the control pushrods and blind rivet the composite wingtips to the outboard end. The ailerons and flaps are assembled and attach to the wing with a few bolts and a hingepin. "
Question 1:
What is meant by ailerons and flaps "assembled"? Meaning they are built for you? Or does it mean: "The builder than assembles the ailerons and flaps and attach them to the wing with a few bolts and hinge pin"?
It goes on to say:
"We estimate that a builder working two hours an evening and a long Saturday can complete a wing to flight status in a week."
Question 2:
Does this "flight status" include landing light(s) and wing tip lights? Or do they mean absolute minimum flight status?
Question 3:
If the latter, then I assume one has to cut the hole(s) for any leading edge landing light(s); cut holes in the wingtips for running lights; and thread the wiring for all that inside a QB wing which does not have the final skin panel on, yes?
Question 4:
How hard is it to thread the said wire through the QB wing and provide it with a solid anchoring throughout the run as well as chafing protection?
Thanks!