Re: strut replacement documentation
Hi Gary,
No, I don't think its that.
Those dimensions changing do not constitute a major difference.
There is some other reason that is yet hidden from us and I suspect that because of two STC's that I have on my Aeronca.
One of the STC's is for the addition of two inspection covers in the leading edge that allow inspection of the top of the front spar of each wing. Simple little inspection covers.
Another is for the replacement of the spar. The difference between the STC'ed spar and the OEM spar is that the plywood plates on the STC spar are not rectangles like the OEM spar. AC43.13-1B tells us not to make rectangular plates. This is not a major issue either.
Thirdly (I don't have this one but I am aware of it) there is an STC for Aeroncas to use#4 screws to hold the ribs on instead of nails. Is that a major issue? I don't think so.
My supposition is that there is some commercial/economic reason for using the STC.
For example; one can sell the simple inspection covers or screw kits to others if there is an STC. I don't object to that it is very convenient however without the STC it is not legally possible. Not sure how that works for spars or struts.
One thing additionally is true about the strut scenario though. Once you install the struts on the plane with the STC those struts are married to that plane and cannot be moved to another plane as a used serviceable part. STCs go with a particular airplane by serial number.
Dave R
Originally posted by PA1195
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No, I don't think its that.
Those dimensions changing do not constitute a major difference.
There is some other reason that is yet hidden from us and I suspect that because of two STC's that I have on my Aeronca.
One of the STC's is for the addition of two inspection covers in the leading edge that allow inspection of the top of the front spar of each wing. Simple little inspection covers.
Another is for the replacement of the spar. The difference between the STC'ed spar and the OEM spar is that the plywood plates on the STC spar are not rectangles like the OEM spar. AC43.13-1B tells us not to make rectangular plates. This is not a major issue either.
Thirdly (I don't have this one but I am aware of it) there is an STC for Aeroncas to use#4 screws to hold the ribs on instead of nails. Is that a major issue? I don't think so.
My supposition is that there is some commercial/economic reason for using the STC.
For example; one can sell the simple inspection covers or screw kits to others if there is an STC. I don't object to that it is very convenient however without the STC it is not legally possible. Not sure how that works for spars or struts.
One thing additionally is true about the strut scenario though. Once you install the struts on the plane with the STC those struts are married to that plane and cannot be moved to another plane as a used serviceable part. STCs go with a particular airplane by serial number.
Dave R
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