Chris,
Mind if I ask a couple of questions regarding the future of this airframe, with an eye towards the hardware in question ? Since you seem to be having problems with the stuff on hand. I would ask, are you planning to fly this aircraft ? Or, are you planning a static restoration ? Either way, what you might want to do is seek the advice of a Aerospace Engineer. If the surrounding structure is alright, with no cracks or corrosion issues, then what you MAY be able to do is do a conversion of the hardware with known NAS, AN, or MS standard hardware.
For example, if the surrounding structure has enough clearance, and is free of damage such as cracks or corrosion, what you might be able to do is rework the fastener holse size to the next closest American Standard hardware size. Bearing in mind that in doing so, will require certain FAA documentation such as a 337 with supporting engineering to allow such a conversion.
Make use of reamers and core drills that are as close to original as possible to original, and seek advise in this from a Engineer that does this for a living. This person would have access to technical data to support the conversion, as well as provide that data for the Form 337 itself.
Now, I am saying all this with the idea that you have access to the current hardware that is used in the States from places such as Aircraft Spruce.
Just a suggestion....if you need some help I might be able to come up with some spec's regarding the hardware. But please bear in mind that with a recent cross country move, most of my stuff is in boxes. Always willing to help if I can.
Respectfully,
Paul
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