180jocky wrote:
You know I talked to Ben about that and this particular part is a cast aluminum channel, at least 1/4" thick. I don't know what we could fabricate it from that would be the correct dimensions.
Marty
That part is an extrusion,
not a casting. A casting would not be strong enough with that thin of a "wall thickness". Look at the main gear outboard bracket on a Cessna tricycle aircraft to see how much thicker a casting has to be than an extrusion.
The nominal distance between your front and rear gear box bulkheads (and doublers) is 6.875 inches. The inboard gear bracket is that distance in fore-aft length, outside to outside. The material is 2024-T4 or T-6. It is not standard T-3.
The shape of this inboard bracket, viewed from the side, is NOT a rectangle. It is a parallelogram 3 or 4 degrees "off-kilter". The hole pattern is identical front versus rear, but the hole patterns are OFFSET VERTICALLY by about .093"... the rear holes are higher than the front holes.
The main channel section can be machined out of a block of aluminum on a mill. Make sure there is a decent radius in the corner. If I am remembering, the "wall thickness" is nominal .1875 inches. You will have a fairly expensive pile of shavings on the ground. 2024 alloy cannot be 100% reliably welded like 6061 can, and the FAA engineers will be
very uneasy (and justifiably so) about welded 2024 unless you are Boeing. So you cannot weld it out of 3/16" plate.
I believe PPONK makes the inboard mounting angle. If they do not, your machine shop can make this angle out of 2024 bar stock. The fancy radius can be done by milling, or to be honest you can just leave the radius out and have a huge massive rectangular bar. The weight difference will be a few ounces. There is a lot of load on the fasteners holding this angle into the main channel, and it is a poor design because the angle does not connect directly to the mounting flanges. So all of your loads go through the ten bolts, and these holes should be a good tight reamed fit, I suggest NAS bolts instead of AN bolts.
Your biggest problem will be drilling the holes in the replacement part to match the holes in the aircraft. Sorry, that's going to be a bitch, and this is the one place where you need perfect holes with no slop.
But the answer to the core question, regarding making an owner produced replacement part, is that this channel is not rocket science and any machine shop can hog this out of a block of metal.