Brady wrote:
Does anyone know if the original 172 main gear will fit into the relocated cessna box section?
Sorry, not on my 1956 Cessna 172, and I doubt that any others would do it either. You (unfortunately) cannot take the tricycle gear boxes and move them forward. The distance between the "landing gear bulkheads" is different.
The "taildragger" gear bulkheads (front and rear door post bulkheads) are 7 inches apart, and with the various doublers in there the Cessna "gear box" fittings are 6 7/8 inches long between the mounting flanges. The "tricycle" gear bulkheads are, I believe, a bit further apart than that.
If you are interested, the reason for all this mayhem is that the (original taildragger) door post bulkheads are so close together that it makes everything hard to work on, and there is no room to put any sort of an adjustable shim or mechanism in there. The bolt heads are difficult to get to, busting your knuckles and creating previously non-existent curse words.
So in 1955 when Cessna engineers were told to develop a tricycle gear for the 170, they had the opportunity to redesign and improve the gear box system from a clean sheet, and to get away from the service difficulties that had become known in the years since the original 170/180 aircraft were in service.
THIS is why the tricycle gear box fittings and attachment methods look so much different than the original taildragger gear boxes. This is why the landing gear sticks through an oval shaped hole in the inboard gear box on the trike version... because of problems and cracks and PITA working with the previous (classic taildragger) design where there was very little "edge distance" for the hole in the end of the gear, and very little room for the end of the gear to sit in the I/B fitting. Cessna wanted to use cheap extrusions and a minimum of milling/drilling/lathe'ing operations.
If you can actually fabricate new, approved, acceptable fittings from flat stock using an old Bolen conversion, then find the documentation on the Bolen conversion and do it that way.
Also, pay attention to the aluminum angle reinforcement that runs spanwise across the entire top/front LG bulkhead. It needs to have a reinforcement there, to transfer and "balance" loads from one side of the airplane to the other. The 172 does not have this piece because it doesn't need the load path there for the trike gear. And let's all give Cessna a big hand, they saved fifty cents by not installing this piece in the 172 !!! Now try and install this piece into an existing (completed) aircraft without disassembling the entire forward fuselage, the control "tunnel" removing the skins, etc..
But wait, Cessna used a custom extrusion to get a "closed" angle of 70 degrees instead of 90 degrees... the angle of the forward floorboards slanting downward demands this. Now, go to your local metal supply house and find a 70 degree closed angle in 2024-T3. Don't worry, I'll be there waiting with the tranquilizer gun and "straight jacket" after you've tried six or seven times
