Engine Bolt Torque
My old 912 ULS powered aircraft used the rear four mounting point's - two top / two bottom. The bolts actually carried the rubber isolators connecting the engine to the frame/aircraft (soft connection). The bolts were all safety wired and fairly lightly torqued (cant remember the actually setting, probably around 30-40Nm).
My new kit aircraft uses the bottom/lower four mounting points - two front / two rear. The bolts are not safety wired and have conventional lock washers (plus a flat washer).
In this application the bolts secure a frame to the engine (hard connection). The frame itself "carries" the "rubber" isolators which then connect to the frame/aircraft.
My intention is to remove the bolts, drill safety wire holes, in the Allan key head & reinstall the bolts with safety wire to prevent unwanted rotation.
My questions are;
What would be an appropriate torque setting for the bolts? &
Should I use an anti gall/electrolysis paste? (steel bolts into aluminium alloy crankcase)