PA-31T Systems
The PA-31, from what I remember: For the propeller, "A combination of nitrogen or air pressure, a spring, blade counter weights, and governor regulated oil pressure is utilized to change the pitch of the propeller blades. Nitrogen or air pressure is supplied from the precharged propeller chamber." As for the landing gear and brakes, it uses a hydraulic reservoir for the gear with engine driven pumps and a master cylinder for the brakes just like most general aviation aircraft. As for the fuel system, it consists of four fuel cells (40 gal outboard and 56 gal inboard) of which 187.3 is usable. There are two engine driven fuel pumps and two emergency fuel pumps. There are also a couple of annunciator lights that warn of an probable fuel flow interruption. There is also a cross feed system in place as well. I think that's all, if you have any other questions PM me. Also, if there is something here that is incorrect, someone jump in a correct me. As always consult the POH (ok, now i'm sounding like a lawyer). Have fun!