POWER PLANT
MA60 is powered by two Pratt and Whitney Canada PW-127J engines driving two 247F-33.962m diameter 4 bladed propellers supplied by Hamilton Standard, USA. The engines are mounted on wings. The power plant has the following features:
·Light weight
·Three axles free turbine engine
·EEC control system supplies accurate control and monitoring
·β control system
·Low fuel consumption, 30% lower than normal technology engine
·Max. Take-of power of 2,750SHP
·Power from free turbine is transmitted to the propeller through a reduction gear box.
·propellers are constant speed, variable pitch (feathering to reverse)and auto synchronized One turbo generator GTCP36-150,made by Honeywell, USA, as APU
·Air conditioning on the ground to improve the cabin environment
·Ground electric power supply and starting engines

FUEL SYSTEM
·Two integral wing fuel tanks (two groups)and two bladder-type tanks with usable capacity of 5,200 liters. Single point pressure refueling offered
·Gravity reading is available
·Normal fuel supply by injection pumps
·Electrical pumps supply the fuel under the emergency condition
·Fuel can also be supplied by gravity now
·Electrically operated cross-feed valve ensures supply of fuel to a single engine from both tanks or to both engines from single tank
·Capacitance gauging show contents of each wing tank and total contents
·Rate of fuel indicator for each engine