PT-6 engine installations are typically equipped with 3 engine controls
1) POWER LEVER..adjusts fuel flow rate to the engine..throttle equivalent in a piston airplane when moved behind the flight idle gate, it manually takes control of the prop governor to adjust blade angle for beta- range operations...RPM is then dependant on the position of the CONDITION LEVER
2) PROPELLOR LEVER..adjusts propellor rpm by setting the prop governor to maintain the requested propellor rpm...prop lever on piston it also simultaneously sets the n1 overspeed governor to a specific value slightly above (3% comes to mind) which allows the fuel control to remove fuel from the engine in event the prop governor fails.
3) CONDITION LEVER adjusts engine idle speed by resetting engine idle fuel flow. Once the power levers are advanced beyond the idle speed range of the CONDITION lever, the CONDITION LEVER will have no effect on engine parameters..it also usually has the idle-cutoff function for most pt-6 installations.
SO IN A PT-6 powered airplane so equipped with separate condition levers...the condition lever is connected to the fuel control unit..it controls N-1 rpm by regulating fuel flow.
TPE-331 (garrett, Honeywell Air research)
1) POWER lever...
a) Fuel control (manual fuel valve) for controlling engine power while operating in the flight range (forward of flight idle)
b) Prop pitch control..for selecting beta range operations (ground idle/reverse) aft of flight idle position
2) SPEED LEVER...is connected to the:
a) prop governor, for selecting a requested rpm in the flight range
b) underspeed fuel governor, for selecting a requested rpm when the engine is not being operated in the prop governing mode..I.E. beta range (on the ground only please!!)
TPE 331 engine installations are typically NOT equipped with a separate condition lever, as the "speed lever" performs this function
Hope this helps...many moons have passed since i taught these types.
