There are 3 levers on the control pedestal of a PT6 powered Beech King Air.
The one closest to the pilot – left hand side is the power lever – sometimes abused by calling it a “Throttle” by those oafs who don't know better.
The purpose of the power lever is two-fold – first it controls the fuel schedule by the interconnect from the engine cambox to the fuel control unit. Depending on the model of PT6 you can have different cambox operation – but in most cases the system will increase gas generator speed in the forward direction for increasing power to the maximum limit allowed and also will add gas generator speed when moved into the reverse position.
The second function of the power lever is to control the propeller blade angle (NOT SPEED) when the engine is operated in “Beta”. This is accomplished by the cambox operation through a push/pull cable (Teleflex) control that is linked to the beta valve on the forward face of the propeller governor and the connection for blade angle feedback that is through a carbon block in a beta ring attached to the propeller.
On the Beech King Air “Beta” range is from a degree or two above your prime blade angle – which is significantly ahead of the flight idle position. Beta in the case of the PT6a-42 in a King Air 200 for example starts at about +21 degrees of blade angle all the way to – 14 degrees in reverse. Flight idle is about 11 degrees.
BETA IS DEFINED AS THE RANGE OF ENGINE OPERATION WHERE THE POWER LEVER CONTROLS THE FUEL SCHEDULE AND THE BLADE ANGLE OF THE PROPELLER.
The second lever on the control pedestal is the “PROPELLER” control. It has 2 functions. When pull all the way aft it will feather the propeller. When pushed out of the feather detent it will be in the “LOW” speed or minimum governing setting – and when advanced increases the speed of the propeller to the “MAXIMUM” speed setting. When the power lever is moved from the flight idle gate the gas generator speed is increasing and the propeller blade angle is increasing as it is still in beta mode. Just above the primary blade angle check prop speed and torque for the day condition the system will transition from beta to constant speed mode – sometimes referred to as “ALPHA” mode. In this range the power lever will control only the gas generator speed and the propeller control lever will control the speed of the propeller through the constant speed governor.
The third lever on the control pedestal is the “FUEL CONDITON” lever. The original purpose of the fuel condition lever was to simply shut off or turn on the fuel to the engine. It is basically a HP (High Pressure) shutoff valve system that is operated by the flight crew to start and shut down the engine. It was modified on the Beech – as well as other aircraft – to include a low idle and a high idle position. The original reason for this was the small PT6 engines would bog down if you turned on the generator,bleed air, or the air conditioner compressor with the engine at idle. The extra loading at idle will cause an increase in fuel flow by the fuel control unit to keep the engine at the idle speed. Under this condition with only idle airflow through the engine - the Inter Turbine Temperature will increase to the point that it will cook the engine.
On some installations the flight crew must remember to advance the power lever to 68% or 70% minimum to obtain sufficient airflow through the engine so when loaded with the generator, bleed air, and/or the air conditioner compressor it had sufficient airflow to absorb the extra heat from the increase in fuel commanded by the fuel control unit.
So the fuel condition lever was modified/designed to “Bump” up – mechanically when advanced to the full forward position the linkage at the fuel control to give an easy way for the flight crew to obtain the correct gas generator speed.
The interactions of the 4 governors on the PT6a engine are complex and have overlapping functions to protect the engine and propeller.
The propeller lever has direct control of the propeller governor in the constant speed range.
The power lever has control of the governor section of the fuel control unit as well as a reset capability for the fuel topping governor.
The propeller hydraulic overspeed governor is set for a specific speed and does not have a cockpit control for it's operation. There is a test function to reset the speed down below that of the propeller governor so it's operation can be checked on the ground.