Illumination of a green alternate feather advisory light indicates what?
The auxiliary feathering pump is operating
When condition leavers are moved to Max propeller RPM is approximately what?
1200 NP
Is the engine driven hydraulic pump driven through the accessory gearbox?
No
Maximum takeoff power is limited to how many minutes?
Five minutes
For the power levers to move below the flight idle detent what must occur?
The flight idle gate release triggers must be raised
The high-pressure compressor is what?
Single stage centrifugal compressor
The Dash8 200 is fitted with which model engine?
PW123C
The power turbine consists of how many stages?
Two
After an engine failure, the power up trim signal is removed when?
The auto feather system is the activated
Normal take off power NTOP Dash8 300 engines each produce how much hp?
2140 SHP
Is the engine driven fuel pump mounted on the propeller reduction gearbox?
No
The accessory gearbox is driven by the what?
High-pressure compressor
To move the condition leavers from start and feather to fuel off you must do what?
Left the condition lever.
Automatic up trim power hp?
2380 hp
What does the accessory gearbox run?
The engine driven fuel pump the oil pump the DC starter/generator.
What’s driven by the propeller reduction gearbox?
A propeller control unit PCU,A PCU oil pump, a propeller over speed governor and an engine driven hydraulic pump.
What is Beta range?
Beta range is where the pilot is directly controlling the propeller blade angle.
Engine fuel Scheduling is controlled by what?
Mechanical fuel control unit MFC, and an electronic control unit ECU
In manual mode fuel control is relative to what?
Power lever angle PLA and condition lever angle CLA.
When the ECU mode is set on the ECU received input from what?
Potentiometer is sensing power lever angle and condition lever angle
During normal flight operations with the power levers forward of the flight beta range, propeller blade angle is governed by what?
Governed by the propeller control unit which regulates propeller speed in response to the condition lever setting
During normal flight in the forward flight range as the power levers are retarded, the propeller control unit does what?
The PCU reduces blade angle as it attempts to maintain the commanded propeller rpm, referred to as NP
In the Disc range, propeller blade angle varies between what?
+20° at flight Idle to +1.5° at Disc detent
What are the propeller blade angles in the reverse Beta range?
Blade angle changes from +1.5° at Disc to -11° at Max reverse stop