Version 1. This test has 51 questions from the CQT drawn at random for you to practice.
Approximately three braking applications
Approximately four braking applications
One brake application
Two brake applications
Yes
No
40
50
60
70
#1 Hydraulic System
#2 Hydraulic System
PTU
#3 Hydraulic System
3 degrees
7 degrees
10 degrees
12 degrees
Yes
No
PSEU
Solenoid Sequence Valve
Landing Gear Valve
PTU Valve
True
False
3 seconds
6 seconds
10 seconds
As long as you hold the switch
PTU
Solenoid Sequence Valve
PSEU
WOW Sensor
#1 Hydraulic system
#2 Hydraulic system
PTU
#1 Standby Pump
Autofeather not armed, flaps >15, power levers not at take-off, and the gear not down and locked
Airspeed < 130 kts, gear not down and locked, autofeather not armed
Airspeed < 130 kts, power levers near flight idle, gear not down and locked
A & C
Autofeather not armed, flaps >15, power levers not at take-off, and the gear not down and locked
Airspeed < 130 kts, gear not down and locked, autofeather not armed
Airspeed < 130 kts, power levers near flight idle, gear not down and locked
Airspeed < 130 kts, one power lever near flight idle, gear not down and locked
2.5 seconds after touchdown
35 kts wheel spin up
Immediately
A & B
True
False
True
False
70
80
90
120
Forward nose gear doors & aft main gear doors
Forward nose gear doors & forward main gear doors
Aft nose gear doors & forward main gear doors
Aft nose gear doors & aft forward gear doors
#2 Master - #1 Slave
Both are Slave to the NWS ECU
It depends on which is started first
#1 Master - #2 Slave
1236
1336
1308
1208
1236
1336
1308
1208
1350
1200
1212
1250
Overspeed Governor, PCL, Main Hydraulic Pump, AC Generator
Overspeed Governor, PCU, Main Hydraulic Pump, AC Generator
Overspeed Governor, PCU, Standby Hydraulic Pump, AC Generator
Overspeed Governor, PCU, Main Hydraulic Pump, DC Generator
Provides protection against the prop entering Ground Beta range unintentionally due to a PCU malfunction.
Provides protection against the prop entering Flight Beta range unintentionally due to a PCU malfunction.
Provides protection against the prop entering an overspeed condition due to a PCU malfunction.
Provides protection against the prop entering an overspeed condition due to a ECU malfunction.
Whenever the power levers are selected below the flight idle gate and the blade angle decreases to 15.5 degrees or less.
Whenever the power levers are selected below the flight idle gate and the blade angle decreases to 16.5 degrees or less.
Whenever the power levers are selected below the flight idle gate and the blade angle decreases to 17.5 degrees or less.
Whenever the power levers are selected below the flight idle gate and the blade angle decreases to 18.5 degrees or less.