2011 Cqt- Practice Test
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Version 1. This test has 51 questions from the CQT drawn at random for you to practice.
- 1.With the accumulator charged to 3000 psi, how many parking brake applications do you have?
- A.
Approximately three braking applications
- B.
Approximately four braking applications
- C.
One brake application
- D.
Two brake applications
- 2.Is the anti-skid available when using the emergency brake?
- A.
Yes
- B.
No
- 3.The tiller provides ___ degrees of nosewheel steering either side of center.
- A.
40
- B.
50
- C.
60
- D.
70
- 4.Where does the normal braking system receive its hydraulic power from?
- A.
#1 Hydraulic System
- B.
#2 Hydraulic System
- C.
PTU
- D.
#3 Hydraulic System
- 5.The rudder pedals provide approximately ___ degrees of nosewheel steering either side of center with the nosewheel steering turned on.
- A.
3 degrees
- B.
7 degrees
- C.
10 degrees
- D.
12 degrees
- 6.Must the gear lever lock release button be held down when making a gear selection?
- A.
Yes
- B.
No
- 7.A LDG GEAR INOP caution light indicates a failure associated with what valve?
- A.
PSEU
- B.
Solenoid Sequence Valve
- C.
Landing Gear Valve
- D.
PTU Valve
- 8.The solenoid sequence valve gets its signal to open or close the gear doors from the PSEU.
- A.
True
- B.
False
- 9.How long do the anti-skid lights stay on when testing is performed on the ground?
- A.
3 seconds
- B.
6 seconds
- C.
10 seconds
- D.
As long as you hold the switch
- 10.Which component monitors the position of the uplocks, downlocks, and gear door positions?
- A.
PTU
- B.
Solenoid Sequence Valve
- C.
PSEU
- D.
WOW Sensor
- 11.Where does the emergency parking brake receive its hydraulic pressure from?
- A.
#1 Hydraulic system
- B.
#2 Hydraulic system
- C.
PTU
- D.
#1 Standby Pump
- 12.When will the landing gear warning horn sound?
- A.
Autofeather not armed, flaps >15, power levers not at take-off, and the gear not down and locked
- B.
Airspeed < 130 kts, gear not down and locked, autofeather not armed
- C.
Airspeed < 130 kts, power levers near flight idle, gear not down and locked
- D.
A & C
- 13.When can the landing gear warning horn be muted?
- A.
Autofeather not armed, flaps >15, power levers not at take-off, and the gear not down and locked
- B.
Airspeed < 130 kts, gear not down and locked, autofeather not armed
- C.
Airspeed < 130 kts, power levers near flight idle, gear not down and locked
- D.
Airspeed < 130 kts, one power lever near flight idle, gear not down and locked
- 14.With anti-skid on and operating, at what point are the brakes available after touchdown?
- A.
2.5 seconds after touchdown
- B.
35 kts wheel spin up
- C.
Immediately
- D.
A & B
- 15.The LDG GEAR INOP caution light requires an alternated gear extension?
- A.
True
- B.
False
- 16.During an alternate gear extension, if the landing gear fails to free-fall to the down and lockedposition the main and nose gear can be manually pumped down.
- A.
True
- B.
False
- 17.How many degrees will the nose wheel free-caster left or right of center?
- A.
70
- B.
80
- C.
90
- D.
120
- 18.Which gear doors remain open after a normal extension?
- A.
Forward nose gear doors & aft main gear doors
- B.
Forward nose gear doors & forward main gear doors
- C.
Aft nose gear doors & forward main gear doors
- D.
Aft nose gear doors & aft forward gear doors
- 19.For the propeller synchrophase system, which prop is the master and which is the slave?
- A.
#2 Master - #1 Slave
- B.
Both are Slave to the NWS ECU
- C.
It depends on which is started first
- D.
#1 Master - #2 Slave
- 20.At what prop RPM will the over-speed governor PNEUMATICALLY control the prop?
- A.
1236
- B.
1336
- C.
1308
- D.
1208
- 21.At what prop RPM will the over-speed governor HYDRAULICALLY control the prop?
- A.
1236
- B.
1336
- C.
1308
- D.
1208
- 22.Max prop rpm in reverse is?
- A.
1350
- B.
1200
- C.
1212
- D.
1250
- 23.What are the major components of the Propeller Reduction Gearbox section of the PW-120Aengine?
- A.
Overspeed Governor, PCL, Main Hydraulic Pump, AC Generator
- B.
Overspeed Governor, PCU, Main Hydraulic Pump, AC Generator
- C.
Overspeed Governor, PCU, Standby Hydraulic Pump, AC Generator
- D.
Overspeed Governor, PCU, Main Hydraulic Pump, DC Generator
- 24.Which of the following describe the Beta Backup System?
- A.
Provides protection against the prop entering Ground Beta range unintentionally due to a PCU malfunction.
- B.
Provides protection against the prop entering Flight Beta range unintentionally due to a PCU malfunction.
- C.
Provides protection against the prop entering an overspeed condition due to a PCU malfunction.
- D.
Provides protection against the prop entering an overspeed condition due to a ECU malfunction.
- 25.When do the prop Ground Range lights illuminate?
- A.
Whenever the power levers are selected below the flight idle gate and the blade angle decreases to 15.5 degrees or less.
- B.
Whenever the power levers are selected below the flight idle gate and the blade angle decreases to 16.5 degrees or less.
- C.
Whenever the power levers are selected below the flight idle gate and the blade angle decreases to 17.5 degrees or less.
- D.
Whenever the power levers are selected below the flight idle gate and the blade angle decreases to 18.5 degrees or less.
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