2011 Cqt- Practice Test
Cancel
-
+
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.
- 26.Which is TRUE concerning the Accessory Gearbox section of the engine?
- A.
The Accessory Gearbox is located underneath the engine and is driven by the Low Pressure Compressor.
- B.
The Accessory Gearbox is located underneath the engine and is driven by the High Pressure Compressor.
- C.
The Accessory Gearbox is located on top of the engine and is driven by the High Pressure Compressor.
- D.
The Accessory Gearbox is located on top of the engine and is driven by the Low Pressure Compressor.
- 27.Which is FALSE concerning the major components of the Accessory Gearbox section of theengine?
- A.
Services provided by the Accessory Gearbox include the Oil Pump, High Pressure Fuel Pump, and the DC Starter Generator.
- B.
Services provided by the Accessory Gearbox include the Oil Pump, Low Pressure Fuel Pump, and the DC Starter Generator.
- C.
Services provided by the Accessory Gearbox include the Oil Pump, High Pressure Fuel Pump, and the AC Starter Generator.
- D.
Both B and C
- 28.Once armed, what triggers an Autofeather? (on the 100’s)
- A.
When one engine’s torque falls below 20% for three seconds while the other engine’s torque is greater than 50%.
- B.
When one engine’s torque falls below 22% for three seconds while the other engine’s torque is greater than 50%.
- C.
When one engine’s torque falls below 22% for three seconds while the other engine’s torque is greater than 60%.
- D.
When one engine’s torque falls below 20% for three seconds while the other engine’s torque is greater than 52%.
- 29.Once the Aux Feathering Pump is selected to Feather, how long will it run?
- A.
18 seconds
- B.
15 seconds
- C.
25 seconds
- D.
Until the prop feathers
- 30.Once the Aux Feathering Pump is selected to Unfeather, how long will it run?
- A.
18 seconds
- B.
15 seconds
- C.
25 seconds
- D.
Until the propeller Unfeathers
- 31.Is automatic Power Uptrim available if the Autofeather is disarmed?
- A.
Yes
- B.
No
- 32.Will the Alternate Feather/Unfeather system work if the engines are not running?
- A.
Yes, for one cycle
- B.
Yes, for two cycles
- C.
No
- D.
Yes, for three cycles
- 33.The props should be within how many rpm before activating the Synchrophase System?
- A.
30
- B.
40
- C.
10
- D.
20
- 34.The Synchrophase System uses the #1 prop as the Master and the #2 prop as the Slave?
- A.
True
- B.
False
- 35.What indication would you have if an ECU has failed on a PW120A?
- A.
Manual indication on the ECU Mode Switchlight and a power uptrim.
- B.
Manual indication on the ECU Mode Switchlight and a power loss.
- C.
Master Warning Light and Engine Manual Warning Light and a power loss.
- D.
Master Caution Light and Engine Manual Caution Light and a power loss.
- 36.Is Power Uptrim available if the Autofeather System is disarmed?
- A.
Yes
- B.
No
- 37.If there is an engine failure after takeoff with the Autofeather selected and armed, how much willthe good engine’s torque be uptrimmed?
- A.
Approximately 15%
- B.
Approximately 20%
- C.
Approximately 10%
- D.
Approximately 25%
- 38.If electrical power is removed from an engine instrument (i.e. Torque, ITT, etc.), what will thegauge indicate?
- A.
Pointer frozen, LCD blank
- B.
Pointer frozen, LCD frozen
- C.
Pointer to zero, LCD frozen
- D.
Pointer to zero, LCD blank
- 39.What do the Condition Levers control?
- A.
Manual prop feathering and unfeathering
- B.
Prop rpm in the foward thrust range
- C.
Fuel on/off control for engine start and shutdown
- D.
All of the above
- 40.What kind of protection is provided for High Pressure Compressor Rotor overspeed?
- A.
Seperate overspeed circuits in each PCU
- B.
Seperate overspeed circuits in each HMU
- C.
Seperate overspeed circuits in each ECU
- D.
Seperate overspeed circuits in each PSEU
- 41.What cockpit caution or advisory lights would be illuminated if an ECU fails or is not operating?
- A.
Master Warning Light, Engine Manual Warning Light
- B.
Master Warning Light, Engine Manual Caution Light
- C.
Master Caution Light, Engine Manual Warning Light
- D.
Master Caution Light, Engine Manual Caution Light
- 42.Why is the ECU Rating Selector placed at TOP for takeoff?
- A.
It gives the engines Takeoff Power
- B.
It provides Fail/Fixed mode
- C.
It insures only a small amount of rollback with a Torque Motor Failure
- D.
Both B and C
- 43.While on takeoff, a non-critical input of the ECU will cause an engine rollback.
- A.
True
- B.
False
- 44.What main functions do the Power Levers control?
- A.
Engine speed (power) in the forward thrust range
- B.
Propeller blade angle in Discing through Reverse range
- C.
Fuel on/off control for engine start and shutdown
- D.
Both a & b
- 45.During Quiet Taxi mode the ECU will maintain prop RPM at?
- A.
875
- B.
785
- C.
575
- D.
578
- 46.Power Uptrim on a PW120A will boost output power to?
- A.
1800 shp
- B.
2140 shp
- C.
2380 shp
- D.
2000 shp
- 47.Upon Nh overspeed, the ECU overspeed circuits revert the ECU to manual mode engineoperation.
- A.
True
- B.
False
- 48.At what Nh speed does the ECU activate overspeed protection?
- A.
100%
- B.
101%
- C.
102%
- D.
103%
- 49.Engine ignition is automatically activated when?
- A.
Engine starting
- B.
Single engine operation
- C.
Flaps extended
- D.
All of the above
- 50.In ECU Manual Mode you have Np underspeed and Nh overspeed protection.
- A.
True
- B.
False
- 51.Once an Nh overspeed has occured, can you select the ECU back on?
- A.
Yes
- B.
No
Back to top
