Book6GP7200Qs.txt

1. ENGINE NACELLE Which loads do the Strut Mounts Transmit?
a. The Engine Thrust Loads
b. The Engine Vertical Loads
c. The Engine Torsion Loads

a. The Engine Thrust Loads

2. Where is the Fan Cowl Up Down Switches Located?
a. On the left-hand and right-land side of the Air Intake Cowl
b. On the left-hand and right-hand Fan Cowl Doors
c. On the left-hand and right-hand side of the Thrust Reverser Cowls

a. On the left-hand and right-land side of the Air Intake Cowl

3. Which of the engines are fitted with Thrust Reverse Cowls?
a. All four engines
b. Engines 1 and 4 only
c. Engines 2 and 3 only

c. Engines 2 and 3 only

ENGINE

4. What is the makeup of the LP Rotor (N1)?
a. The Fan, and a Four stage compressor, drive by a five stage LP Turbine
b. The Fan, and a Five stage compressor, drive by a six stage LP Turbine
c. The Fan, and a Six stage compressor, drive by a seven stage LP Turbine

b. The Fan, and a Five stage compressor, drive by a six stage LP Turbine

5. Which bearings support the HP Rotor?
a. No.3 Roller Bearing, No.4 Ball Bearing and No.5 Roller Bearing
b. No.3 Roller Bearing, No.4 Ball Bearing and No.4 Roller Bearing
c. No.3 Roller Bearing, No.3 Ball Bearing and No.4 Roller Bearing

c. No.3 Roller Bearing, No.3 Ball Bearing and No.4 Roller Bearing

6. Which Station Number represents the Inlet to the HP Compressor?
a. STA2.0
b. STA2.5
c. STA 3.0

b. STA2.5

FUEL SYSTEM

7. How many fuel pumps are housed in the Fuel Pump Assembly?
a. One Pump
b. Two Pumps
c. Three Pumps

b. Two Pumps

8. Where is the fuel sent to after it leaves the Fuel Pump Gear Stage?
a. It is sent to the Fuel Flow Transmitter
b. It is sent to the Fuel Metering Valve
c. It is sent to the Main Fuel Filter Assembly

c. It is sent to the Main Fuel Filter Assembly

9. Which fuel operated servo valves have a BIASED servo fuel supply?
a. HP ACC, LP ACC, VSV SERVO
b. HP ACC, LP ACC, START BLEED VALVE
c. HP ACC, LP ACC, 2.5 BLEED SERVO

b. HP ACC, LP ACC, START BLEED VALVE

FADEC AND EIPM

10. How can the EEC be powered?
a. By the PMA or from the aircraft via the EMU
b. By the EMU of from the aircraft via the EIPM
c. By the PMA or from the aircraft via the EIPM

c. By the PMA or from the aircraft via the EIPM

11. How is the N1 (LP Shaft) Speed measured?
a. By the N1 Sensor attached to the front of the accessory gearbox
b. By the N1 Sensor attached to the fan hub frame at the 1 O'clock position
c. By the N1 Sensor attached to the fan hub frame at the 7 O'clock position

c. By the N1 Sensor attached to the fan hub frame at the 7 O'clock position

12. Which of the servo fuel operated valve/actuators are NOT supplied with BIASED Fuel?
a. VSV Servo and HPT ACC
b. 2.5 Bleed and HPT ACC
c. 2.5 Bleed and VSV Servo

c. 2.5 Bleed and VSV Servo

ENGINE PROTECTION SYSTEMS

13. What is the monitored parameter for the Thrust Control Malfunction system?
a. N2 Speed
b. N1 Speed
c. EGT

b. N1 Speed

14. What happens if the EEC detects an N1 or N2 Overspeed?
a. The EEC will set the engine to Idle
b. The EEC will shut down the engine
c. The EEC will limit the N1 and N2 Speeds

b. The EEC will shut down the engine

ENGINE INDICATING

15. On which ECAM display can the Total Fuel Used indication be found?
a. The SD CRUISE Page
b. The EWD
c. The SD ENGINE PAGE

a. The SD CRUISE Page

16. Which Throttle Control Levers have the instinctive cut-out button fitted?
a. Engines 2 and 3
b. Engines 1 and 4
c. All Engines

b. Engines 1 and 4

17. What is the NORMAL throttle lever operating range for the A/THR system?
a. Between the Idle Stop and the MCT Detent
b. Between the Idle Stop and the CL Detent
c. Between the Idle Stop and the TOGA Detent

b. Between the Idle Stop and the CL Detent

IGNITION AND STARTING

18. What type of starter is used on the GP 7200?
a. An Electric Starter
b. A Hydraulic Starter
c. A Pneumatic Starter

c. A Pneumatic Starter

19. During a ground automatic start, what does the EEC do if it detects a No Light-Up condition?
a. It will abort the start, then do a dry crank, before aborting the start sequence
b. It will continue the start by introducing the second ignition system
c. It will abort the start, then do a dry crank, before attempting a new start

c. It will abort the start, then do a dry crank, before attempting a new start

20. During a Manual Start, when does the EEC Close the Starter Air Valve?
a. When N2 reaches 58.4%
b. When N2 reaches 68.4%
c. When N2 reaches 48.4%

a. When N2 reaches 58.4%

ENGINE AIR SYSTEM

21. Which air is used for the HPTACC and LPTACC Systems?
a. HPC 2 Air
b. HPC 3 AIR
c. Fan Air

c. Fan Air

22. How are the VIGV/VSV actuators controlled and operated?
a. Electrically controlled, fuel operated
b. Electrically controlled, electrically operated
c. Electrically controlled, pneumatically operated

a. Electrically controlled, fuel operated

23. What is the position of the 2.5 Bleed Valve during reverse thrust operation?
a. PARTIALLY OPEN
b. FULLY CLOSED
c. FULLY OPEN

c. FULLY OPEN

ENGINE THRUST CONTROL AND ENGINE MASTER CONTROL

24. What is the result of an Alpha Floor Detection?
a. A/THR is automatically engaged active and commands the MCT thrust mode
b. A/THR is automatically engaged active and commands the CL thrust mode
c. A/THR is automatically engaged active and commands the TOGA thrust mode

c. A/THR is automatically engaged active and commands the TOGA thrust mode

25. After activation of the N1 Degraded mode, when can this condition be reset?
a. If the Air Data Inputs are restored
b. Only after an EEC Replacement
c. Only after MASTER lever reset

c. Only after MASTER lever reset

26. What is the Auto Thrust Mode during Take-Off?
a. Engaged but not active
b. Engaged and active
c. Not engaged

a. Engaged but not active

ENGINE THRUST REVERSE

27. Which of the Translating Cowl actuators are fitted with the Primary Locks?
a. The Lower Actuators
b. The Upper Actuators
c. The Centre Actuators

b. The Upper Actuators

28. What power supply is used to release the Power Drive Unit Brake?
a. 115 VAC
b. 270 VDC
c. 28 VDC

b. 270 VDC

29. How is power from the Power Drive Unit (PDU) transferred to the Translating Cowls?
a. From the PDU to the Lower Actuator
b. From the PDU to the Centre Actuator
c. From the PDU to the Upper Actuator

b. From the PDU to the Centre Actuator

ENGINE OIL SYSTEM

30. What is the maximum pressure inside the oil tank?
a. 10 PSI
b. 15 Psi
c. 20 PSI

a. 10 PSI

31. What is the make up of the Oil Pump Unit?
a. A Dual pressure pump and nine scavenge pumps
b. A Single pressure pump and five scavenge pumps
c. A Single pressure pump and six scavenge pumps

b. A Single pressure pump and five scavenge pumps

32. Which engine bearing(s) is (are) located in B SUMP?
a. The No.4 Bearing
b. The No.3 Bearing
c. The No.2 Bearing

a. The No.4 Bearing

INTERFACES

ATA 24 - ELECTRICAL POWER

33. What is the rated output of the VFGs?
a. 250 KVA, 115 VAC, 3 Phase
b. 200 KVA, 115 VAC, 3 Phase
c. 150 KVA. 115 VAC 3 Phase

c. 150 KVA. 115 VAC 3 Phase

ATA 36 - PNEUMATICS

34. How many Crossbleed valves are fitted?
a. Two
b. Three
c. Four

b. Three

ATA 26 - FIRE PROTECTION

35. Which of the following occurs when an ENG/FIRE P/BSW is pushed?
a. The VFG is de-energised, The HP Valve closes and the Engine Fuel LP Valve closes
b. The VFG is de-energised, The FCV closes and the Engine Fuel LP Valve closes
c. The VFG is de-energised, The FCV closes and the Engine Fuel HP Valve closes

b. The VFG is de-energised, The FCV closes and the Engine Fuel LP Valve closes

ATA 30 - ICE AND RAIN

36. Regarding the Engine Anti-Ice, what are the functions of the Anti-Ice Control Unit 2 Channel B?
a. Monitoring of Engine 1 and control of Engine 3 Anti-Ice
b. Monitoring of Engine 2 and control of Engine 3 Anti-Ice
c. Monitoring of Engine 4 and control of Engine 2 Anti-Ice

a. Monitoring of Engine 1 and control of Engine 3 Anti-Ice

Regarding the Engine Anti-Ice, what are the functions of the Anti-Ice Control Unit 2 Channel B

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EA GP7200