Book6RRT900Qs.txt

1. Which loads does the Aft Engine Mount Carry?
a. Vertical, Side and Torsion Loads
b. Vertical, Side and Thrust Loads
c. Vertical, Torsion and Thrust Loads

a. Vertical, Side and Torsion Loads

2. Where is the Oil Access Door Panel Located?
a. On the left-hand side of the Air Intake Cowl
b. On the right-hand Fan Cowl Door
c. On the right-hand side of the Air Intake Cowl

b. On the right-hand Fan Cowl Door

3. How are the Exhaust/Thrust Reverse Cowls operated to Opened and Closed?
a. Pneumatically
b. Hydraulically
c. Electrically

c. Electrically

I LOST CONNECTION HERE FOR A BIT!!!!

ENGINE

4. What is the make up of the IP Rotor (N2)?
a. An eight stage IP compressor driven by a signal stage IP turbine
b. A seven stage IP compressor driven by a two stage IP turbine
c. A six stage IP compressor driven by a single stage IP turbine

a. An eight stage IP compressor driven by a signal stage IP turbine

5. In which direction do the LP, IP and HP Rotors turn (As viewed from the rear)?
a. LP and IP Counter Clockwise, HP Clockwise
b. LP and IP Clockwise, HP Counter Clockwise
c. HP and IP Counter Clockwise, LP Clockwise

a. LP and IP Counter Clockwise, HP Clockwise

6. Which Station Number represents the exit from the HP Compressor?
a. STA 20
b. STA 30
c. STA 40

b. STA 30

FUEL SYSTEM

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

c. Three Pumps

8. At what pressure does the Full Flow relief valve open at, to relieve the HP pump outlet pressure back to the inlet?
a. 2250 psid
b. 2500 psid
c. 2750 psid

a. 2250 psid

At what pressure does the Full Flow relief valve open at, to relieve the HP pump outlet pressure back to the inlet

9. Which of the following will cause the Protection Torque Motor to operate?
a. EGT Overtemperature
b. HP Turbine Overtemperature
c. N1 or N2 Overspeed

c. N1 or N2 Overspeed

FADEC AND EIPM

10. Which engine mounted units make up the FADEC system?
a. The EEC and the EIPM
b. The EEC and the EMU
c. The EMU and EIPM

b. The EEC and the EMU

11. How is the EEC Channel B harnesses colour coded?
a. With Green Stripes
b. With Yellow Stripes
c. With Blue Stripes

a. With Green Stripes

12. With the Engine shut down, what power supply is used to power the EEC?
a. Two airframe 115 VAC supplies through the ElPM control logic function
b. A single airframe 115 VAC supply through the ElPM control logic function
c. Two airframe 28 VDC supplies through the EIPM control logic function

a. Two airframe 115 VAC supplies through the ElPM control logic function

ENGINE PROTECTION SYSTEMS

13. 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

14. For a Thrust Control Malfunction, which RU provides the signal to allow the EEC to shut down the engine?
a. The Flight Control Secondary Computer
b. The Flight Control Primary Computer
c. The Engine Monitoring Unit

b. The Flight Control Primary Computer

For a Thrust Control Malfunction, which RU provides the signal to allow the EEC to shut down the engine

15. What happens if the EEC detects a Turbine 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

16. Which secondary engine parameters are displayed on the System Display?
a. N1, N3 FF
b. N2, N3 and Fuel Used
c. N2, N3 and FF

c. N2, N3 and FF

17. Which Throttle Control Levers have reverse levers fitted?
a. Engines 2 and 3
b. Engines 1 and 4
c. All Engines

a. Engines 2 and 3

18. With one engine shut down, what is the throttle lever operating range for the A/THR system on the other three engines?
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

a. Between the Idle Stop and the MCT Detent

With one engine shut down, what is the throttle lever operating range for the A/THR system on the other three engines

IGNITION AND STARTING

19. Which ignition system is used for automatic engine starting on the ground?
a. Both ignition systems are used at the same time
b. Ignition unit "A" with "B" as backup
c. The EEC alternates between "A" and "B"

c. The EEC alternates between "A" and "B"

20. During a ground Automatic Start, when does the EEC introduce Fuel and Ignition?
a. At 25% N1Speed
b. At 25% N3 Speed
c. At 25% N2 Speed

b. At 25% N3 Speed

21. How is the Starter Air Valve controlled and operated?
a. Electrically Controlled, Pneumatically Operated
b. Pneumatically Controlled, Pneumatically Operated
c. Electrically Controlled, Electrically Operated

a. Electrically Controlled, Pneumatically Operated

ENGINE AIR SYSTEM

22. How many HP 3 Bleed valve are installed?
a. Two are installed
b. Three are installed
c. Four are installed

b. Three are installed

23. What is the position of the VIGV/VSVs when the engine is shut down?
a. OPEN
b. CLOSED
c. 50% OPEN

a. OPEN

24. What is the Spring-loaded position of the IP and HP Bleed Valves?
a. All OPEN
b. All CLOSED
c. IP OPEN, HP SHUT

a. All OPEN

ENGINE THRUST CONTROL AND ENGINE MASTER CONTROL

25. What is the Normal operating mode for the engine?
a. N1 Mode
b. N2 Mode
c. Turbofan Power Ratio

c. Turbofan Power Ratio

26. 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

27. 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

28. 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

29. How is power from the Power Drive Unit (DU) 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

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

b. 270 VDC

ENGINE OIL SYSTEM

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 nine scavenge pumps
c. A Single pressure pump and six scavenge pumps

b. A Single pressure pump and nine scavenge pumps

32. At what pressure does the Oil Scavenge Filter Differential Pressure Switch Operate at?
a. 33 psid
b. 23 psid
c. 13 psid

c. 13 psid

33. How many scavenge pumps are installed in the Oil Pump Unit?
a. Nine are installed
b. Seven are installed
c. Five are installed

a. Nine are installed

INTERFACES

ATA 24 - ELECTRICAL POWER

34. 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

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

b. Three

ATA 26 - FIRE PROTECTION

36. 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

37. 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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RR TRENT 900

ENGINE NACELLE