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1. ATA 77 Engine Indicating /How does the EIVMU communicate with the EEC?. The EIVMU communicates data to/from the EEC by an ARINC connection. There is no direct data connection between the EIVMU and the EEC. The EIVMU communicates data to/from the EEC by an Ethernet link.

2. ATA 77 Engine Indicating What engine data shows on the CRUISE page?. Fuel used, fuel flow and engine vibration indication. Fuel used indication only. Fuel used, oil quantity and engine vibration indication.

3. ATA 26 Fire Protection Where are the fire detectors?. Exhaust and Pylon, Zone 2 and 3. Zone one left and right, Zone 2 and 3. Pylon, Zone 1 left and right, Zone 2 and 3.

4. ATA 71 Power Plant General What is the correct fan cowl door latch opening and closing sequence?. Opening latch sequence L1, L2, L3 and L4; Closing latch sequence L2, L3, L4, L1. Opening latch sequence L4, L2, L1 and L3; Closing latch sequence L4, L3, L2, L1. Opening latch sequence L1, L2, L3 and L4; Closing latch sequence L4, L3, L2, L1.

5. ATA 78 Exhaust Which T/R actuators provide a Primary Lock?. middle actuators. lower actuators. upper and lower actuators.

6. ATA 78 Exhaust What ECAM message shows when the thrust reverser is deployed?. REV green in the middle of N1 dial. REV green in the middle of N1 dial and green MEMO on ECAM WD. REV white in the middle of N1 dial.

7. ATA 78 Exhaust Which is the second line of diference on the TRAS (Thrust Reverser Actuating System)?. A. EIVMU, EEC and IVU (Isolation VLV Unit. FCPC (Flight Control Primary Computer) and TLS (Tertiary Lock System). EEC and DCU (Directional Control Unit).

8. ATA 76 Engine Controls What supplies load feedback to the throttle control lever?. Artificial feel unit. TCU. Potentiometers.

9. ATA 76 Engine Controls What is the total number of N1 sensors on the engine?. 8. 4. 6.

10. ATA 73 Engine Fuel and Control When does the PMA supply power to the EEC?. N1 < 6%. > 6% N2. When OMS is in the interactive mode.

11. ATA 73 Engine Fuel and Control Which components use servo fuel to operate?. Thrust reverser primary/secondary locks. IP and HP bleed valves. VIGV/VSV.

12. ATA 73 Engine Fuel and Control How does the EEC control the HMU rate of fuel flow?. by using a Electro Hydraulic Servo Valve. by using a dual LVDT. by using solenoid valves.

13. ATA 72 Engine Performance How is are the EEC Engine Temperature values are trimmed from. DEP (Data entry plug) data. EIU (Engine Interface Unit) data. EEC (Engine Electronic Controller) data.

14. ATA 30 Ice and Rain Protection /What valve gives primary regulation for the engine anti-ice system?. PRSOV (Pressure Regulating and Shutoff Valve). PRV (Pressure Regulating Valve). Both at the same time.

15. ATA 30 Ice and Rain Protection What is the status of the solenoids when NAI P/B is set to ON?. Solenoid S1 energized, S2 and S3 de-energized. EEC energises only solenoid S3 of the PRSOV. All three solenoids S1-S3 are de-energised.

16. ATA 74 Ignition Which ECAM message is not related to ignition system monitoring?. ENG X IGN BOTH FAULT. ENG X IGN A+B FAULT. ENG X IGN A (B) FAULT.

17. ATA 79 Engine Oil Where is the Engine oil temperature sensor located?. upstream of the SAOHE (Surface Air Oil Heat Exchanger). in the combined oil scavenge pipe. downstream of the FOHE (Fuel Oil Heat Exchanger).

18. ATA 79 Engine Oil/How can you see the engine oil level?. By a sight-glass on the oil tank. By a dial gauge on the oil tank. By the dip-stick on the oil tank.

19. ATA 75 Air What air goes through the HPTCC valve?. LPC discharge air. 4th stage HPC air. Fan air.

20. ATA 75 Air Which stage supplies air to the Engine Section Stator Anti-Ice valve?. IP 6. HP 3. IP 8.

21. ATA 70 Construction, Arrangement and Operation /How is the Slat to T/R Cowl clearance maintained? by a cut out in the Slat. by a cut out in the Slat. by a Cowl Open Proximity Switch inhibiting the Slat Operation. by a Slat Clearance Panel on the Inboard Translating Sleeves.

22. ATA 70 Standard Practices Engine How is the preservation procedure determined?. A. Depending on the climatic conditions and duration. B. Depending on the maintenance status of the engine. C. Depending on the engine hours and cycles.

23. ATA 70 Standard Practices Engine What is the purpose of the engine nacelle?. Aerodynamic structure around the engine. Reduce noise of cold and hot air stream. Attaches the engine to the strut.

24. ATA 70 Standard Practices Engine What does the red line on the fan cowl show?. Hazard area aft of the line when engine operates. Hazard area forward of the line when engine operates. Hazard area when performing thrust reverser operation.

25. ATA 70 Standard Practices Engine Which direction do the engine shafts turn (AFT looking FWD). N1 Low pressure and N2 intermediate pressure shaft counter-clockwise, N3 high pressure shaft clockwise. N1, N2, N3 all turning counter-clockwise. N1 Low pressure and N3 high pressure shaft clockwise, N2 intermediate pressure shaft counter-clockwise.

26. ATA 80 Starting What could occur if the EIVMU (Engine Vibration Monitoring Unit) has a failure?. EEC de-powered. EEC will be powered for 15 minutes. EEC will be permanently powered.

27. ATA 28 Fuel How many fuel tanks does the A330-800 have?. 6. 5. 4.

28. ATA 36 Pneumatic Where does the Bleed Monitoring and Pressure Sensor output go?. BMC 2 channel A and B. DMC 1 and 2. BMC 1 and 2.

29. ATA 36 Pneumatic Which statement to the power-up test of the BMC (Bleed Monitoring Computer) is correct?. BMC 1 and 2 monitor ENG 1/2, APU and wing loops. BMC 1 monitors ENG 2 pylon and wing loops. BMC 2 monitors ENG 1, wing and APU loops.

30. ATA 36 Pneumatic/When energized, what pressure does the PRV (Pressure Regulation Valve) regulate downstream pressure to?. 60 PSI. 40 PSI. 50 PSI.

31. ATA 72 Engine (Turbine / Turboprop) What is the arrangement of the turbine section?. 1 high pressure turbine stages and 5 low pressure turbine stages. 2 stage high pressure turbines, 3 stage intermediate pressure turbine and 4 stage low pressure turbine. 1 stage high pressure turbines, 1 stage intermediate pressure turbine and 6 stage low pressure turbine.

32. ATA 73 FADEC What is the purpose of the Rotor Over-Speed protection system?. Monitors HPC and turbine shaft speed and gives a flight deck warning. Opens all IP and HP bleed valves when a stall or surge situation is detected. Fuel shutoff when an overspeed condition on LP or IP shaft is detected.