Boeing 767 200-300

1. What services may provide the APU?. A. Hydraulic and oxygen supply. B. Pneumatic and electrical power. C. Fuel and hydraulic power.

2. Which are the fuel tanks of the 767?. A. Left main, right main, center tank. B. Left aux, right aux, trim tank C. Center tank only. C. Center tank only.

3. How are the engine fire extinguisher bottles discharged?. A. Automatically. B.Manually. Electrically only.

4. Which system detects a hot air leakage on the pneumatic ducting?. A. Fuel leak system. B. Wing and body duct leak system. C. Cabin smoke system.

5. Which message single loop operation generates?. A. Warning only. B. Status and maintenance. C. Cabin advisory only.

6. On which tank does the NGS work?. A. Left main tank. B. Right main tank. C. Center tank.

7. What is the function of waste tank point level sensor?. A. Measures water temperature. B.The two tank point level sensors send a signal to the logic module when a tank is full. C. Controls lavatory lights.

8. What is the useable capacity of main water tank?. A. 109 US gallons. B. 80 US gallons. C. 150 US gallons.

9. Where is the logic for the recirculation fan?. A.The ECS (fan) control cards are in the P50 card file and give control logic for the recirculation fans. B. P6 panel. C. Cargo compartment.

10. Which pressure is used to close TRIM AIR PRSOV?. A. Upstream pressure. C. Cabin pressure. Downstream pressure pushes on the close side of the pneumatic actuator to move the valve towards close.

11. When performing an equipment cooling manual test on the P61 panel, will the ground crew horn sound?. A. No. B. Yes, after 30 seconds holding the switch. C. Only during flight.

12. On which cooling pack mode will the pack be set to supply the most cooling?. A. AUTO. B. HIGH. C. STBY C.

13. Where can the flight deck zone trim modulating valve position be observed?. A. P5 and EICAS ECS/MSG. B. P61 only. C. FMC CDU.

14. What are the consequences if the zone duct overheat switch detects an overheat condition?. A. Pack shuts down. B. Related zone trim air air modulating valve closes. C. Ram air door opens.

15. When will the AUTO INOP light illuminate on the cabin altitude control panel?. A. When MAN is selected and both automatic controllers fail. B. During takeoff only. C. When outflow valve is open.

16. When the aircraft is unpowered what will be the outflow valve indicator needle position?. A. Full open. B. Goes off scale. C. Mid position.

17. In case of failure on one cabin pressure controller, will it automatically swap to the operative controller?. A. Yes it will change automatically. B. No. C. Only on ground.

18. How are the equipment cooling fans configured during smoke override mode?. A. Supply OFF / Exhaust ON. B. Supply ON / Exhaust OFF. C. Both OFF.

19. Are both primary and secondary heat exchangers the same?. A. Yes. B. No, the secondary has wider ram air section and stronger fins. C. Both OFF.

20. The service life of the lavatory waste compartment extinguisher bottle reservoir is: A. 2 years. B. 5 years. C. 10 years.

21. Under which condition can we approach a running engine?. A.Engine is at minimum idle, using the safety corridor and establishing communication with then flight deck. B. At any idle power. C. Only with beacon OFF.

22. How is the thrust reverser system actuated?. A. Both pneumatic. B. CF6 pneumatic / PW4000 hydraulic. C. Both hydraulic.

23. How is the mixture of air and fuel ignited on the combustor?. A. Spark plug wires. B. Two igniter plugs in the combustor. C. Compression only.

24. How is the CF6 engine controlled?. A.By the FADEC. B. Hydraulic governor. C. Manual cable system.

25. Which are the different engine start system air sources?. A. Battery, GPU, hydraulic. B. Ground air, APU air, engine air. C. Cabin air only.

26. How is the engine attached to the aircraft structure?. A. By side braces only. B. By forward and aft mounts. C. By pylon bolts only.

27. Which components convert aircraft electrical power to the voltage required to make a high energy spark at the igniter plug?. A. Generators. B. Ignition exciters. C. Transformers.

28. Which component controls the fuel flow through the FMU and protects the engine?. A. EEC. B. Fuel pump. Oil cooler.