Ge-fam

In case of an emergency operation,how is the electrical network supplied. To be connected in parallel. The Emergency Generator (EMERGEN) supplies the A/C with electricalpower. To be supplied by APU gen or EXT PWRonly.

2. What is the function of the TR?. To convert the 28 VDC into 115 VAC. To convert the 115 VAC into 28 VDC. To convert the 115 VDC into 28 VAC.

3. The CIDS controls and monitors thecabin lights through the panel calle?. Forward attendant panel FAP. Flight attendant panel FAP. MCDU in the cockpit.

4. How are divided the wing tanks?. Outer cell and inner cell. Outer cell and ACT. Inner cell ,outer cell and ACT.

How many refuel valves has the fuel system. Three refuel valves,one for each tank. Only tank has refuel valves. Six refuel valves, two for each tank.

6. Where are the ENGINE fire detectors located. On the pylon, the fan and the core. On the core and the gearbox. On the fan and the turbine.

7. How is an APU fire on ground normallyextinguished?. From APU fire panel. Automatically. From external power panel.

8. What is the main function of the APU ?. To produce independent pneumatic andAir conditioning. To produce independent pneumaticand electrical power. To produce independent electrical powerand Hydraulic.

9. Which component controls andmonitors the APU?. The electronic control box (ECB). The electronic engine control (EEC). The IGV control unit.

What does the FADEC systemconsists of ?. One main frame computer for all engines. BññThe EEC and its peripherals, perengine. A single EEC and its peripherals, for bothengines.

11. What is the purpose of the PACK?. The packs are responsible for basictemperature regulation. To adjust the temperature in the three. To regulate hot air pressure to the cabins.

12. The pneumatic system operatespneumatically and is monitored by: One BMC for the two engines. 3 Bleed Monitoring Computers (BMC 1 & 2, 3) .There is one BMC for each engine bleed system and one of back up.. 2 Bleed Monitoring Computers (BMC 1 & 2) .There is one BMC for each engine bleed system.

13. How is used the PROBEIWINDOWHEAT P/BSW (normally in the AUTOposition) on ground?. May be used in arder to give reliableinformation to the air data systems. May be used to select the probeheating ON with the engines running. May be used to select the probe heatingON with the engines shut down.

14. Bleed air from the engines or theAPU is supplied to?. Each wing through a pressureregulating and shut off valve calledWing Anti-Ice (WAI) valve. Each wing through a pressure regulatingand shut off valve called Engine Anti-Ice (EAI)valve. Both wing through a pressure regulatingand shut off valve called Engine Anti-Ice (EAI)valve.

15. Which hydraulic systems arepressurized by an engine driven pump?. Green and yellow. Blue and green. Yellow and blue.