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1- With respect to the fuel transfer operation. It is possible to do it only in flight. It is possible to do it only on ground. It can be done in flight or on ground.

2- What happens if the Lavatory & Galley Ventilation Fan is lost?. The zone controller will maintain a duct temperature of 15C. What happens if the Lavatory & Galley Ventilation Fan is lost. The primary function of the Pack temperature controller is lost.

3- The engine fuel LP valve closes when: The engine fire detection system senses an engine fire. The fuel booster pump presure decreases. The engine is shut down or the Eng Fire pushbutton is released out.

4- The computers used in the Air Conditioning System are: Two Zone Controller and one Pack Controller. One Zone Controller and one Pack Controller. Two Pack Controller and one Zone Controller.

5- Which Slats are protected by the wing anti ice system?. All the SLATS. Only the SLATS 1 and 2. Only the SLATS 3-4-5.

6- The air used for the Nitrogen Generation System is taken from: The aircraft pneumatic system. Air taken from the airflow that it is passing through the main/primary heat exchangers. Ambient air taken directly through a dedicated ram air inlet.

7- The Fuel Quantity Indicating System comprises: Two FQICs and two FLSCUs. One FQIC and two FLSCUs. Two FQICs and one FLSCUs.

8- If the pack controller fails (total lost), the pack outlet temperature is controlled by: The Pack Valve. The Pack Anti-Ice Valve. The ByPass Valve.

9- Where can you see the Wing anti-ice valves position indication?. In the COND page of ECAM. They are not shown. In the BLEED page of ECAM.

10- How does the pack controller avoid overtemperature in the compressor discharge?. By modulating the Hot Trim PRV. By opening the ram air inlet door. By modulating the Flow Control Valve.

11- The purpose of the fuel sequence valves is : To reduce pressure on the APU boost pump. To reduce output pressure of the wing boost pumps. To reduce output pressure of the center boost pumps.

12- In regards to the air conditioning packs indications, What are the components shown in the ECAM Bleed page?. By-Pass Valve and Flow Control Valve. Flow Control Valve and Anti-ice Valve. Anti-ice Valve and Trim Air Valves.

13- What happens if the EIU and/or PHC C/B are pulled?. Nothing. The related probes and static ports will be de-energized. The related probes and static ports will be heated.

14- The ice on the wing leading edge slats is prevented by: Opening the two electrically operated valves. Hot air coming from the respective pack valve. Hot air comming from the pneumatic system.

15- Pneumatic leak in the engine pylons. Is detected by an ambient sensor. Is detected by a single loop. Is detected by a double loop.

16- In relation to the Cross Bleed valve and its operation: It has two electrical motors, one for manual and other for auto operation. It is a valve that operates pneumatically. It has one electrical motor, for auto and manual operation.

17- What is the purpose of the CT sensor in the pneumatic system?. To send a T signal to BMC, to control the FAV and maintain the Pneumatic system T within limits. To send a pneumatic signal to control the Pressure Regulating Valve (PRV). To control pneumatically the Fan Air Valve, to maintain pneumatic T within limits.

18- The normal maximum Cabin Altitude of the system is: Up to 15.000 ft. or less. About 6.000 ft. 8.000 ft.

19- The MODE SEL pushbutton controls..(Fuel system). Center and wing tanks pumps. Wing tank pumps only. Center tanks pumps only.

20- When does the FAULT light in the CABIN PRESS panel come ON?. When both Cabin Pressure Controllers are defective. When the Mode Selector P/B switch is in MANUAL position. When either cabin pressure controller 1 or 2 is defective.

21- When the center tank is empty (130 kg), in AUTO MODE, the center tank pumps. Must be manually switched off. Stop automatically and wing tank pumps start running. Stop automatically after 5 minutes.

22- The pneumatic system is monitored by: The EC. Two BMCs. Both EECs (ECUs).

23- In flight, the bleed air can be obtained from: The Engines or APU. The APU only. Engines only.

24- What is the purpose of the CTS sensor in the Pneumatic system?. To send a electric signal to the Over Pressure Valve. To send a pneumatic signal to regulate or shut-off the Pressure Regulating Valve. To keep bleed temperature within limits when 7 stage is open.