A320

What is the function of the TR (Transformer Rectifier)?. To convert the 115 VAC into 28VDC. To convert the 220 VDC into 28VAC. To convert the 28 VDC into 115VAC.

What is the main difference between the A319/320/321 and the A318 vertical stabilizers?. The new rib 12N is on the STA5970. There is no difference thevertical stabilizer is the same of the A318. The new rib 14N is en the STA5970.

What do the visual attention getters consist of?. A red an amber light below the E/WD display. A green MASTER Warning and an amber MASTER Caution in front of each. A red MASTER Warning and amber MASTER Caution in front of each pilot.

The sliding windows and the side fixed windows are contained in the ATA reference number?. Ata 56. Ata 57. Ata 53.

What does PFD mean. Primary flight display. Programer flight display. Principal flight display.

What are the two types of composite parts for Airbus A320?. Monolithic or sandwich construction. Monocoque and semimonocoque. Monocoque and monolithic.

AC ESS BUS is normally supplied by the. ACBUS 1. DC BUS 2. AC BUS 2.

What is the basic role of the DMCs?. They compute and generate displays. They generate amber warnings. They generate audio warnings.

The reference (station 0) for all structural measurements for the X axis is set at (datum. 100 in (254 cm) forward of the A/C nose. 100 in (254 cm) rearward of the A/C nose.

How is separated the EIS?. EFIS, CLOCK, ECAM. ECAM & PFD. EFIS & ECAM.

Which computer processes the warnings?. FWC. SDAC. DMC.

How many frames are added to the A321 respect to A320?. 11 FRAMES +. 14 FRAMES +. 12 FRAMES. 13 FRAME +.

What is the function of the RAT?. Generate Hydraulic. Generate pneumatic. Generate Electric.

What is the function of the DMC 3?. Records DMC failures. Acts as a backup for DMC 1 or DMC 2. Processes all warnings messages.

Display are installed on A320 Enhanced are CRT. False. Verdadero.

When is the Static Inverter operating?. When on batteries only. Permanently. With APU.

What is the function of the static inverter?. To transform the 115 VDC to 28 VAC in emergency configuration. To transform the 28 VDC to 115VAC in emergency configuration. Permit the A/Celectrical network to be connected in parallel. To transform the 28 VAC to 115VDC in emergency configuration.

The cockpit panels and instrument lighting controls are located on?. On Overhead panels. On three different panels, and underneath the glareshield. Both are correct.

What is the purpose of the Fan air valve. The FAV blows downstream the precooler to maintain the temp. within limits. The FAV blows upstream the precooler to maintain the temp. within limits. The ensure the correct pressure in the pre-cooler. The FAV blows across the precooler to maintain the temp. within limits.

How are supplied the engines after the center tank is empty?. fuel is supplied from the wing inner cells. fuel is supplied from the ACT. fuel is supplied from the wing over cells.

Where are located the ENGINE fire detectors located. Pylon, fan and core. LP Rotor and HP Rotor. Only engines. All are correct.

What does the FADEC system consists of?. EEC and its peripherals. MCDU and ECAM. EEC and FCU.

What is the main function of the APU?. To produce electrical and hydraulic power. To produce hydraulic power only. To produce Electrical power only. To produce pneumatic and electrical power.

What are the engine valves from ATA 36?. Inlet valve and Outlet Valve. IP, Inlet Valve and Outlet Valve. IP and HP. IP, HP, PRV, OPV and FAV.

what is the thrust of engine V2533?. 33,000 lbs. 27,000lbs. 33,000kg. 30,000lbs.

The pneumatic system operates pneumatically and is monitored by: 3 Bleed Monitoring Computers (BMC 1 & 2, 3). One BMC for the two engines. EEC- Electronic Engine Control. 2 Bleed EEC- Electronic Engine Control Monitoring Computers (BMC 1 & 2).

The CIDS controls and monitors the cabin lights through the panel called?. Flight interphone. Flight attendant panel (FAP). Center pedestal.

How are divided the wing tanks?. Inner cell, outer cell and ACT. LH And RH Wing Tank. Outer cell and inner cell. Outer cell and ACT.

How is controlled the brightness of the reading lights?. Each reading lightpushbutton controls the brightness. By displays. Each reading light potentiometer controls the brightness.

Which component controls and monitors the APU?. FADEC. Fire Detector Unit (FDU). Electronic engine control (EEC. Electronic control box.

How is an APU fire on ground normally extinguished?. Automatically. From APU fire panel. Bottle extinguished. From external power panel.

What is the purpose of IP/HP switching?. Control and monitor the wings. HP bleed is use when the engine are low power. iP is sufficient, HP closes. To generate hydraulic power.

How are supplied the engines after the center tank is empty. fuel is supplied from the wing over cells. fuel is supplied from the ACT. fuel is supplied from the wing inner cells.

At what height are emergency masks activated?. At 14,000 feet from altitud cabin. At 10.000 feet from altitud de cabin. At 8.000 feet from altitud de cabin.

What does the PTU. Transfer only pressure between the green and yellow system. Transfer only pressure between the blue and yellow system. Transfer only pressure between the green and blue system.

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. The 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.

In normal operation, what is the blue hydraulic system pressurized by?. The power transfer unit. An engine driven pump. An electric pump.

17. Where are the EDPs 1 and 2 located?. They are located on the accessory gearbox of engine 1(EDP 1 green system) and engine 2 (EDP 2 yellow system). They are located on the accessory gearbox of engine 2(EDP 1 green system) and engine 1 (EDP 2 yellow system). They are located on the accessory gearbox of engine 1(EDP 1 blue system) and engine 2 (EDP 2 yellow system).

Which hydraulic system powers the nose wheel steering?. Green system. Blue system. Yellow system.

Which surfaces are used to control the roll?. Ailerons and spoilers 2 to 5 numbered from the wing root to wing tip. Elevators and spoilers 2 to 5 numbered from the wing tip to wing root. Spoilers 1 to 5 numbered from the wing root to wing tip.

The two side sticks are used for?. Automatic roll control and manual yaw control. Automatic pitch and yaw control. Manual pitch and roll control.

Which surfaces can be mechanically controlled?. Rudder and THS. Ailerons and THS. Spoilers and THS.

Which computers control the rudder?. The FAC. The SEC. The ELAC.

How can be open the emergency exits on the A318, A319 and A320 aircraft, for emergency evacuation?. The exit can be opened from inside or outside the cabin to activate the evacuation system. The exit can be opened from inside Only the cabin to activate the evacuation system. The door cannot be opened from the outside in such a configuration.

When are the passenger oxygen mask automatically released. When the cabin reaches 14,000 feet. When the aircraft reaches 10,000 feet. When the cabin reaches 8,000 feet.

When does the chemical oxygen generation start?. By pulling the mask the oxygen generator is activated and produces pure oxygen to the masks for a limit time. By pulling the mask the oxygen generator is deactivated and produces pure oxygen to the masks for all time. By pulling the masks the oxygen generator is activated and produces pure oxygen to the masks for all time.

How can be opened the doors in case of failure of the container door opening?. Manually with a special tool located in the cabin crew workstation. By pressing mask manual on pushbutton. By pressing reset pushbutton.

What is the main purpose of the FAP?. The FAP is used for control and programming the functions of the CIDS. The FAP is used only for testing the functions of the Light. The FAP is used for control and programming the functions of the CFDIU.

Where does the toilet bowl rinsing water come from. Waste water system. Waste water tank. The potable water system.

The toilet system is monitored by. The VSC. The MCDU. The CFDS.

Where is the waste quantity displayed?. On the Flight Attendant Panel. On both panels. On the toilet service panel.

How many toilet service panels are fitted on the aircraft. One. Three. Two.

Which component replaces the 3 stand by instruments?. ISIS. EGPWS. ADIRU.

Pitot probes, static ports, TAT sensors are part of?. ADR portion of the ADIRU. FMS system. IR portion of the ADIRU.

Where are the FMGC functions controlled from?. The MCDUS and FAP control panel. The FCU and rudder trim control panel. The FCU and MCDUS.

What is the purpose of the CVR?. The cockpit voice recorder records the last 2 hours of the flight crew Conversations, communications, and aural warnings. To record crew conversations as soon as an incident occurs. To record radio communications during Takeoff and landing.

How many frames are added to the A321 respect to A320. 13 frames. 8 frames. 7 frames.

The Pylons are contained in the ATA reference number. 54. 52. 56.

What is the function of the DMC 3. Acts as a backup for DMC 1 or DMC 2. Records DMC failures. Processes all warnings messages.

What is the basic role of the DMCs. They compute and generate displays. They generate amber warnings. They generate audio warnings.

Which computer processes the warnings?. DMC. FWC. AEVC.

Autopilot is composed. Flight management Flight guidance Flight augmentation Fault isolation and detection system. Flight computer Flight control. Flight automátic Flight control.

What is the function the FG. Autopilot Flight direction Autothrust. Autopilot Radio communication. Control Flying Flight direction.

The Flight Argument part fulfills the following funcións Rudder trim Yaw damper Rudder travel limitation Flight envelope protección. True. False.

Where is the MCDUs. Pedastal Center. Glashi panel. Main centrel panel.