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When a warning or caution occurs, a message appears on the: Engine /Warning Display (EWD). System display (SD).

The Electronic Instrument System (EIS) is composed of: 3 DMCs, 2 SDACs, 2 FWCs and 6 Liquid Crystal Display (LCD) units. 3 DMCs, 2 SDACs, 23FWCs and 4 Liquid Crystal Display (LCD) units.

The Integrated Drive Generator (IDG) in case of failure can be disconnected: From IDG P/B SWs. From IDG P/B CADI.

The AC ESS bus is normally supplied by: AC BUS 1. The Emergency Generator.

The FCU (Flight Control Unit) is normally used: For a short term order selection. For a long term order selection. No special principle applies to the FCU.

The main computer of the CFDS System is the: CFDIU (Centralized Fault Display/interface Unit). CFDIU (Centralized Display/interface Unit).

The Airbus Single Family aircraft use the _________ Aircraft as the base to make the other planes: Airbus A320. Airbus A321. Airbus A330.

The IDG (Integrated Drive Generator) power is: 115v, 400Hz, 3 Phases, 90Kva. 115v, 400Hz, 3 Phases, 80Kva. 116v, 400Hz, 3 Phases, 90Kva.

The Power Transfer Unit (PTU) allows: The Yellow system to power the Green system and vice-versa. The Yellow system to power the Blue system and vice-versa.

The Yellow System can be pressurized by: Engine Drive Pump 2, Electric pump, Power Transfer Unit (PTU). Engine Drive Pump 2, Electric pump, Hand Pump.

The Normal Braking is supplied by: Green Hydraulic system only. Green and Yellow hydraulic systems.

The Cargo Doors are Hydraulically operated by the: Yellow system. Blue system. Red system.

The Tachometers send wheel speed values to: BSCU (Braking Steering Control Unit). ADIRU (Air Data/Inertial Reference Unit).

Supplies Electrical Power to the Aircraft Electrical Network. Integrated Drive Generator (IDG). Maintenance Bus Switch.

Supplies both ECAM displays in normal configuration. DMC 1. DMC 3.

The FIDS function is only active in. FAC 1. FMGC 1.

The Flight Control Surfaces are mainly made of: Composite material but Slats are made of Aluminum Alloys. Composite material but Flaps are made of Aluminum Alloys.

Functions of the Spoiler: Ground spoiler, roll spoiler and speed brake. Ground spoiler, roll spoiler and speed.

The Oxygen for the Flight Crew is supplied by (NEO A/C): Two oxigen cylinder for all crew members. Portable bottles, one per crew member. Portable bottles, one per crew.

When Flushing the Toilets, the electrical unit that controls the Rinse valve and the Flush Valve is the: FCU (Flush Control Unit). FDU (Flush Control Unit).

In the A320 NEO, the fuel is supplied directly to the engines from: The wing tanks only. Inner cells or center tank. Inner cells or center tank.

The CFM56-5B is available in several thrust ratings, due to a: Identification plug installed in the ECU. Different ECU part numbers. Different HMU part numbers.

In the CFM56-5B, the HPT (High Pressure Turbine) has: Single stage turbine. 2 turbine stages.

The main computer that control the APU is the: Electronic Control Box (ECB). Electronic Control Box (EDB).

The primary computer of the Full Authority Digital Engine Control (FADEC) system is: Electronic Control Unit (ECU). Electronic Control Unit (EDU).

The Fuselage of the A320 Family is divided into: 5 parts: Nose Fwd Fuselage, Fwd Fuselage, Center Fuselage, Rear Fuselage, Cone-Rear Fuselage. 5 parts: Fwd Fuselage, Center Fuselage, Rear Fuselage, Cargo Fuselage, Cone –Rear Fuselage.

The Fuel Tank Inerting System includes two (2) subsystems; they are. The Conditioned Air System (CSAS) and Inert Gas Generation System (IGGS). The Conditioned Air System (CSAS) and Inert Gas Generation System .

Ice protection of the AOA, Pitot Probes, static ports and TAT is automatically controlled by the: PHC (Probe Heat Computer). PVC (Probe Heat Computer).

The computer that carry out the Automatic Control of the Outflow valve is the: CPC (Cabin Pressure Controller). RPCU (Residual pressure Control Unit).

How many fire extinguisher bottles use each engine?. 2 Fire Bottles. 1 Fire Bottle.

When the Wing Anti-ice Push Bottom is set to ON, how many valves open: 2 WAI Valves. 4 WAI Valves. 3 WAI Valves.

The cargo Smoke Detector system is monitored by: CIDS-SDF (Cabin Intercommunication Data System - Smoke Detection Function). SDCC (Smoke Detection Control Computer).

Where are located the Inflation Reservoir for Over-wing Emergency Exit Escape Slide of the A320: In the after cargo compartment. In the wing root. In the forward cargo compartment.