A330 L&B - GENERAL FAMILIARIZATION

Each IDG is controlled and monitored by a computer called?. EMERG GCU. GAPCU. GCU.

Which computer controls the FADEC of RR TRENT-700 engine?. EEC (Engine Electronic Control). EIVMU (Engine Interface and Vibration Monitorin Unit). OPU (Overspeed Protection Unit).

Which hydraulic system driven the emergency generator?. Green hyd system. Blue hyd system. Yellow hyd system.

The Flight Control surfaces are mainly made of: Composite material but Slats are made of Aluminum Alloys. Aluminum Alloy but Slats are made of composite Material. Composite material but Flaps are made of Aluminum Alloys.

The ECAM system is composed of?. EWD and SD displays. PFDs and EWD displays. PFD and ND displays.

For surge protection, the ECB controls: The IGVs actuator. The surge control valve. The fuel flow parameter.

How is APU fire normally extinguished on the ground?. Automatically through AFECU. Manually from the cabin. From the external power control panel.

What is the purpose of the trim tank transfer system?. For greater flight autonomy. Controls the A/C center of gravity. Controls all transfers to feed the engines.

What is the main parameter for engine power: EPR. N3. EGT.

Which component controls and monitors the APU?. FMU (Fuel Metering Unit). ECB (Electronic Control Box). EEC (Engine Electronic Control).

What components make up the EIS system?. 3 DMCs, 2 FWCs and 2 SDACs. 2 DMCs, 2 FWCs and 1 SDACs. 2 DMCs, 3 FWCs.

How many main fuel pumps has the A330?. 4 main fuel pumps, 2 on each wing tank. 6 fuel pumps, 3 on each wing tank. 2 fuel pumps, 1 main and 1 stand-by on each wing tank.

The Flight Control systems are controlled through: 3 FCPC (PRIM), 2 FCSC (SEC). 2 FCPC (PRIM), 3 FCSC (SEC). 1 FCPC (PRIM), 4 FCSC (SEC).

Which are all AC power suppliers?. IDGs and APU generator. IDGs, external power A & B, APU generator, emergency generator and static inverter. IDGs, external power A & B, APU generator, emergency generator and TR.

The function of the MLG SHORTENING MECHANISM: Decreases the overall length of main landing gear during gear retraction. Ensure that in flight the lever is not selected to the DOWN position. Helps the LDG GRVTY EXTN system to operate quickly.

Which hydraulic system supplies the normal brake system?. Green hyd system only. Green and blue hyd systems. Blue hyd system only.

Wich hydraulic system power the Ram Air Turbine?. Blue hydraulic system. Yellow hydraulic system. Green hydraulic system.

Who perform the radio navigation control normal tuning?. RMP Back-up scale. MCDUs. FMGECs.

Automatically controls the engine thrust via Full Authority Digital Engine Control (FADEC). AFS - FMGECs. Side Stick inputs. Thrust Control Levers.

The pilots interface with the FMGEC (FG part) via the Flight Control Unit (FCU) for: Short-term actions. Long-term actions. Flight-term actions.

Stop and hold the transmission if the SFCCs detect some types of failures such as asymmetry, runaway or over speed: OPU (Over speed Protector). WTB (Wing Tip Brake). POB (Pressure Off Brake).

How is the A330 fuselage divide?. 5 main sections. 6 main sections. 7 main sections.

What is the name of the system to avoid collision with other aircraft in flight?. TCAS. GPS. EGPWS.

How many fire extinguisher bottles are there for the LDCC (Lower Deck Cargo Compartments)?. 1 Bottle. 2 Bottles. 3 Bottles.

The accessory gearbox is driven and connected to the shaft: N1 LP rotor. N2 IP rotor. N3 HP rotor.