diferencias

A320 NEO family consists of?. A318/A319/A320 Aircrafts. A319/A320/A321 Aircrafts. A318/A320/A321 Aircrafts.

What is the function of the Flight Control Unit (FCU) located on the glareshield?. Control and monitoring of the Auto Flight System (AFS). Control and monitoring of the Auto Flight System (AFS). Control and monitoring of the Auto Land (AFS).

Which indication needs awareness but not immediate action on the aircraft?. Amber master caution. Amber master warning. Red master caution.

Which aircrafts are powered by the PW1100G. A319/A320/A321 Neo. A318/A319/A320/A321 Neo. A318/A319/A320 Neo.

How can the thrust rating be changed on the PW1100G?. A Data Storage Unit (DSU) which is connected onto the Electronic Engine Control (ECU). A Data Storage Unit (DSU) which is connected onto the Electronic Engine Control (EEC). A Data Storage Unit (DSU) which is connected onto the Electronic Engine Control (FMGC).

The air produced by the fan is know as?. secondary airflow or parasite airflow. Primary airflow or by pass airflow. secondary airflow, or by pass airflow.

Which rotor is rotated during engine starting?. The Intermediate pressure compressor through the gearboxes. The LP compressor through the gearboxes. The hp compressor through the gearboxes.

How is electrically powered the FADEC when the engine is running?. FADEC operation is supplied by a ignition system driven by the gearbox. FADEC operation is supplied by a dedicated alternator driven by the gearbox. FADEC operation is supplied by a dedicated alternator driven by the engine starter.

How are monitored the fan cowl latches PW1100g. The FAN cowl latches of the a320 neo are monitored by proximity switches wich send their position signal to the EEC. The FAN cowl latches of the a320 neo are monitored by proximity switches wich send their position signal to the ECB. The FAN cowl latches of the a320 neo are monitored by proximity switches wich send their position signal to the EIU.

Where are installed the primary components of the fuel system?. The primary components of the fuel system are on the RH side of the engine core. The primary components of the fuel system are on the both sides of the engine core. The primary components of the fuel system are on the LH side of the engine core.

Why are aerodynamic strakes mounted on the fan cowls?. Aerodynamic strakes are mounted on the fan cowls to reduce aircraft performance during manoeuvres. Aerodynamic strakes are mounted on the fan cowls to improve aircraft performance during manoeuvres. Aerodynamic strakes are mounted on the reverser improve aircraft performance during manoeuvres.

Which engine mount assembly bears engine vertical and radial loads?. The aft mount. Forward Mount. Both forward and aft mounts.

What is the purpose of the FDGS?. It helps to increase the fan rotating speed and permits the LPC to rotate at a higher speed. It helps in reducing the fan rotating speed and permits the LPC to rotate at a lower speed. It helps in reducing the fan rotating speed and permits the LPC to rotate at a higher speed.

How many fuel nozzles and igniter plugs houses the combustion chamber?. The annular combustion chamber houses 12 fuel nozzles (6 simplex and 12 Duplex) and 2 igniter plugs and supports effective combustion of the air/fuel mixture. The annular combustion chamber houses 18 fuel nozzles (6 Simplex and 6 Duplex) and 2 igniter plugs and supports effective combustion of the air/fuel mixture. The annular combustion chamber houses 18 fuel nozzles (6 air/fuel and 6 Duplex) and 4 igniter plugs and supports effective combustion of the air/fuel mixture.

Which parameter is used to control the FRV depending on the fuel to the tanks?. The FRV is controlled by the Electronic Engine Control (ECU) depending on the fuel temperature. The FRV is controlled by the Electronic Engine Control (EEC) depending on the fuel pressure. The FRV is controlled by the Electronic Engine Control (EEC) depending on the fuel temperature.

Where is drained the residual fuel after engine shutdown?. The residual fuel in the manifolds is drained back through the FDV to an ecology collector tank. The residual fuel in the manifolds is drained back through the FDV to the ecology collector tank. The residual fuel in the manifolds is drained back through the FDV to the aircraft tanks.

Which computer provides overspeed protection for N1 and N2 by driving to close the Thrust Control Malfunction (TCM)/Overspeed torque motor in the Integrated Fuel Pump and Control (IFPC)?. EEC. FPCU. PHMU.

How is normally powered the PHMU?. The PHMU receives aircraft 28V DC directly from the aircraft normal DC power bus through the EIU. The PHMU receives aircraft 115V AC directly from the aircraft normal AC power bus through the EIU. The PHMU receives aircraft 28V DC directly from the aircraft normal DC power bus through the EEC.

How can be set the engine thrust?. Manually from the master lever or automatically from the Auto Flight System (AFS). Manually from the throttle control lever or automatically from the Auto Flight System (AFS). Manually from the throttle control lever or automatically from the Auto Thrust System (AFS).

What are the defense lines used to prevent inadvertent deployment of the thrust reverser?. Primary locks each actuator and one tertiary lock at the upper of each translating sleeve. Primary locks each actuator and one tertiary lock at the bottom of each translating sleeve. Primary locks each actuator and one tertiary lock at the bootom of each translating cowl.

Which components are normally controlled by each BMC?. Normally BMC 1 controls the LH bleed system and BMC 2 the RH bleed system. Normally BMC 1 Channel A does all the control and monitoring of the LH EBAs and BMC 1 Channel B the RH EBAs. Normally BMC 2 Channel A does all the control and monitoring of the LH EBAs and BMC 1 Channel A the RH EBAs.

Which stage of the of the engine supplies hot air for the engine anti ice sytem?. Hot air for the engine anti-ice system is supplied by a dedicated HP 7th stage. Hot air for the engine anti-ice system is supplied by a dedicated HP 6th stage. Hot air for the engine anti-ice system is supplied by a dedicated HP 5th stage.

Where are located the fire detector on the PW/1100G?. Pylon, Aft-Core compartment. Fan, Pylon, Core compartment. Pylon, Core compartment, TEC.

Where is sent the fuel recirculated on the engines?. Center tank. Inner Cell. Outer Cell.

Where is circulated the fuel when the outer cell is full?. Fuel overflows to the surge tank through a spill pipe. Fuel overflows to the inner cell through a spill pipe. Fuel overflows to the center tank through a spill pipe.