PW1000G

The accessory gearbox is installed under the core engine and is driven by?. The LP rotor through the Angle Gearbox. The HP rotor through the Angle Gearbox. The HP rotor through the FDGS.

The Propulsion Control System (PCS) is composed by?. EEC, PHMU and EIU. ECU, PHMU and EIU. EEC, PHMU and EVMU.

Which parameters are monitored by the PHMU?. The PHMU interfaces with the EIU. It monitors the Engine Vibrations and the Oil debris. The PHMU interfaces with the EEC. It monitors the Engine Vibrations and the Oil temperature. The PHMU interfaces with the EEC. It monitors the Engine Vibrations and the Oil debris.

Where are located the EEC and PHMU?. The EEC and Prognostic and Health Monitor Unit (PHMU) are on the UPPER side of the fan case. The EEC and Prognostic and Health Monitor Unit (PHMU) are on the RH side of the fan case. The EEC and Prognostic and Health Monitor Unit (PHMU) are on the LH side of the fan case.

Which part on the engine is used to enable troubleshooting of the leaking components?. Drain Mast. EEC. Fuel Diverter.

Which engine mount assembly bears engine thrust, vertical and lateral loads?. The AFT mount assembly bears the engine thrust, vertical and lateral loads. The both mount assemblies bears the engine thrust, vertical and lateral loads. The FWD mount assembly bears the engine thrust, vertical and lateral loads.

Which component provides approximately the 90% of the thrust?. LPC. Fan Rotor. HPC.

Where is obtained the air for the bleed system?. The HP Compressor supplies air from Stage 3 and stage 8 to the aircraft systems. The HP Compressor supplies air from Stage 5 and stage 8 to the aircraft systems. The HP Compressor supplies air from Stage 3 and stage 10 to the aircraft systems.

Which components are included on the TEC?. The TEC provides the attachment point for the forward engine mount and houses for Exhaust Gas Turbine (EGT) thermocouples. The TEC provides the attachment point for the rear engine mount and houses for Exhaust Gas Turbine (EGT) thermocouples. The TEC provides the attachment point for the read engine mount and houses for EPR sensors.

How is closed the fuel LPSOV in a normal shutdown?. During a normal engine shutdown, the Master Lever controls the LPSOV to close and sends a shutdown signal to the PHMU. During a normal engine shutdown, the manual pushbutton controls the LPSOV to close and sends a shutdown signal to the EEC. During a normal engine shutdown, the Master Lever controls the LPSOV to close and sends a shutdown signal to the EEC.

What is the function of the Fuel Filter Differential Pressure (FFDP) sensor?. The FFDP measures the differential pressure across the fuel manifold, this helps to detect of the filter is partial or totally clogged. The FFDP measures the differential pressure across the fuel filter, this helps to detect of the filter is partial or totally clogged. The FFDP measures the normal pressure across the fuel manifold, this helps to detect of the filter is partial or totally clogged.

When is the EEC electrically supplied for the aircraft network?. When high pressure rotor sped (N2) is below 10% or when the dedicated Permanent Magnet Alternator (PMA) has failed. When high pressure rotor sped (N2) is above 10% or when the dedicated Permanent Magnet Alternator (PMA) has failed. When high pressure rotor sped (N2) is below 10% or when the dedicated Permanent Magnet Alternator (PMA) has started.

How does the SAV works?. The SAV is electrically controlled by the EEC and pneumatically operated. The SAV is electrically controlled by the ECU and pneumatically operated. The SAV is electrically controlled by the EIU and pneumatically operated.

When is displayed a clogged fuel filter message?. A CLOG message appears in amber, associated with an ECAM message only when the differential pressure across the fuel filter is excessive. A CLOG message appears in amber, associated with an EFIS message only when the differential pressure across the fuel filter is excessive. A CLOG message appears in amber, associated with a MCDU message only when the differential pressure across the fuel filter is excessive.

When is the HP bleed system used?. The HP bleed system is only used when the engines are at high power and for engine efficiency the High Pressure Valve (HPV) is kept closed during cruise. The HP bleed system is only used when the engines are at low power and for engine efficiency the High Pressure Valve (HPV) is kept closed during cruise. The HP bleed system is only used when the engines are at low power and for engine efficiency the High Pressure Valve (HPV) is kept open during cruise.

What is the purpose of the Bleed Pressure Sensor (BPS)?. It provides to BMC the actual bleed air pressure delivered through the PRV. It provides to BMC the actual bleed air pressure delivered through the PRV, the HP and cross-bleed valves. It provides to BMC the actual bleed air pressure delivered through the OPV.

What is the function of the PCS in the ice and rain system?. PCS is responsible for the bleed management when the engine anti ice (A.ICE) system is switched ON. PCS is responsible for the bleed management when the engine anti ice (A.ICE) system is switched OFF. PCS is responsible for the bleed management when the WING anti ice (A.ICE) system is switched OFF.

What is the difference between the PW1100G fire extinguisher bottles and the other engines of the A320 Family?. There is no difference all the bottles has the same size and part number. The PW1100G are smaller. The PW1100G are larger.

Which computer receives the signal of the overflow sensor in order to close The FRTT?. EEC. FQI. FLSCU.

How many frames is constructed the whole family A320 NEO?. 80 fr. 87 fr. 100 fr.

Which indication needs immediate action on the aircraft?. Red Master Caution. Red Master Warning. Amber Master Caution.

Which indication needs awareness but not immediate action on the aircraft?. Amber Master Caution. Amber Master Warning. Red Master Caution.

Why is a safety jack positioned at the rear of the aircraft?. Prevents the aircraft from sideward movement. Prevents the aircraft from tipping down. Prevents the aircraft from tipping up.

What is the purpose of the geared turbo fan engine?. To increase fuel consumption, air pollution and noise. To reduce fuel consumption, air pollution and noise. To reduce oil consumption, air pollution and noise.