GEN FAM A320 ATAS NIVEL 1

The fuel tanks are integrated into the?. Outer cell and inner cell. Inner cell and ACT. Center fuselage área and the wings.

What is the function of static Inverter?. Don’t permit the A/C eléctrical network to be connected in parallet. permit the A/C eléctrical network to be connected in parallet. To transform the 24 VDC to 115VAC in Emergency configuration.

What is the main difference between the A320/A321 and the A319 stabilizers?. The new rib 100N is on the STA007. The new rib 12N is on the STA5970. There is no difference the vertical stabilizer, is the same of the A319.

What is the function of the TR’s?. To convert the 28 VDC into 115 VAC. To convert the 115 VDC into 28 VAC. To convert the 115 VAC into 28 VDC.

What happens when the APU FIRE P/B is released out?. The fire extiguinsher bottle is discharged. Fuel, eléctrical power and bleed supply are cut off and the APU is immediately shut down. Fuel, eléctrical power, hydraulic power and bleed supply are cut off and the APU is immediately shut down.

What are the main power sources to supply the A/C eléctrical network?. There are three idéntical integrated Drive Generators (IDGs) 115 VDC 400Hz. There are two idéntical integrated Drive Generators (IDGs) 115 VDC 400Hz. There are two idéntical integrated Drive Generators (IDGs) 115 VAC 400Hz.

Which computer receives the data from the SDACS to genérate de Amber cautions?. FWC. DMC. SDAC.

The side stick controller (SSC) replaces the. Convetional Aircraft steering. Convetional Aircraft ailerons. Convetional Aircraft Yoke.

What do the Electronic instrument SYSTEM (EIS) consist of?. EIS is a pink and black light below the E/WD display. The EIS is separated into two subsystems: EFIS and ECAM. EIS is a green MÁSTER Warning and amber MASTER caution on each wing.

What do te visual attention getters consist of?. A green MASTER warning and amber MASTER caution in front of each pilot. A Red MASTER warning and amber MASTER caution in front of each pilot. A Res MASTER warning and amber MASTER caution in front of captain.

On which display does the warning message appear?. EWD, the upper Area is used to display the warning message. EWD, the lower area is used for warning, caution and Memo messages. EWD, the upper area is used to display the MLG parameters.

The “Master Warning” and the “Master Caution” lights are also located on. The MCDU. The Glareshield. The overheat panel.

What’s happen when the ENG FIRE P/B is released out?. Fuel, elec power, hydraulic power and bleed supply are not cut off and the ENG is immediately shutdown. Fuel, elec power, hydraulic power and bleed supply are cut off and the ENG is immediately shutdown. Fuel, elec power, hydraulic power and bleed supply are cut off and the APU is immediately shutdown.

How Many Frames are removed to the A319 respect to A320?. 7 frames. 13 frames. 8 frames.

The enhanced main instrument panel instrumentation has been update by: Liquid Crystal Displays (LCDs) replace the existing CRTs. Liquid Crystal Displays (LCDs) replace the existing CFRPs. the existing CRTs Replace the liquid Crystal Display (LCDs).

(A320) How are supplied the engines after the center Tank is empty?. Fuel is transferred from the cockpit to the center tank. Will be necessary to do a refueling. Fuel is supplied from the wing inner cells.

The engine fire Protection is fulfilled by two sub-Systems: The fire detection system and the fire extinguishing system. On the pylon , the fan and the core. On the fan and the turbine.

Which computer send data to the FWC to generate amber cautions?. DMC. SDAC. FWC.

What is the function of the MAINT BUS SW located on FWD C/B cabin panel?. This sw is used on ground and in flight to supply service buses only. This sw is used in flight to supply service buses only. This sw is used on ground to supply service buses only.

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

(A321) How are supplied the engines after the center tank is empty?. Fuel is supplied from the wing tanks. Fuel is supplied from the wing inner tank. Will be necessary to do a refueling.

What are lights controls and monitors by CIDS Through the FAP?. Strobe lights. Cabin lights. Landing lights.

What is fly by wire control?. Both the them. Electrically operated and hydraulically controlled. Electrically controlled and hydraulically operated.

The reference (station 0) for all structural measurements for the X axis is set at?. Is located 2.54 inch (100 m) forward of the aircraft. Is located 254 m (1000 inch) forward of the aircraft. Is located 2.54 m (100 inch) forward of the aircraft.

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

Where is the inflation reservoir of scape slide of emergency exit located?. In the AFT cargó compartment for the A321 and the overheat stowage comparment over the door for the A318/A319/A320. In a container at the bottom of the door. In the AFT cargó compartment for the A318/A319/A320 and in overheat stowage comparment over the door for the A321.

What component does have three servo controls?. RUDDER. THS. AILERON.

Which surfaces are used to Aileron Droop function?. The ailerons are deflected downwards when the Elevators are extended. The ailerons are deflected downwards when the flaps are extended. Spoiler 1 to 5 numbered from the wing root to wing tip.

What happens when the arming lever is set to the armed position?. The girt bar slides towards the telescopic fork. The girt bar Stays attached to the cabin door. The girt bar Stays attached to the cabin floor.

How is supply the oxygen to the cockpit crew?. The nitrógen is supplied from a high pressure oxygen cylinder. The oxygen is supplied from a high pressure nitrogen cylinder. The oxygen is supplied from a high pressure oxygen cylinder.

Where are passenger oxygen masks stored?. In the passenger service unit. In the overheat stowage compartment. In the seat arm rest.

Which surfaces are used to speed brakes function?. Spoilers 2 to 5 numbered from the wing root to wing tip. Spoilers 2 to 4 numbered from the wing root to wing tip. Ailerons 2 to 4 numbered from the wing root to wing tip.

Which hydraulic system operates NLG extensión?. Yellow system. Blue system. Green system.

How can the normal brake be hydraulically powered?. Either by yellow High pressure or by the brake accumulator. Only by the green hydraulic system. Only by the brake accumulator.

What protections are active in a normal law?. In this law are not available the flight envelope protections. All protections are lost in direct law. All protections are available in normal law.

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

The alternate law is automatically introduced as soon as: The normal law is lost due to system failures. The alternate law is not automatically introduced. The direct law is lost due to system failures.