A320 general familiarization

sHow many frames are added to the A321 with respect to A320?. 20 frames. 13 frames. 15 frames.

How many frames does the A320 Family have?. 87 frames. 120 frames. 75 frames.

The reference (station o) for all structural measurements for te X axis is set at (Datum)?. 120 inch. 200 inch. 100 inch.

What is the material used to construct the vertical stabilizer of the A320?. Carbón fiber reinforced plastic ( CFRP), Glass fiber reinforced plastic (GPRP). Fiber plastic (FP), carbón plastic (CP). Glass fiber reinforced (GFR) Carbón fiber (CF).

What is the main difference between the A319/320/321 and the A318 vertical stabilizers?. A318. 15 RIB. A318 12 RIB. A319/20/21 13 rib.

The pushbuttons light and annunciator lights are in different colors according to?. Red lights. Ámbar lights. According functions.

Which computer processes the warnings. System Warning Computer. The Flight Warning Computer (FWC). The Warning Computer System.

What are the two types of composite construction of the Airbus A320?. Aluminium or copper. Aluminium or fiber plastic. Monolithic or Sandwich.

The sliding windows and the side fixed windows are contained in the ATA reference number?. ATA 25. ATA 56. ATA 70.

What is the function of the DMC 3?. Activation lights. BackUp. Memory display.

Which are the displays in EIS?. Warning Computer,dysplay fly, engine dysplay. Navegation display, Computer Warning, dysplay System. Primary fly display, navegation display, engine Warning display, System display.

What do visual attention getterw consiste of. Red Master Warning ,Ambar Master caution. Gren Warning , yellow Warning. Red and yellow Warning.

Which computers receive the data from the SDACS to generate amber cautions. The Warning Computer (TWC). The flight Warning Computer (FWC). The Warning display (TWD).

Which are the main functions of AIDS?. Lighting controls, lights status. Monitor Engine Estatus, APU status, Aircraft performance. Engine repair, APU status.

On which display does the warning message appear?. Engine Estatus Dysplay. Engine Warning Dysplay. Warning Computer Engine.

The post flight report is made up from. Last Leg Report , Last Leg ECAM Report. Switch last Report, ECAM REPORT. The post flight report.

DC BAT BUS can be supplied by the? Emergency Generator Static inverter. APU Inverter. Bus Inverter. Static Inverter.

In case of an emergency operation, how is the electrical network supplied?. APU. RAT. Static inverter.

What is the function of the RAT?. Pressurizes the hidraulic system,Powers the emergencia generator. Helps the APU. Monitoring Engine Warning display.

The cockpit panels and instrument lighting controls are located. Engine Dysplay. On three different panel and Underneath the Glareshield. Warning Computer dysplay.

The CIDS controls and monitors the cabin lights through the panel called?. Engine Estatus Dysplay, The passenger reading. The RAT, The Dysplay system,the power Dysplay. The passenger lighted signs,The passenger reading lights, the passenger calls.

What does FAP mean?. Warning and caution display. Flight Attendant Panel. Dysplay System Engine.

When si the static inverter operating. Inverter 18v DC a 115V AC. Converter 24v DC a 24v AC. Inverter 115v DC a 200v DC.

How are the engines supplied after the center tank is empty. Supplied for inner cello,outer cell. Center tank. Right wing.

How are divided the wing tanks. Four tank refuel. Six refuel tank per valve. One refuel tank per valve.

What kind of pump do you use A321 Center tank. Four fuel pumps. Two fuel pumps. Five fuel pumps.

Where are the ENGINE fire detectors located ?. Pylon, fan , Core. APU,wings,engine. Cockpit, pylon ,engine.

Which component monitors cargo compartments smoke?. Fire detection. Smoke detection and fire extinguishing. Fire Warning Computer.

How is an APU fire on ground normally extinguish. On ground manually. Automatic. No extinguishing.

What is the main function of the APU?. Electronic control. Control power. Electrical power , Pneumatic power.

Where can an APU emergency shutdown be performed from the outside?. Power Control manual. External Power Control Panel. Panel engine Warning.

APU Bleed is available up to?. Up to front firewall. Up to wings. Up to exit.

Which component controls and monitors APU?. Engine control System. APU control System. Electronic Control Box (ECB).

What are the characteristics of V2500 engine?. Available For A318. Available For A319/A320/A321, axial flow ,2,500 pounds of thrust. 1000 pounds of thrust,axial flow.

How to change the available thrust in V2500 engine. Electronic Engine Control (EEC). Fire detection control. Warning Computer dysplay.

Where are located the main components of the fuel system in the engine?. Located on the lift side of the engine. Located on the tail. Located on the APU.

What does the FADEC system consist of. engine turbine. Is fuel System display. (EEC) Electronic Engine Control and peripherals.

The V2500-A5 powers the complete single aisle family of aircraft except?. A322. A318. A330.

How many stages LP/HP compressor have V2500 engine?. 2 primary modules. 8 primary modules. 5 primary modules ,fan,low pressure ,hight pressure ,lp turbine ,accesory drives.

The pneumatic system operates pneumatically and is monitored by?. Computer Data system. Bleed Monitoring Computer (BMC 1 y 2). System and data Computer.

What is the purpose of the pack?. The pack are responsable for basic temperature regulation. Fuel pumps responsable. Pumps hidraulic system regulation.

What is the purpose of the Fan air valve. Maintenance temperature low. Blow across the pre- cooler to maintein the temperature whitin limits. Maintenance temperature hight.

What is the purpose of IP/HP switching?. HP is only usted low pressure, IP close when there is enought pressure. HP/IP closed in the ground. HP/IP Open in hight pressure.

What is the purpose of the pack?. The pack are responsable For low pressure. The pack For responsable For ice and rain temperature. The pack are responsable For basic temperature regulation.

What is the purpose of the bypass valve?. Regulates pressure. Regulates temperature of packs. Regulates hidraulic system.

What is the function of ACSC. Control and monitor the temperature regulation System For the cabin zones. Monitor System Engine. Monitor and regulation lights of the cockpit.

What happens in case of loss of electrical power supply to the engine anti-ice valve?. Manually. Will automatically. Only maintenance.

Bleed air from the engines or the APU is supplied to?. Engine Control. Fuel System. Wing anti-ice(WAI).

How are the waste water drain masts heated?. Manually heated. They are electrically heated. None is correct.

Which hydraulic systems are pressurized by an engine driven pump?. Yellow hydraulic system. Green system. Blue hydraulic system.

In normal operation, what is the blue hydraulic system pressurized by?. Automatic activated. By an electric pump, manually activated on ground. Only maintenance ground.

Where are the EDPs 1 and 2 located?. On the APU control. On the cabin and cockpit. On the accesory Gearbox of engine.

What is the function of FSOV?. Closed en the valve fuel tank. Normally closed ,insolates the IGGS from the fuel tank. Open in the fuel pumps.

Which hydraulic system powers the nose wheel steering?. Green hydraulic system. Brow hydraulic system. Black hydraulic system.

How can the parking brake be hydraulically powered?. Black hydraulic System. Blue hydraulic system. Yellow hydraulic system,brake accumulator.

Which computer controls gears extension and retraction sequence. Engine Estatus Dysplay. Landing Gear Control and Interface Unit (LGCIU). Warning Computer dysplay.

Which hydraulic system powers the alternate braking. Yellow hydraulic system. Alternate braking System. Power Control Panel.

Which surfaces are used to control the roll. Nose. Wings. Aileron.

The two side sticks are used for?. For automatically aileron control. For manual pitch and rool control. For engine control.

How are all flight control surfaces controlled and operated. electrically controled , hidraulically operated. Manually activated, controled hidraulically. Control manual and operating manual.

The level of flammability defined in the proposal was established based upon comparison of the safety record of. Wing tank refuel. Center wing fuel tank. Wing tank FUEL.

Where is discharged the OEA in the FTIS. In the flight. In the ground. Over-board.

What is the computer that monitors the FTIS?. AAC. ICU. FAA.

What is the function of ASM. Separates fuel of engine. Separates oxygen from fuel tanks. Oxigen an hidraulically operated.

What is the function of the door damping and emergency operation cylinder. An emergency acts For automatically door opening. Not automatically door. In the ground manually activated.

How can be open the emergency exits on the A318, A319 and A320 aircraft, for emergency evacuation?. Open manually. Opened from inside or outside the cabin. Opened from cockpit.

What happens when the arming lever is set to the armed position?. Not ready to deploy. Slide ready to deploy and inflate in case of emergency. Not automatically in case of emergency.

When are the passenger oxygen masks automatically released. 40,000 feet. 20,0000feet. 14,000 feet automatically.

When a does the chemical oxygen generation start?. In case of emergency. In case of cabin depressurization. In case of fire.

How can be opened the doors in case of failure of the container door opening?. Opened from cargo compartments. Open from Windows exit. Opened from the cockpit or manually.

How is the waste transported to the waste holding tank?. Is send under effect of cabin differential pressure. Send from inside pressure. Send from fuel tanks.

The toilet system is monitored by: Yellow hydraulic System. (VSCF) Vacum system controller function. Flight Warning Computer.

Which component replaces the 3 stands by instruments?. Automatically in case of failure. Operate independently, failure of one not affect the other. Manually in case of failure.

Pitot probes, static ports, TAT sensors are part of?. VSCF Vacum system. ISIS integrated standard. ADIRIS System have peripheral components conect LRU.

RA displayed in PFD below?. 3,000 feet automatically. 2,500 feet Above Ground Level (AGL). 5,000feet Above.

What are the basic functions of the FACS. System Warning dysplay, engine Estatus. Flight Augmentation,Faul Isolation ,Detection System. Static inverter, operating manual.

Where are the FMGC functions controlled from?. Flight Warning, dysplay System. Flight Management, Flight Guidance. Computer Data, system controller.

What's is the purpose of the RMPS. The passenger calls. Give the capability of tuning all comunication radios. Signal of failure radios.

Which computer is the heart of the audio System. The Audio Management Unit (AMU). The Aircraft performance (ATP). The passenger lighted ( TPL).

What is the purpose of the CVR?. Record the last flight. Record the las 2 hour For the flight crew conversation. Record the conversation of the cabin.

Where are displayed the messages related to pre-FANS status?. Control manual ICU. Monitoring FTIS. Displayed on the EWD Engine Warning dysplay.

How is the pilot noticed when new ATC messages are transmitted to the aircraft?. The passenger calls. The ATC menu. The Dysplay system regulation.