A320 fam rec

What is the material used to construct the vertical stabilizer of the A320?. +13. -7.

What is the material used to construct the vertical stabilizer of the A320?. Carbon fiber monolithic. made from aluminum alloy. Glass Fiber Reinforced Plastic.

What are the two types of construction of the Airbus A320?. 1.FUSELAGE STRUCTURE PRINCIPLE, 2.MONOLITHIC SKIN, 3.SANDWICH PART STRUCTURE PRINCIPLE, 4.WINGBOX STRUCTURE PRINCIPLE. 3.SANDWICH 2.MONOLITHIC. 1WINGBOX STRUCTURE PRINCIPLE 2.FUSELAGE STRUCTURE PRINCIPLE.

The sliding windows and the side fixed windows are contained in the ATA reference number?. Ata 56. Ata 52. Ata 53.

ATA 31 Which computer receive the data from the SDACS to generate amber cautions ?. Flight Warning Computers (FWC). Display management Unit (DMC). Centralized Fault Display Interface Unit (CFDIU).

ATA 31 The post flight report is made up from: It summarizes and displays the list of the ECAM warning messages and the fault messages that occurred during the last flight, with the associated time, flight phase and ATA reference. it is stored in the BITE memory and is transmitted to the CFDIU The ECAM, which generate warning and status messages,.

ATA 24 When is the static inverter operating?. converts the direct current from battery 1 into an AC current if no other source is available. tell all personnel on the aircraft that the lights will g o out Some components are heavy .

ATA 24 In case of an emergency operation ,how is the electrical network supplied ?. This hydraulic power to drive the EMER GEN is supplied by the Blue Hydraulic system via the Ram Air Turbine (RAT). Falso.

ATA 33 The CIDS controls and monitors the cabin lights through the panel called?. FAP. The CIDS also controls: - the passenger lighted signs, - the passenger reading lights, - the passenger calls. Falso.

ATA 28 How are divided the wing tanks?. divided into inner and outer cells. Falso.

ATA 26 Where are the ENGINE fire detectors located?. The engine fire extinguishing bottles are located in the pylon. There are access panels on both sides of the pylon. Falso.

ATA 26 How is an APU fire on ground normally extinguished?. APU shuts down and automatically discharges a dedicated fire extinguisher bottle. Falso.

ATA 49 What is the main function of the APU ?. The APU is a self contained unit, which enables the A/C to be independent of external pneumatic and electrical power source. Falso.

ATA 70 Where are located the main components of the fuel system in the engine?. primarily housed in the wing tanks, the center wing box, and on the overhead flight deck panel. Falso.

ATA 70 What does the FADEC system consists of ?. In order to increase engine reliability and efficiency,. Falso.

ATA 36 The pneumatic system operates pneumatically and is monitored by: There is one BMC for each engine bleed system. Falso.

ATA 21 What is the purpose of the pack?. packs supply dry air to the cabin for air conditioning, ventilation and pressurization . Falso.

ATA 21 What is purpose of the bypass valve?. the ram -air doors are fully open and the bypass valve is fully closed For maximum heating, the ram -air doors are nearly closed and the bypass valve is fu. Falso.

ATA 30 What happens in case of loss of electrical power supply to the engine anti-ice valve ?. the valve opens automatically to ensure the engine intake is continuously protected against icing. Falso.