Cuestionario Airbus A320 P.6

What is the definition of corrosion?. Enhancement of metals. Destruction of metals by chemical effects. Strengthening of metals. Natural wear and tear of metals.

Which of the following is NOT a step necessary for satisfactory control of corrosion?. Regular maintenance. Applying heat. Initial identification of corrosion. Complete removal of corrosion when it occurs.

Which of the following is NOT a corrosive agent?. Acids. Alkalies. Pure water. Salts.

Which atmosphere can cause special problems due to the presence of oxidized sulphur and nitrogen compounds?. Marine Atmosphere. Industrial Atmosphere. Tropical Atmosphere. Desert Atmosphere.

How many main zones are the internal areas of an aircraft divided into, in terms of surface protection?. Two. Three. Four. Five.

Which of the following is NOT a group of protective treatment mentioned?. Pretreatment. Paint coatings. Special coatings. Heat treatments.

What is the primary purpose of pretreatment of materials?. To add color to the materials. To increase weight. To increase corrosion-resistant properties and provide a good surface for paint adhesion. To make the material shiny.

What is the primary cause of corrosion in the general atmosphere?. Lack of oxygen. Excess of nitrogen. Moisture and oxygen. Carbon dioxide.

Which of the following is NOT a step necessary for satisfactory control of corrosion??. Regular maintenance. Applying heat. Initial identification of corrosion. Complete removal of corrosion when it occurs.

The fastener contact area of the tool must be rough and textured. True. False.

A clear indication of a loose fastener is when the head of a fastener is rolled upwards at its periphery. True. False.

If a fastener is suspected to be loose, it should be ignored until the next maintenance cycle. True. False.

The use of a washer under a nut/collar is only permitted when used in the original construction. True. False.

It's always recommended to use two washers instead of one under the nut/collar. True. False.

The hand hammering method is the most recommended method for installing rivets in the aircraft structure. True. False.

What type of doors are the forward and aft passenger doors of the Airbus A320 Family?. Swing-type doors. Sliding doors. Plug-type doors that open upward, outward, and forward. Hydraulic doors that open automatically.

How do the passenger doors of the Airbus A320 Family open?. Open inward and upward. Swing outward and downward. Open upward, outward, and forward parallel to fuselage. Automatically open and close hydraulically.

What is the purpose of the slide ARMING/DISARMING lever on the passenger doors?. Control cabin temperature. Activate emergency lighting. Disarm the escape slide. Connect the slide to the floor for automatic deployment.

How does the escape slide on the passenger doors deploy in an emergency?. Automatically inflates when the door is opened from the outside. Manually inflated by passengers. Automatically inflates when the slide-arming lever is disarmed. Requires activation by cabin crew.

How many overwing emergency exits are typically found on the Airbus A321?. Two exits. Four exits. Six exits. None of the above.

How can the overwing emergency exits on the A318, A319, and A320 be opened for evacuation?. Only from inside. Only from outside. Both from inside or outside. They cannot be opened for evacuation.

How are the cargo compartment doors of the Airbus A320 Family operated?. Electrically using the yellow system. Manually with a locking handle. Hydraulically using the blue system. Automatically via the cockpit controls.

What is the function of the bulk cargo door on the A320 and A321 aircraft?. Provides access to the avionics compartment. Gives access to the bulk cargo compartment. Opens into the passenger cabin. Acts as an emergency exit.

How are the avionics compartment access doors on the lower fuselage operated?. Manually. Electrically. Automatically. Using a hand pump.

What is the purpose of the Cockpit Door Locking System (CDLS) in the Airbus A320 Family?. Control cabin temperature. Prevent unauthorized cockpit access. Manage the escape slide. Activate the emergency lighting.

How is the cockpit door typically locked when the aircraft is powered?. Manually with a key. Automatically by CDLS. Electronically with a keypad. Physically by flight crew.

What does the cockpit door escape hatch feature, and how is it kept in position?. Contains emergency supplies. Has a locking handle. Includes a keypad for access authorization. Secured with two pip-pins.

What components are part of the Cockpit Door Locking System (CDLS) in the Airbus A320 Family?. Cockpit door panel on the pedestal with a toggle switch. Control cabin temperature. Overhead control unit in cockpit with integrated maintenance annunciators. Electrical release strikes.

What is the purpose of the buzzer located on the cockpit overhead panel?. Control cabin temperature. Prevent unauthorized cockpit access. Activate the emergency lighting. Provide maintenance alerts.

How does the avionics compartment door locking mechanism operate on the Airbus A320 Family aircraft?. Electrically. Manually. Automatically. Using a hand pump.

The escape slide inflates automatically when the slide-arming lever is in the ___(?)___ position and the door is opened from the inside. armed. disarmed. closed. locked.

The A321 is equipped with four emergency exit doors located forward and aft of the ___(?)___. cockpit. avionics compartment. wing. cargo compartment.

To activate the evacuation system through the overwing emergency exits on the A318, A319, and A320, authorized personnel must ___(?)___ the exits from the inside. disarm. lock. open. activate.

The cargo compartment doors on the Airbus A320 Family give access to the forward and aft ___(?)___ compartments. cargo. cockpit. avionics compartment. passenger.

In case of electrical failure, the cargo compartment door can be opened manually using a ___(?)___. hydraulic system electric pump. hand pump. slide ARMING/DISARMING lever. keypad.

There are ___(?)___ avionics compartment access doors on the lower fuselage around the nose landing gear bay. two. three. four. five.

The locking mechanism for the avionics compartment access doors is ___(?)___ on each door. different. identical. electronic. manual.

The cockpit door on the Airbus A320 Family is designed to prevent ___(?)___. cabin temperature. hijacking attempts. unauthorized access. mechanical failures.

The cockpit door escape hatch is secured with two ___(?)___ to keep it in position. toggle switches. pip-pins. escape slides. keycards.

The A318 and A319 are equipped with two overwing emergency exits, and the A319 can optionally have ___(?)___ additional exits. one. two. three. four.

The avionics compartment access doors on the lower fuselage open ___(?)___. inward. outward. upward. downward.

To perform normal door opening from the outside, one must check that the arming lever is in the ___(?)___ position and that the cabin pressure indicator is not flashing. disarmed. armed. locked. opened.

In case of emergency opening, the arming lever should be in the ___(?)___ position, and after pulling the door control handle rapidly fully up and releasing it, the door opens and locks automatically. armed. locked. disarmed. opened.

How many main parts is the fuselage divided into?. Three. Four. Five. Six.

What are the names of the main parts that make up the fuselage?. Forward, center, rear, cone. Nose, forward, center, rear, cone. Upper, lower, middle, aft, tip. Front, back, middle, aft, end.

How does the length of the A321 forward fuselage compare to the A320, and which frames does the additional section (14A) extend between?. It's eight frame bays longer, extending between Fr 35 and Fr 35.8. It's five frame bays longer, extending between Fr 47 and Fr 47.5. It's three frame bays shorter. It's four frame bays shorter.

The fuselage of the Airbus A320 is divided into five main parts. (True/False). True. False.

The forward fuselage of the A321 is longer by eight frame bays compared to the A320, and it includes an additional section between frames (Fr) 35 and 35.8. (True/False). True. False.

The A319 forward fuselage is four frame bays shorter than the A320. (True/False). True. False.

An additional emergency exit is installed on both sides of the A319 in section 15 to accommodate a cabin capacity of at least 160 passengers. (True/False). True. False.

The nose forward fuselage contains the nose landing gear bay and access and service door cutouts. (True/False). True. False.

The nose landing gear bay is shaped by three machined panels reinforced by horizontal and vertical extruded sections attached to the corresponding frames. (True/False). True. False.

The central panel of the lower fuselage in the nose forward fuselage contains an opening for access between Fr 3 and 5 and the opening for the nose landing gear bay between Fr 9 and 20. (True/False). True. False.

What is the extent of the cone/rear fuselage section, measured in frame numbers?. Fr 65 to Fr 90. Fr 70 to Fr 87. Fr 60 to Fr 80. Fr 50 to Fr 75.

What does the rear pressure bulkhead separate within the fuselage? (Choose all that apply). Pressurized rear fuselage,Un-pressurized cone/rear fuselage. Cargo compartment. Cone rear fuselage. Landing gear bay.

How is the tail cone unit connected to section 19?. By four lugs and one spigot. Welded joints. Glue and rivets. Bolted connections.

What is the primary function of the engine pylons installed under each wing?. To support the engine. To house electrical wiring. To support the nacelle. To store fuel.

Which part of the pylon primarily houses most of the systems connected with the engine?. Secondary structure. Primary structure. Fairings. Fan cowl doors.

How many points attach the pylon box to the wing?. Three. Four. Two. Five.

What components make up the stabilizers?. Trimmable Horizontal Stabilizer (THS), elevators, vertical stabilizer, and rudder. Wings, ailerons, flaps, and slats. Engines, pylons, and nacelles. Landing gear and doors.

What is the main structure of the Trimmable Horizontal Stabilizer (THS)?. Spar boxes. Elevators. Leading edge. Trailing edge.

What are the primary functions of the engine pylons installed under each wing of the aircraft?. To support the engine, to transmit the engine thrust, to enable the routing and attachment of all the systems connected with the engine. To provide additional lift to the aircraft, to house the landing gear, to store fuel. To provide structural support to the wing, to house the pilot, to store luggage. To house the aircraft's avionics, to support the hydraulic system, to provide additional fuel storage.

Where can detailed information about the structure of the nacelle be found? (Choose all that apply). In the aircraft's maintenance manual, In the nacelle manufacturer documentation. In the pylon manufacturer documentation. In the IPC and SRM. In the aircraft's flight operations manual.

How many points support the engine on the pylon box?. Two points. One point. Three points. Four points.

The hinge fittings of thrust reverser doors are installed on the forward fairing (secondary structure) of the pylon. True. False.

The pylon box is attached to the wing at two points. True. False.

The aft engine to pylon attach fitting is located at Rib 4 for the CFM 56-5 engine configuration. True. False.

Stabilizers include wings, flaps, slats, and ailerons. True. False.

The adjustment of the angle of incidence of the THS is achieved by a hydraulic actuator. True. False.

There are two spar boxes in the Trimmable Horizontal Stabilizer (THS). True. False.

The center joint in the spar box assembly is made from aluminum. True. False.

The leading edge of the Trimmable Horizontal Stabilizer (THS) includes avionics and hydraulics. True. False.

The cockpit has four fixed windows: two windshields and two fixed side windows that can be removed from the exterior. True. False.

The sliding windows in the cockpit can only be opened and controlled from the outside of the aircraft. True. False.

Cabin windows consist of a seal, inner and outer panes made of stretched acrylic resin, held together by a seal. True. False.

In normal operation, both the inner and outer panes of cabin windows are pressurized to maintain cabin pressure. True. False.

Circular windows on passenger/crew doors and emergency exit doors are used for inspection and observation. True. False.

The inner pane of door windows is not designed to maintain cabin pressure in case of outer pane failure. True. False.

The cockpit has both fixed and sliding windows. True. False.

The windshield panes in the cockpit are made of hard glass and are not interchangeable between different suppliers. True. False.

The fixed side windows in the cockpit are held by retainers bolted onto the outer surface of the frame. True. False.

The fixed side windows have an integral anti-icing and defogging system. True. False.

The sliding windows in the cockpit can be controlled from inside the cockpit and used as emergency exits. True. False.

The sliding windows have only one layer of glass without interlayers. True. False.

Cabin windows are installed and removed from the inside of the aircraft. True. False.

The inner pane of cabin windows is pressurized in normal operation. True. False.

Door windows are used for inspection and observation to check if the cabin is pressurized or to verify if the outside is clear. True. False.

The outer pane of door windows has a vent hole that allows pressurization only in normal operation. True. False.

The primary function of the sliding windows in an emergency is to act as __(?)__. ventilation. observation points. emergency exits. additional lighting.

The windshields are equipped with an anti-icing and __(?)__ system. anti-fogging. defogging. heating. cooling.

The windshield panes are mounted with retainers on the ______ surface of the frame. inner. outer. top. bottom.

The fixed side windows are installed with an integral __(?)__ system. heating. anti-icing. defogging. cooling.

Cabin windows are installed and removed from __(?)__. the exterior. the inside. either side. the top.

The inner pane of the cabin windows is designed to __(?)__ cabin pressure. increase. decrease. maintain. monitor.

The circular windows help check from outside if the cabin is __(?)__. pressurized. ventilated. illuminated. conditioned.

In case of outer pane failure, the __(?)__ pane is able to maintain the cabin pressure. outer. inner. cockpit. passenger.

The circular windows are essential for verifying if the outside is clear for __(?)__. landing gear deployment. engine start. door opening/slide deployment. air conditioning activation.

Which spoiler is connected to the false rear spar?. Spoiler 1. Spoiler 2. Spoiler 3. Spoiler 4.

How are the bottom surface access panels of the fixed leading edge attached?. With screws. With adhesive. With quick release fasteners. With bolts.

Which component of the A321 flaps is made of honeycomb core with a skin made of aluminum sheet metal?. Leading edge. Flap box. Trailing edge. Tab.