B767 AE

Where are the passenger oxygen masks located?. On the individual mask storage modules, above each seat group. On the individual mask storage modules, below each seat group. Oxygen masks are distributed by the flight attendants in case of emergency.

How the pilots engage the autopilot and make the different autoflight mode selection: By a switch on the control wheel. By the CDU "Execute" switch. By the AFCS mode control panel.

What service or services may provide the APU: Pneumatic and electrical power. Electrical power only. Pneumatic power only.

How can the yaw movement be manually controlled?. By the rudder pedals. By the control wheels. By the control columns.

Which of the following are the primary flight controls: Flaps, slats and the horizontal stabilizer. Speedbrakes, flaps and the yaw damper. Aileron, rudder, elevator and spoiler system.

What is the primary source of power for the left and right hydraulic systems: The Engine Driven Pumps (EDP). The Air Driven Pumps (ADP). The AC electric pumps (ACMP).

How the waste is disposed on the Boeing 767: Toilet waste is stored in a toilet tank in each lavatory, containing a chemical solution. By a vacuum system that throws to the exterior the waste generated. By two independent vacuum toilet systems that stores the waste in two tanks.

How can we control and monitor the bleed system on the flight deck?. Through the overhead Bleed Air Supply panel. Through mechanical push-pull cables on the front panel. Via Control Display Unit, on the bleed system menu.

Where does the NGS take the air from?. From the bleed air manifold. A dedicated air compressor. From the RAM inlet door.

By connecting headsets, are we able to establish communication between the APU compartment and the right wheel well?. No; it is not possible to establish direct communication between service compartments. Yes; through the Passenger Address jacks located on those areas. Yes; through the Service Interphone jacks located on those areas.

What is the purpose of the Passenger Address (PA) system: To allow the passengers to make phone calls from the aircraft to the ground. To allow the flight crew to transmit speech communications to the Air Traffic Control. To allow the flight crew or flight attendants to transmit announcements to the passengers.

What system provides an interface between the pilots and all internal or external means of communication: The Cabin Interphone system. The Voice Recorder system. The Flight Interphone system.

Which are the fuel tanks on the B767: Left Main, Right Main and Center Auxiliary tanks. Right Main, Left Main and Horizontal Stabilizer auxiliary tanks. Left Main and Right Main tanks, with no auxiliary tank.

What power sources supply AC electrical power for airplane ground operations: The external power or the auxiliary power unit (APU) generator. Left and right engines Integrated Drive Generators (IDGs). Both main battery and auxiliary battery through the static inverter.

How many Control Display Units (CDU) are located on the flight deck: Three; left, right and center for the first observer. Two; left for the captain and right for the first officer. There is only one CDU on the center of the pedestal.

What system provides the pilots with a visual indication of weather conditions in order to avoid heavy precipitation or turbulence: The Flight Management System. The Weather Radar System. The Ground Proximity Warning System.

Which system is used to calculate an accurate airplane position and time by using navigation satellites: The Air Data Computer (ADC). The Global Positioning System (GPS). The Inertial Reference System (IRS).

How may the pressurization system be controlled: In automatic mode only. In manual mode only. In automatic and manual modes.

The term "WARNING" is used on the AMM to call attention about: Methods and procedures which must be followed precisely to avoid damage to equipment. Use of material, processes, methods, procedures or limits which must be followed to avoid injury or death to persons. Methods which make the job easier or provide supplementary or explanatory information.

GE CF6) Where is the engine oil stored?. Into the oil tank. Inside the engine gearbox. Along the oil tubing.

GE CF6) How the mixture of air and fuel is ignited on the combustor?. By entering into contact air and fuel. By two Igniter plugs in the combustor. By increasing the air pressure.

GE CF6) Which is the engine component that meters the fuel that is delivered to the Combustor?. The IDG fuel/oil heat exchanger. The Hydromechanical Unit (HMU). The Pressure Regulating Valve (PRV).

Which lights located on the fuselage, are high intensity Xenon strobe lights and flash 48 Times per minute. The red and green Position lights. The Landing and Runway Turnoff lights. The Anti-Collision Lights.

When does the Cargo Compartment Fire Alarm sound: When an overheat is detected on any of the Cargo Compartments. When smoke is detected on any of the Cargo Compartments. If any of the Cargo Compartment fire extinguisher bottles has discharged.

PW 4000) Which are the different Engine Start System air sources?. Ground air, APU air and engine air. From either, left or right engine air. A dedicated start air compressor and APU air.

(PW 4000) Which system heats the fuel, and cools engine oil and IDG oil?. The compressor airflow control. The fuel/oil cooling system. The bleed air system.

(PW 4000) Which component controls the fuel flow through the FMU and protects the engine?. The Flight Management Computer (FMC). The Electronic Engine Controls (EEC). The Fuel Metering Unit (FMU) itself.

Which system recordss flight parameters on magnetic tape for the purpose of providing information on flight conditions and airplane systems operation for analysis in the event of a crash or accident?. The Flight Data Recorder system. The Aircraft Condition Monitoring system. The Cockpit Voice Recorder system.

Which windows can be opened from inside the flight compartment: None of the windows can be opened. All the windows can be opened. The number two window on each side.

Which flight control surfaces are attached to the horizontal stabilizer: The elevators. The ailerons. The rudder.

What system allows passengers to escape through passenger entry/service doors in an emergency: The emergency flexible hanging ladders. The escape ropes fitted on each door frame. The door-mounted escape slide/rafts.