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General fam Boing 777
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Título del Test:
General fam Boing 777 Descripción: Examen Autor: Tito peña OTROS TESTS DEL AUTOR Fecha de Creación: 28/07/2023 Categoría: Personal Número Preguntas: 40 |
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Variable stator vane (VSV) operates using Pneumatic Hydraulic Fuel. What is the main indication for engine thrust on the Trent 800? Engine pressure ratio (EPR) Brake horsepower (BHP) N1. Rolls Royes engines are High bypass, single shat, axial flow High bypass, triple shat, axial flow High bypass, twin shaft, axial flow . What type of engine starter is used on the Trent engine? Pneumatic starter Electrical starter Hydraulic starter. When do the emergency lights operate? When normal lights fail When normal power sources are not available When the pilot declares an emergency. When standby power switch is selected in auto Standby power provide power to the entire aircraft system Standby electric power system under generator control units control Standby electrical power system under ELMS control . Which air data sensor is not anti-iced? Left and right Angle of Attack (AoA) Total Air Temperature (TAT) Static ports. Overhead Flight Crew Rest (OFCR) area air condition exhaust air duct is connected to: Overhead flight crew rest ventilation system Passenger cabin circulation system Lav/galley ventilation system. Where are the lavatory galley fans located? Aft of bulk cargo compartment Behind aft cargo fwd. bulkhead Aft galley ceiling panel. What happens when the engine fire switch is pulled? Hydraulic pump depressurized Hydraulic fluids return to reservoir Hydraulic pumps continue operation. Where is engine fire extinguisher bottle located? Engine pylon Fwd. cargo bay Landing gear wheel well. One of many functions of Engine Fire detection system is. Measures nacelle temperature Gives a light indication in the flight deck Gives aural warning of fire on engine. When does the read light overfill indication illuminate? Fuel tank unbalanced quantity Fuel in the surge tank or overfill test in progress Fuel spill overboard from either tank. Passenger oxygen mask release automatically when Crew activates the automatic mask drop Airspeed < 80 knots and cabin altitude above 13,500 feet Airspeed > 80 knots and cabin altitude above 13,500 feet . What does the engine anti-ice system do? Head the leading edge of the engine inlet cowls to prevent ice collecting on them Head the engine fan blades to prevent ice collecting on them Head the leading edge of the engine inlet cowls to remove ice from them. . What does AIMS stand for? Aircraft Interface Management System Airplane Interface management System Airplane Information management System. In what way is the water drained from the water storage and distribution Fwd. system drain valve, Mid system drain valve , tank drain valve Fwd. system drain valve, aft system drain valve, tank drain valve Fwd. system drain valve, Mid system drain valve, aft system drain valve. What controls the ignition system? The Engine electronic control (EEC) The ignition switch in the cockpit Ignition exciter. How is the continuous ignition selected Automatic via EEC Only single ignition allowed Manually by crew. The MAT communicates with Central Maintenance Computer Functions in AIMS cabinets via 2 fiber optic interfaces 1 fiber optic interfaces 3 fiber optic interfaces. What is GE 90 thrust ratio? 20:80 50:50 30:70. When is the engine electronic controller (EEC) powered by the aircraft power? Always powered by the aircraft When the engine is not running When the engine is running. What is purpose of the back drive actuators? To provide the flight crew with visual tactile indication of the performance of the autopilot flight director system Convert the electrical signals from the autopilot flight director system into command signals to the flight controls To provide the flight crew with and artificial feel of the performance of the autopilot flight director system. What power the Integrated Refueling Panel (IRP) when the power switch is in the battery position? Hot battery bus Aircraft electric power system Aircraft main battery. Where are the APU speed sensors and inlet temperature sensor located? On the bottom of APU Top of APU On the side of APU. What does the passenger door emergency power assist (EPAS) system do? Helps to open the passenger door in an emergency Assists in the normal opening and closing of the passenger door Helps deploy the emergency escape slide. What type of doors are the passenger and service doors? Plug type doors Swing type doors Slide out doors. Where can the PMAT receptacles be found? Panel 40 Main leg P20 second observer panel Inside Stabilizer jack access door. How is the fuel supply that flows to the combustor controlled? By the EEC, which controls the metering valve in the fuel metering unit (FMU) By the thrust lever angle resolver, which sends an electric signal to the fuel metering unit (FMU) Directly by a cable from the thrust levers to the fuel metering unit (FMU). How is the PW4000 started? Electric starter Pneumatic starter Hydraulic starter. What type of thrust reverser is fitted to the PW400? Hydraulically powered and electrically operated Pneumatically powered and electrically operated Electrically powered and operated. Thrust Reverser Actuation System (TRAS) moves t/R sleeves by using Hydraulic power Pneumatic power Fuel power. Which airflow passes through the engine compressor, and turbine? Primary and secondary airflow Secondary airflow Primary airflow . Which flight management system CDU is used as the interface of the passenger address/cabin interphone (PA/CI) controller? None Center CDU All CDUs. What is displayed on the integrated standby flight display? Altitude and speed Attitude and speed Attitude, Airspeed, Altitude. Cargo heating is controlled by Environmental control system miscellaneous card (ECSMC) Equipment cooling controllers (ECC) Cabin Temperature Controller (CTC). What is used to prevent incorrect connection of the rigid tubing that connects the fire bottles to the check valves? Different colour code tube between engine 1 and engine 2 Different fitting diameter engine 1 and engine 2 Quick release connection with different fitting for both engines. Ram Air Turbine generates continuous supply of: 90 kva 20 kva 7.5 kva. When the Vertical Navigation (VNAV) mode is active it will be shown on Navigation display (ND) Both Primary flight Display (PFD) and Navigation Display (ND) Primary Flight Display (PFD). The ADIRU can be switched off with the ADIRU switch and will only go off when Ground speed <20 kts Ground speed >30 kts Computed Airspeed <40 kts . |
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