TEST BORRADO, QUIZÁS LE INTERESE:
BOEING 767-300 APU, EMERGENCY, COMMUNICATION
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BOEING 767-300 APU, EMERGENCY, COMMUNICATION Descripción: BOEING 767-300 APU, EMERGENCY, COMMUNICATION Autor:
Fecha de Creación: 26/05/2021 Categoría: Otros Número Preguntas: 44 |
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Where is the switch that uses ground personnel to turns on the cockpit ground call light? (FCOM, 5.10.3, 5.30.1) A.- FWD cabin attendant panel. B.- APU ground control panel C.- AFT cabin attendant panel. . What is the function of the VHF TFR (transfer) switch? (FCOM, 5.10.4) A.- Transfer control between the left and right VHF comm radios. B.- Transfer control between the VHF comm radio and the VHF nav radio. C.- Controls which VHF communications frequency is to be used. What is controlled by the service interphone switch on the pilots accessory panel when is in ON position? (FCOM, 5.10.6) A.- The service interphone system. B.- Adds external (unpressurized area) headphone jacks to cabin interphone system. C.- The service interphone jacks located in pressurized areas. What does in the cabin interphone system pressing the ALERT switch on the pilot call panel (PCP) do? (FCOM, 5.30.2) A.- Causes the cabin call chime to sound continuously until a handset is picked up B.- Causes all the pink call light to flash until a handset is picked up. C.- Illuminates the calls lights and sounds a chime at all interior station except for the originating station. To erase a voice recorder, what conditions must be met? (FCOM,5.10.11) A.- Airplane on the ground, push and hold erase button. B.- Airplane on the ground, both engines shut down, pudh and hold erase button for 7 seconds. C.- Push and hold erase button and if the airplane on the ground, AC power on, parking brake is set. The flight interphone system can be used for communications between the cockpit and the ground personnel on the main landing gear strut. (FCOM, 5.30.1) A.- TRUE. B.- FALSE. The flight/cabin interphone system can be connected to: (FCOM,5.30.3) A.- The service interphone system. B.- All service in cabin crew stations C.- All service ground crew only. The flight attendants communicate between flight attendant stations with the flight deck using: (FCOM, 5.30.2) A.- Only the forward handset flight attendant station. B.- Any of the handset of the cabin. C.- Only the aft handset flight attendant station. One of the following methods is used to alert pilots to incoming calls from the cabin: (FCOM, 5.30.2) A.- Alert light flashes, bell sounds. B.- Alert light flashes. C.- An aural chime sounds in the flight deck. Flight deck crew members can make announcements with any microphone by: (FCOM, 5.30.3) A.- The ground personnel can make announcement to passenger from ground. B.- The flight deck crew members cannot use any microphone of flight deck. C.- Pushing the PA (Passenger address) transmitter select switch on an audio control panel. COMMUNICATIONS GRAPHIC 3: When the flight recorder is automatically activated on the ground? (FCOM, 10.30.12) A.- Either engine must be operating. B.- After both engines are started or inflight C.- After the ACARS out time is recorded. COMMUNICATIONS GRAPHIC 2: The SERV INTPH (service interphone) switch must be on to enable communications at what cabin/service interphone stations? (FCOM, 5.10.6) A.- Interior. B.- Exterior. COMMUNICATIONS GRAPHIC 1: What frecuency is the radio tuned to? A.- 120.6 B.- 118.3. Can communications with all flight crew members stations be established using an oxygen mask microphone? (FCOM, 5.20.1) A.- YES. B.- NO. Where are flashlights kept? (FCOM, 1.45.4) A.- In every lavatory. B.- On the aft wall of the forward lavatory. C.- At each flight attendant station. What are the passenger cabin emergency lights powered by? (FCOM, 1.40.4) A.- The airplane battery. B.- Each light has its own battery. C.- Remote batteries. The two emergency locator transmitters are located under the pilot's seats. (FCOM, 1.45.2) A.- TRUE. B.- FALSE. The passenger oxygen system uses the same source as the cockpit crew? (FCOM, 1.40.5) A.- TRUE. B.- FALSE. The passenger door evacuation slide/rafts are disarmed by. (FCOM,1.40.9) A.- Positioning the arming lever to the disarmed position. B.- Pressing the abort switch. C.- Resetting the slide dettachment handle. The lower EICAS display shows what oxygen pressure? (FCOM, 1.40.5) A.- Passenger oxygen pressure. B.- Cockpit crew pressure. C.- Flight attendant oxygen pressure. The flight deck number two windows can be open: (FCOM, 1.40.7) A.- on the ground or in flight. B.- only on the ground. C.- only in flight. The crew can escape from the cockpit using the cockpit window emergency pneumatic slide. (FCOM, 1.40.7) A.- TRUE B.- FALSE. If a fire extinguisher is to be discharged in the flight deck area, crew members must wear oxygen mask and use 100% oxygen with emergency selected. (FCOM, 1.45.1) A.- TRUE. B.- FALSE. EMERG. EQUIP GRAPHIC 2: Is the Pass Oxy switch in normal operation?(FCOM, 1.30.21) A.- True. B.- False. EMERGENCY EQUIP GRAPHIC: 4 This is the symbol for an exit path with slide/raft. (FCOM, 1.45.3) A.- TRUE. B.- FALSE. EMERGENCY EQUIP GRAPHIC: 3 What does the passenger oxygen switch status ON indicate? (FCOM,1.30.21) A.- The passenger oxygen system masks have dropped. B.- The oxygen light at the passenger seat are on C.- The passenger oxygen system is ready for pilot activation. EMERGENCY EQUIP GRAPHIC 2: When is the UNARMED light illuminate? (FCOM, 1.30.9) A.- The emergency lights switch is in the armed position. B.- The emergency lights illuminate when fault. C.- Illuminated (amber) – the emergency lighting system has been manually actuated or the emergency lights switch is OFF. EMERGENCY EQUIP GRAPHIC 1: Where is the Oxygen Flow Indicator? (FCOM, 1.30.22) A.- 1. B.- 2. C.- 3. Do not operate the cargo doors with winds at the door of more than 25 knots. (1.40.12) A.- True. B.- False. With the APU operating, what happens when the APU FAULT light illuminates? (FCOM, 7.42.1) A.- A normal shutdown sequence starts. B.- The APU has automatically shut down. C.- The APU fuel val eicas message also illuminates. Will the APU FUEL VAL advisory message (EICAS) be displayed during normal APU start and shutdown? (FCOM, 15.20.8) A.- Yes, the message is displayed for normal transit then extinguishes. B.- No, the message is inhibited on EICAS when the valve is in transit. Which of the following describes the start position of the rotating APU selector? (FCOM, 7.15.1) A.- The APU fuel valve opens and at the same time the APU inlet door begins to open. A fuel pump also begins to operate. Return to ON when released. B.- Latches, remains in start until moved. C.- Magnetically held until started cutout. When will moving the battery switch off cause the APU to shutdown? (FCOM, 7.30.2) A.- On the ground. B.- In flight. C.- On the ground and in flight. When in ground the APU RUN light illuminates, the APU may be used to supply: (FCOM, 7.30.2) A.- Electrical power and bleed air. B.- Only electrical power C.- Only hydraulics power. When does the APU cool down timing delay begin? (FCOM, 7.30.2) A.- When the APU generator trips off. B.- When the rotating APU selector is moved to off position. C.- When the rotating APU selector is moved to off position and bleed air valve closes. What the APU fault light indicate? (FCOM, 7.15.1) A.- An amber FAULT light on the APU control panel illuminates whenever a fault is sensed B.- alternative a) and c) are correct. C.- The FAULT light also comes on when the APU fuel valve is not in the commanded position. What is the minimum power needed to start and operate the APU? (FCOM, 7.30.1) A.- APU battery only. B.- APU start on ground requires both the APU battery and the aircraft main battery. C.- APU battery and ground handling buses. What is indicated by an illuminated fault light when the APU selector is off? (FCOM, 7.15.1) A.- The APU fuel valve disagrees with the commanded position. B.- APU fault only. C.- Either a fuel valve fault or an APU fault. What is cut off first when the APU selector is moved off? (FCOM,7.30.2) A.- Fuel. B.- APU Bleed air valve. C.- Generator output. What does the rotating APU selector when turned off? (FCOM, 7.30.2) A.- Opens APU bleed valve. B.- Begin the shut down cooling cycle by closing the APU bleed air valve. C.- Cuts off fuel. What does the APU run light indicate? (FCOM, 7.15.1) A.- APU generator is running. B.- APU selector in on. C.- APU is at operating speed. What does the APU FUEL VAL advisory message (EICAS) mean? (FCOM, 7.30.1) A.- The fuel valve did not close. B.- The APU fuel valve position disagrees with the commanded position. C.- The fuel valve did not open. The APU selector is moved from off to start and released to on. When does the electric starter engage? (FCOM, 7.30.1) A.- Immediately. B.- When the fuel valve has opened. C.- When the inlet door has opened. - How can an APU fault must be reset? (FCOM, 7.15.1) A.- Placing battery switch off. B.- Moving APU selector to start or off. C.- Only by moving APU selector to off. |
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