Boeing B777 - Air Systems
During climb, what parameter(s) schedule cabin altitude?
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When is the pack OFF light illuminated amber?
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Two outflow valves are installed: one forward and one aft. Normally, most of the outflow is through the forward outflow valve.
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This improves ventilation and smoke removal. Cabin altitude and full ventilation rates can be maintained by either valve.
What happens if the FLT DECK TEMP control is moved to the 'C' position?
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Which of the following is false for the PACK Switch illuminating OFF?
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What does the PACK MODE R EICAS message indicate?
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The cabin altitude limiter closes both outflow valves if cabin altitude exceeds:
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How many packs are there and what is their main function?
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What must be done to manually set a landing altitude?
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Which system(s) supply trim air to the flight deck?
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During preflight, what position should the FWD and AFT OUTFLOW VALVE switches and LDG ALT selector be in?
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Which of the followings are bleed air sources?
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Landing altitude (normally provided by the FMC) can be manually set using the LANDING ALTITUDE selector. Landing field selection limits are _____ below sea level to _____ feet above sea level.
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Where does air to the cabin come from, and what are the additional sources?
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If the cruise altitude is unavailable from the FMC in AUTO, the cabin altitude controllers assume a cruise altitude of 39,000 feet.
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What is the normal position of the forward outflow valve after landing?
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Why should you minimize flight time at low altitude when the EQUIP COOLING OVRD message is displayed?
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When does a visible orange lip indicate on a pressure relief valve?
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If a pack overheats or fails the pack shuts down and an air conditioning may be needed.
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After engine start, what is the correct position for the L ENG and R ENG BLEED AIR switches?
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Why should the CABIN TEMP control be set to mid position?
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During normal bleed air operation, what position should the L, C, R ISLN BLEED AIR switches be in?
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What cabin differential pressure is scheduled for takeoff?
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Whic trim air valve can be moved directly by the flight crew, and how is it monitored?
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What does the MAN position on the FLT DECK TEMP control do?
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How are cargo compartments controlled in terms of temperature ranges?
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Where is the target temperature for the air conditioning zones displayed?
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What is the most correct statement about the equipment cooling override mode?
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If cruise altitude is unavailable from the FMC in AUTO, the cabin altitude controllers assume a cruise altitude of:
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What is the source of supplemental heat for the aft cargo compartment?
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What is the function of the negative pressure relief vents?
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Which component can be reset by the air conditioning reset switch.
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What happens when you select the FWR CARGO A/C control to AUTO?
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What is bleed air used for?
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If an overheat or other significant pack fault is detected, the pack shuts down automatically. An attempt to restore pack operation may not be made by pressing the AIR COND RESET switch.
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How are zone target temperatures selected, and what is the temperature range?
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What system provides the heat for the forward cargo compartment?
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Forward Equipment Cooling system does not reconfigure automatically to override mode automatically for which of the following?
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When is the center bleed isolation valve open?
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In the cabin altitude controller cruise mode, maximum cabin altitude is 8,000 feet. The cabin altitude controllers enter cabin altitude controller descent mode at T/D or at initial descent of approximately _____ from cruise altitude, regardless of T/D.
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Which of the following are landing elevation limits for B777?
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What happens when the BULK CARGO TEMPERATURE selector is positioned to HIGH?
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What will cause the automatic closure of a bleed valve?
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What is the indication that an outflow valve is in manual control?
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What happens if the forward equipment cooling primary supply fan fails?
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During preflight, what position should the APU BLEED AIR switch be in?
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Flight Deck Temperature (FLT DECK TEMP) selector in mid position sets the temperature to approximately 75°F (24°C)
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If a duct leak is detected, the system automatically isolates the leak. The EICAS caution message BLEED LEAK is displayed. The automatic isolation logic may include:
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During isolation, the ENGINE and/or APU bleed switch OFF lights and the ISOLATION switch CLOSED lights illuminate and extinguish as the repective valves close and open.
In the standby cooling mode, what will the pack automatically do if the airplane is not in an area of sufficient cooling?
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The controller uses ambient pressure and flight plan data from the FMC to calculate a cabin pressurization schedule. The schedule provides a comfortable cabin climb to cruise altitude.
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What action is required during preflight if the LANDING ALTITUDE EICAS message is displayed with the FWD and AFT OUTFLOW VALVE switches in AUTO?
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The LANDING ALTITUDE advisory message indicates which of the following?
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With the CARGO TEMPERATURE selector set to LOW or HIGH, the respective cargo heat shutoff valve opens and the temperature control valve opens and closes to maintain the temperature in the compartment.
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If one pack is in standby cooling and the other pack is operating normally, the pack in standby cooling mode shuts down at lower altitudes and higher outside air temperatures when ambient conditions do not permit standby cooling.
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What causes the trim air FAULT light to come on?
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Why should you minimize flight time at low altitude when the EQUIP COOLING OVRD message is displayed?
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The aft and bulk cargo compartments have independent bleed air heating systems. An insulated curtain separates the two compartments.
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What is the normal source of bleed air to start the second engine?
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Each trim air system supplies three zone supply ducts, with the left trim air system also supplying the flight deck.
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What protects the fuselage against excessive differential pressure?
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In flight, the normal source of bleed air for all systems except the engine anti-ice is the engine low stage compressor (at high power) or intermediate stage compressor (at low power).
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What is the cabin altitude at maximum certified airplane operating altitude?
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In flight, the cabin altitude controller operates in:
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For Boeing 777, the APU Bleed Air is available at all altitudes.
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Automatic ventilation of the Forward Cargo Compartment Air Conditioning System ensures that smoke and objectionable odors do not enter the flight deck or passenger cabin.
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If landing altitude is unavailable from the FMC (and not set in MAN), the EICAS advisory message LANDING ALT is displayed. The cabin altitude controller:
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Why does the flight deck receive air from the left pack at a higher pressure than the passenger cabin?
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When does the ground crew call horn sound?
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What landing altitude is displayed on the EICAS pressurization system indications when the airplane has traveled more than 400 miles or has passed the halfway point?
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How does the trim air system meet zone temperature requirements?
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What determines the pack outlet temperature?
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Boeing B777 – Air Systems