Boeing 777 Progress Test 2
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What is the V1 for this take-off?
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What is the Assumed Temperature for this take-off?
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What is the Take-off Performance Limit (TOPL) Weight for this take-off?
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A final loadsheet showing ‘Compliance with’ indicates that the;
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Which is the limiting Weight?
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If a single IDG is powering both buses, what will occur if the Primary EXT power switch is pressed with the Primary EXT power available?
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Inflight, what powers the Main and APU battery Chargers?
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When will an IDG automatically disconnect?
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Inflight, what happens to the Right Transfer Bus if the right IDG fails?
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What is the in-flight priority for powering the Main AC busses?
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If both Transfer Busses become unpowered, what initially supplies power to the DC system?
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What is the primary source of power for the Flight Control Buses?
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What is the primary power source for the First Officers’ Flight Instrument Bus?
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After first engine start, the APU oil temperature rises above a certain limit. Which EICAS alert will be displayed?
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When is the APU in Attended Mode?
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Which of the following conditions is required to start the APU?
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In flight, the APU has started automatically. How would you shut the APU down?
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Which tank provides fuel for the APU when the fuel pumps are off?
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An APU can be used in flight for which of the following?
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How is fuel balancing completion indicated?
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Why would the fuel balance pointer flash when carrying out fuel balancing?
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During push back, on APU power before engine start, with all Fuel Pumps ON, you notice the Centre Tank R pump PRESS light is illuminated. What action is required?
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During which phase of flight can fuel balancing be carried out?
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When will the expanded fuel indications automatically appear?
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During flight, what do the fuel TOTALIZER and CALCULATED quantities represent on FMC Progress Page 2?
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Where is the Fuel Tank Temperature indicated?
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During Fuel Jettison, where is the ‘Jettison Time’ displayed?
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If the Engine START/IGNITION control switch is at CON, when will the ignitors operate?
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How is APPROACH idle selected?
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During a normal Autostart, placing the FUEL CONTROL switch to RUN will do what?
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Why are the thrust levers moved to the mid position before selecting Alternate Mode on the EEC? To prevent…
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Following an engine start, what does the EICAS Caution message ‘ENG START CUTOUT L’ indicate?
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When will Auto-Relight operate?
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Following an in-flight engine shutdown, where is the in-flight start envelope displayed?
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How can an EGT exceedance be recalled?
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During a twin-engine autoland, when does the initial runway alignment manoeuver begin
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When is the Go-around function of TO/GA mode armed?
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What is the Autothrottle FMA annunciation during a VNAV SPD Climb?
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What does the V/S window display on V/S engagement?
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If the Autothrottle is in V/S mode, what is the Autothrottle FMA annunciation?
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When will VNAV mode disengage?
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During a VNAV climb, the aircraft levels off at an intermediate altitude which has been selected on the MCP. What will the FMA pitch mode annunciation be?
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If armed, at what height will VNAV engage during take-off?
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On a normal take-off, what will be the autothrottle mode after 80kts?
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