Boeing 777 Progress Test 2Home / Boeing 777 Progress Test 2 Boeing 777 Progress Test 2 Boeing 777 Progress Test 2 1 / 44 What is the V1 for this take-off? 131Kts 124Kts 130Kts 137Kts 2 / 44 What is the Assumed Temperature for this take-off? 42 c 18 c 46 c 14 c 3 / 44 What is the Take-off Performance Limit (TOPL) Weight for this take-off? 205,700Kgs 231,400Kgs 232,100Kgs 210,000Kgs 4 / 44 A final loadsheet showing ‘Compliance with’ indicates that the; MACTOW and MACZFW are within 4 percent of the provisional figure MACTOW and MACZFW are within 3 percent of the provisional figure TOW is within +5000Kg and -1000Kg TOW is within +1000Kg and -5000Kg 5 / 44 Which is the limiting Weight? Take-off Weight Taxi Weight Landing Weight Zero Fuel Weight 6 / 44 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? Nothing Primary power will connect to both buses Primary power will connect to the Right bus Primary power will connect to the Left bus 7 / 44 Inflight, what powers the Main and APU battery Chargers? Ground Handling Bus Left Transfer Bus Ground Service Bus Left Main AC Bus 8 / 44 When will an IDG automatically disconnect? When it is overheating When its drive shaft has failed When its AC Bus is not powered When its oil pressure is low 9 / 44 Inflight, what happens to the Right Transfer Bus if the right IDG fails? A Back-up Generator connects to the Right Transfer Bus It will be powered by the Static Inverter The left IDG powers the Right Transfer Bus via the Right Main AC Bus It will remain unpowered 10 / 44 What is the in-flight priority for powering the Main AC busses? APU, respective IDG and then opposite IDG Respective IDG, the opposite IDG and then the APU Respective IDG, APU and then the opposite IDG Respective IDG, OR opposite IDG and then the APU 11 / 44 If both Transfer Busses become unpowered, what initially supplies power to the DC system? The RAT Generator The Main Battery The Standby Inverter The APU Generator 12 / 44 What is the primary source of power for the Flight Control Buses? The Main Battery The Left and Right Transfer Buses C1 and C2 TRU’s The PMG’s 13 / 44 What is the primary power source for the First Officers’ Flight Instrument Bus? C1 TRU R TRU L TRU C2 TRU 14 / 44 After first engine start, the APU oil temperature rises above a certain limit. Which EICAS alert will be displayed? APU SHUTDOWN caution APU SHUTDOWN warning APU LIMIT caution APU LIMIT warning 15 / 44 When is the APU in Attended Mode? When an engine is started or running, or when the aircraft is in flight When the ground engineers are in attendance When the APU is starting When the pilots are on the flight deck 16 / 44 Which of the following conditions is required to start the APU? External electrical power must be connected Ground air supply must be connected Main tank L aft pump must be selected ON The Battery switch must be ON 17 / 44 In flight, the APU has started automatically. How would you shut the APU down? Through the menu key on the L/H CDU By positioning the APU selector ON then OFF By selecting the battery switch OFF It happens automatically on landing 18 / 44 Which tank provides fuel for the APU when the fuel pumps are off? Main tank Left The Centre tank Main tanks Left and Right Main tank Right 19 / 44 An APU can be used in flight for which of the following? Pneumatics only, up to 15,000ft Pneumatics and electrics up to 15,000ft Pneumatics up to 22,000ft, and electrics up to aircraft’s max certificated altitude Electrics only 20 / 44 How is fuel balancing completion indicated? A memo message FUEL BALANCED Solid white fuel balance arrows which flash for 10 seconds FUEL BALANCED replaces FUEL QTY on the Expanded Fuel Quantity display, and flashes for 5 seconds An advisory FUEL BALANCED message 21 / 44 Why would the fuel balance pointer flash when carrying out fuel balancing? The fuel balancing is going in the wrong direction The main tank fuel differs by more than 500Kgs The main tank fuel differs by more than 100Kgs and a cross-feed valve is open The fuel balancing is complete 22 / 44 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? Start the engines using the main tank pumps only Consult the MEL for dispatch criteria None, this is normal Carry out the procedure in the QRH 23 / 44 During which phase of flight can fuel balancing be carried out? In any phase of flight In the holding pattern Climb and descent Cruise Phase only 24 / 44 When will the expanded fuel indications automatically appear? By selected FUEL on the display select panel By selecting ENG on the display select panel With one or both cross feed valves open With one electrical power source and both centre tank pumps on 25 / 44 During flight, what do the fuel TOTALIZER and CALCULATED quantities represent on FMC Progress Page 2? Fuel in the tanks at take-off and the fuel used since take-off Current fuel quantity in the tanks and the FMC calculated fuel remaining The difference between Main and Centre Tank fuel Fuel quantity, and the fuel used by the engines 26 / 44 Where is the Fuel Tank Temperature indicated? The EICAS and Fuel synoptic The CDU’s Secondary EICAS display The overhead panel 27 / 44 During Fuel Jettison, where is the ‘Jettison Time’ displayed? FMS PROG page 2 STATUS Fuel synoptic EICAS 28 / 44 If the Engine START/IGNITION control switch is at CON, when will the ignitors operate? At all times Continuously if the FUEL CONTROL SWITCH is at RUN Only during starting Only if the wing anti-ice is ON 29 / 44 How is APPROACH idle selected? Automatically if that engine bleed air switch is OFF Manually adjusted to 5% above normal idle If a hydraulic pump fails with flap UP Automatically with flap selection of 25 degrees or more 30 / 44 During a normal Autostart, placing the FUEL CONTROL switch to RUN will do what? It opens the fuel spar valve and arms the engine fuel valve and the ignitors It opens all fuel valves and switches on the ignitors It will open the engine fuel valve and arms the ignitors It arms both the spar and engine fuel valves and the ignitors 31 / 44 Why are the thrust levers moved to the mid position before selecting Alternate Mode on the EEC? To prevent… autothrottle re-engagement N1 overspeed Engine surges Thrust overboost 32 / 44 Following an engine start, what does the EICAS Caution message ‘ENG START CUTOUT L’ indicate? The start cycle is complete The Bleed Air Valve has failed to close The engine has achieved ‘max motoring’ The Start Valve is open when commanded closed 33 / 44 When will Auto-Relight operate? When turbulence is detected When engine overboost is detected At glideslope capture When rapid N2 deceleration is sensed 34 / 44 Following an in-flight engine shutdown, where is the in-flight start envelope displayed? On the EICAS display By the N2 indicator on the Secondary Engine Indications On the ENG OUT CRZ page on the CDU On the Air Synoptic 35 / 44 How can an EGT exceedance be recalled? By pressing the CNL/RCL button on the display select panel By pressing the EICAS Event-Record Switch. By selecting the EEC Mode switch to ALT. By pushing the status switch on the Display Select Panel. 36 / 44 During a twin-engine autoland, when does the initial runway alignment manoeuver begin G/S Capture 1000RA 500RA 1500RA 37 / 44 When is the Go-around function of TO/GA mode armed? When APCH is armed On LOC capture On G/S capture If 1700RA is passed on the descent 38 / 44 What is the Autothrottle FMA annunciation during a VNAV SPD Climb? IDLE SPD THR THR REF 39 / 44 What does the V/S window display on V/S engagement? Current V/S Remains Blank A magenta bug Zero 40 / 44 If the Autothrottle is in V/S mode, what is the Autothrottle FMA annunciation? HOLD SPD THR REF THR 41 / 44 When will VNAV mode disengage? As the LOC is captured. If Autothrottle is disconnected. When the MCP windowed altitude is reached. If FLCH is selected. 42 / 44 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? VNAV SPD VNAV ALT VNAV PTH VNAV 43 / 44 If armed, at what height will VNAV engage during take-off? 200ft 50ft 100ft 400ft 44 / 44 On a normal take-off, what will be the autothrottle mode after 80kts? THR HOLD SPD THR REF Your score is