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During VNAV PATH descent and below the Speed Restriction Altitude, the FMC Alerting Message OVERSPEED DISCONNECT means: start learning
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VNAV has disengaged because airspeed has exceeded FMC Speed Restriction by more than 15 knots
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Electrical power to start the APU comes from:- start learning
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No. 1 transfer bus or the airplane main battery.
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Elevator feel system is provided by the elevator feel computer. This computer receives inputs of: start learning
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airspeed and stabilizer position
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Engaging LVL CHG descent mode start learning
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automatically engages the A/T in RETARD, and then ARM when thrust is at idle
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Engine number 1 bleed switch is in the ON position but the engine is not running. Will the number 1 bleed air valve be open? start learning
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Engine oil pressure is in the amber band at take-off thrust. Which of the following is true? start learning
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Entry or Cargo Doors should not be opened if the windspeed exceeds: start learning
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Entry or Cargo Doors should not be opened if the windspeed exceeds: start learning
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Extending the airstairs using the STANDBY system on the Interior Panel: start learning
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by-passes the handrail and lower ladder safety circuits
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Extinguisher continuity can be tested by pushing and holding the start learning
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F/D Go-around. If both autopilots are not engaged, a manual F/D only go-around is available under which of the following conditions? start learning
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Inflight below 2000ft RA, Inflight above 2000ft RA with flaps not up or G/S captured and not in takeoff mode
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Failure of one temperature controller will be annunicated to the crew by start learning
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“Zone Temp” On Master Caution recall
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Failure of two temperature controllers will be annunicated to the crew by start learning
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Illumination of the Master Caution
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Fire extinguishers provide a means of extinguishing: start learning
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only engine fire, cargo, APU fire and lavatory fires
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Flight spoiler deflection is initiated on the down going wing when the control wheel is displaced more than approximately: start learning
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Flight spoilers are operated: start learning
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2 left wing and 2 right wing by system A, 2 left wing and 2 right wing by system B
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For ground service, a GROUND SERVICE SWITCH is located: start learning
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on forward attendant´s panel.
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For ground servicing, a GROUND SERVICE Switch is placed: start learning
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on the Forward Attendant ́s panel
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For ground servicing, a GROUND SERVICE Switch is placed: start learning
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on the Forward Attendant ́s panel
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For landing, what is the maximum fuel imbalance between No. 1 and No. 2 main tanks? start learning
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For landing, what is the maximum fuel imbalance between the No. 1 and No. 2 main tanks? start learning
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For RVSM operation, the maximum allowable altitude display difference for sea level, between the Captain and F/O's on the ground is? start learning
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From where does the Cabin Auto Controller get its inputs? start learning
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Fuel for the APU is normally (AC fuel pumps operating) supplied from: start learning
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The left side of the fuel manifold
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Fuel for the APU is normally supplied from the: start learning
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Left side of the fuel manifold.
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Full rudder pedal displacement will turn the nosewheel by: start learning
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How can TOGA be selected for takeoff if both flight directors are OFF? start learning
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Pressing TOGA after 80 knots and before 150 seconds after lift off.
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How can VNAV be terminated? start learning
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selecting a different pitch mode
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How do you activate the APU fire extinguisher from the wheel well? start learning
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Pull the T-handle down to arm the system, then move the discharge switch to the left position to fire the squib.
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How do you set the Audio Control Panel to receive NAV and ADF voice and range audio? start learning
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Set the Filter Switch to B (Both)
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How is an APU bleed air duct leak annunciated in the flight deck? start learning
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By the MASTER CAUTION, AIR COND and Left WING-BODY OVERHEAT lights
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How is the accessory gearbox connected to the engine? start learning
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It is mechanically linked to the N2 rotor
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How is the cabin altitude warning horn silenced? start learning
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By pushing the ALT HORN CUTOUT switch on the forward overhead panel.
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How is the hard alternate mode entered? start learning
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When in Soft Alternate mode, retard the thrust lever or push the EEC switch
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How many fire extinguisher bottles are available for the APU FIRE protection system? start learning
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How many fuel measuring sticks are installed? start learning
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How many modes of control does the outflow valve have on the 737-800? start learning
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Three. One manual and two automatic - 'AUTO - ALTN - MAN'
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How many positive pressure relief valves are on the 737-800? start learning
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How many pressure relief valves are fitted to provide safety pressure relief? start learning
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How many spark igniters are there on each engine? start learning
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How many times can the TRIP RESET button be used to reset a related system? start learning
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Unlimited number of times
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How much greater is the fluid volume supplied by an engine driven hydraulic pump, compared to the related electric motor-driven hydraulic pump? start learning
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Hydraulic system pressure indication on the lower DU is derived from: start learning
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combined engine and electric pump outputs.
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If 'ON DC' on left IRS Mode Selector Unit comes ON steady it means: start learning
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the related IRS is operating on DC power from the switched hot battery bus
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If a cowl anti-ice valve fails to move to the selected position: start learning
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the COWL VALVE OPEN light remains illuminated bright blue
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If a crossbleed start is recommended for inflight starting, where is the Magenta "X-BLD" Indication displayed? start learning
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If a fire extinguisher is to be discharged on the flight deck: start learning
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all crewmembers to wear oxygen masks with 'EMERG' selected
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If a landing is made with RTO selected: start learning
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AUTO BRAKE DISARM light illuminates 2 seconds after touchdown
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If a leak develops in the supply line to System A engine-driven hydraulic pump, what approximate reservoir quantity would you expect? start learning
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If a wet start is detected, when will the EEC automatically turn off ignition and shut off fuel to the engine? start learning
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15 seconds after the start lever is moved to IDLE during ground starts
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If a wheel spin-up signal is not detected on landing and the speed brake is ARMED, the flight spoilers will deploy automatically: start learning
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When the Air/Ground system senses ground mode (any gear strut compresses).
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