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término definición
During VNAV PATH descent and below the Speed Restriction Altitude, the FMC Alerting Message OVERSPEED DISCONNECT means:
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VNAV has disengaged because airspeed has exceeded FMC Speed Restriction by more than 15 knots
Electrical power to start the APU comes from:-
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No. 1 transfer bus or the airplane main battery.
Elevator feel system is provided by the elevator feel computer. This computer receives inputs of:
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airspeed and stabilizer position
Engaging LVL CHG descent mode
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automatically engages the A/T in RETARD, and then ARM when thrust is at idle
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?
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No
Engine oil pressure is in the amber band at take-off thrust. Which of the following is true?
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Do not take-off
Entry or Cargo Doors should not be opened if the windspeed exceeds:
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40kt
Entry or Cargo Doors should not be opened if the windspeed exceeds:
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40 knots
Extending the airstairs using the STANDBY system on the Interior Panel:
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by-passes the handrail and lower ladder safety circuits
Extinguisher continuity can be tested by pushing and holding the
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EXT TEST switch
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?
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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
Failure of one temperature controller will be annunicated to the crew by
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“Zone Temp” On Master Caution recall
Failure of two temperature controllers will be annunicated to the crew by
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Illumination of the Master Caution
Fire extinguishers provide a means of extinguishing:
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only engine fire, cargo, APU fire and lavatory fires
Flight spoiler deflection is initiated on the down going wing when the control wheel is displaced more than approximately:
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10 degrees
Flight spoilers are operated:
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2 left wing and 2 right wing by system A, 2 left wing and 2 right wing by system B
For ground service, a GROUND SERVICE SWITCH is located:
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on forward attendant´s panel.
For ground servicing, a GROUND SERVICE Switch is placed:
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on the Forward Attendant ́s panel
For ground servicing, a GROUND SERVICE Switch is placed:
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on the Forward Attendant ́s panel
For landing, what is the maximum fuel imbalance between No. 1 and No. 2 main tanks?
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453 Kgs.
For landing, what is the maximum fuel imbalance between the No. 1 and No. 2 main tanks?
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453 Kgs
For RVSM operation, the maximum allowable altitude display difference for sea level, between the Captain and F/O's on the ground is?
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50 feet
From where does the Cabin Auto Controller get its inputs?
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From the ADIRUs.
Fuel for the APU is normally (AC fuel pumps operating) supplied from:
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The left side of the fuel manifold
Fuel for the APU is normally supplied from the:
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Left side of the fuel manifold.
Full rudder pedal displacement will turn the nosewheel by:
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7 degrees.
How can TOGA be selected for takeoff if both flight directors are OFF?
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Pressing TOGA after 80 knots and before 150 seconds after lift off.
How can VNAV be terminated?
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selecting a different pitch mode
How do you activate the APU fire extinguisher from the wheel well?
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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.
How do you set the Audio Control Panel to receive NAV and ADF voice and range audio?
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Set the Filter Switch to B (Both)
How is an APU bleed air duct leak annunciated in the flight deck?
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By the MASTER CAUTION, AIR COND and Left WING-BODY OVERHEAT lights
How is the accessory gearbox connected to the engine?
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It is mechanically linked to the N2 rotor
How is the cabin altitude warning horn silenced?
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By pushing the ALT HORN CUTOUT switch on the forward overhead panel.
How is the hard alternate mode entered?
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When in Soft Alternate mode, retard the thrust lever or push the EEC switch
How many fire extinguisher bottles are available for the APU FIRE protection system?
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1
How many fuel measuring sticks are installed?
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16
How many modes of control does the outflow valve have on the 737-800?
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Three. One manual and two automatic - 'AUTO - ALTN - MAN'
How many positive pressure relief valves are on the 737-800?
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2
How many pressure relief valves are fitted to provide safety pressure relief?
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2
How many spark igniters are there on each engine?
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2
How many times can the TRIP RESET button be used to reset a related system?
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Unlimited number of times
How much greater is the fluid volume supplied by an engine driven hydraulic pump, compared to the related electric motor-driven hydraulic pump?
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6 times greater.
Hydraulic system pressure indication on the lower DU is derived from:
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combined engine and electric pump outputs.
If 'ON DC' on left IRS Mode Selector Unit comes ON steady it means:
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the related IRS is operating on DC power from the switched hot battery bus
If a cowl anti-ice valve fails to move to the selected position:
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the COWL VALVE OPEN light remains illuminated bright blue
If a crossbleed start is recommended for inflight starting, where is the Magenta "X-BLD" Indication displayed?
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above the N2 dial
If a fire extinguisher is to be discharged on the flight deck:
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all crewmembers to wear oxygen masks with 'EMERG' selected
If a landing is made with RTO selected:
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AUTO BRAKE DISARM light illuminates 2 seconds after touchdown
If a leak develops in the supply line to System A engine-driven hydraulic pump, what approximate reservoir quantity would you expect?
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20% full
If a wet start is detected, when will the EEC automatically turn off ignition and shut off fuel to the engine?
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15 seconds after the start lever is moved to IDLE during ground starts
If a wheel spin-up signal is not detected on landing and the speed brake is ARMED, the flight spoilers will deploy automatically:
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When the Air/Ground system senses ground mode (any gear strut compresses).

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