sistemas semestre 2

The Extinguisher TEST switch can test the circuitry (NG). to the squibs on all three bottles. to the detector loops.

Weather radar and TCAS can be displayed in the mode.(NG). expanded MAP only. center MAP only. expanded MAP and Center MAP.

Which key is used to remove messages or data from the scratchpad ?(NG). CLEAR. DELETE.

The FIRE WARNING lights and the bell can also be cancelled by pressing the switch on the Aft Electronics Panel.(CL). "BELL CUTOUT". EXTERNAL FIRE POWER.

Overheat Detection occurs if both loops detect an overheat; or one detects an overheat and the other detects a or if one loop detects an overheat and the other has a fault; or if only one is selected and the selected loop detects an overheat.(CL). loss of engine thrust. fire.

The APU bottle has external blow out discs located on the AFT - side of the aircraft.(NG). left. right.

The wheel well system monitors fire conditions, but does not monitor conditions.(CL) or fault. overheat. power.

Each Loop Selector switch is usually in the NORMAL position. If loop "A" or "B" is selected and loop is defective, the amber light indicates the selected engine loop has failed.(CL). Fault. Inop.

The MAP mode is displayed in a orientation.(NG). Track Up. Heading Up.

The MASTER CAUTION lights illuminate when the amber illuminate on the Aft Electronics Panel.(NG) - or APU DET INOP lights. ENG OVERHEAT. ENG FIRE.

If the Loop Selector is in the Both position and a single loop fault is detected, the FAULT Light will not come on. Single loop mode is automatically selected (NG). True. FALSE.

Since there is no overheat detection for the APU, the APU switch will automatically(NG). unlock only if a fire is sensed. unlock if either an overheat or a fire condition is sensed.

With VNAV engaged, the Cruise mode automatically engages when(NG). the aircraft reaches the planned cruise altitude. the aircraft reaches the MCP altitude.

Using the FMS, how do you get the aircraft to enter a holding pattern at a fix that is already on route?(NG). You have to enter the holding pattern fix on the LEGS page as a waypoint. Just tune in the Desired VOR and press the HOLD key.

With VNAV engaged, the Cruise mode automatically engages when (NG). the aircraft reaches the planned cruise altitude. the aircraft reaches the MCP altitude.

A modification that requires a waypoint change will be made to which CDU page?(NG). LEGS. RTE.

If the VNAV mode is engaged and you are climbing in the MAX ANGLE CLB mode, what VNAV mode will engage when you reach the plan altitude at the top of climb? (Hint: You have not changed the speed on any cruise page).(NG). MACH .760 CRZ. ECON CRZ.

What is normally selected to exit the holding pattern and continue along the prescribed route? (NG). Press the EXIT HOLD prompt. Press the HOLD key.

(associated with the APU extinguisher bottle) can be viewed by the pilot during the external preflight inspection. (NG). Two colored discs. One colored disc.

Which Descent mode is the default mode? (NG). ECON PATH DES. ECON SPEED DES.

If the VNAV mode is engaged and you are climbing in the MAX ANGLE CLB mode, what VNAV mode will engage when you reach the plan altitude at the top of climb? (Hint: You have not changed the speed on any cruise page). (NG). ECON CRZ. MACH .760 CRZ.

Which key is used to remove messages or data from the scratchpad. CLEAR. DELETE.

The MASTER CAUTION lights illuminate when the amber illuminate on the Aft Electronics Panel. (NG) - or APU DET INOP lights. ENG OVERHEAT. ENG FIRE.

If both loops on one engine are malfunctioning when the OVHT/DET switch is in the NORMAL position - the _(CL). "FAULT" light illuminates only during recall. "FAULT" light illuminates.

The Standby Airspeed Indicator and Standby Altimeter are displayed on the panel.(CL) instrument. Center. Captain's.

If the Loop Selector is in the Both position and a single loop fault is detected, the FAULT light will not come on. Single loop mode is automatically selected.(NG). True. False.

The FIRE WARNING lights and the bell can also be cancelled by pressing the switch on the Aft Electronics Panel.(CL). EXTERNAL FIRE POWER. "BELL CUTOUT".

What is the maximum operating FL altitude of the APU?. FL330. FL370.

The APU start cycle can take up to __ seconds. 120. 130.

When a Manual mode is selected. the green MANUAL light illuminates. the manual AC motor starts running. the manual DC motor starts running. the AC motor is disabled.

The airflow through the cold mix valve is delivered to the. secondary heat exchanger. water separator. turbine. compressor.

If the aircraft is climbed higher than planned, the system will maintain the cabin altitude differential of until level flight is reached. 7.9 psid. 8.03 psid. 7.25 psid. 7.45 psid.

An amber OFF SCHED DESCENT light illuminates if the airplane begins to descend. without setting the landing altitude in the window. without reaching the planned cruise altitude. for the landing airport. more than 120 miles from the destination.

Single engine performance is calculated to be dangerous with a pack in HIGH. TRUE. FALSE.

The forward outflow valve is the overboard discharge exit for air circulated around the. forward cargo compartment. mid cabin. full cabin. rear cargo compartment.

Which pack normally delivers conditioned air to the cabin?. RIGHT. LEFT. NEITHER. BOTH.

During isobaric cruise, minor airplane excursions from flight altitude may cause the pressure differential to go as high as________to maintain a constant cabin altitude. 8 psid. 8.9 psid. 8.45 psi. 7 psid.

The APU Bleed Air Valve also functions as a give priority to the delivery of electrical power. Pneumatic switch. Exhaust. Emergency release valve. Load Control Valve.

In the manual mode, the pilot must manually move the outflow valve. TRUE. FALSE.

How many equipment cooling fans are installed?. FOUR. THREE. TWO. ONE.

AUTO provides extended. if either pack is shut off inflight with flaps. low flow. high flow. max flow. no flow.

The purpose of the flow control valve is to maintain airflow over the. AFT CARGO. galleys. aircraft electronics. forward cargo.

The maximum cabin altitude of________normally occurs when the aircraft is at flight altitude FL370. 8000. 7.800. SEA LEVEL. 8.330.

If the Battery Switch is turned OFF on the ground, the APU will. continue to operate. shutdown.

What is the maximum operating FL altitude of the APU?. FL370. FL330.

For extended operations, APU fuel may be provided by_______the pump in the Center tank. LEFT. RIGHT.

The purpose of the flow control valve is to maintain airflow over the. galleys. aircraft electronics. forward cargo. aft cargo.

After the APU control switch is moved to START, approximately how long (in seconds) does it take for the Inlet Door to open?. 20. 30.

Single engine performance is calculated to be dangerous with a pack in__ HIGH. TRUE. FALSE.

The altitude horn activates when the cabin altitude reaches____feet. 10,000. 15,000. 12,500. 14,000.

If the Battery Switch is turned OFF on the ground, the APU will. shutdown. continue to operate.

The airflow through the cold mix valve is delivered to the_. secondary heat exchanger. water separator. turbine. compressor.

Does the Battery Charger continue to charge the aircraft battery during APU start?. NO. YES.

The deflector doors extend when on the ground and in-flight in icing condtions to provide slush and debris protection to the Ram Air system. TRUE. FALSE.

Which pack normally delivers conditioned air to the cabin?_. RIGHT. LEFT. NEITHER. BOTH.

How many electrical systems and packs can be powered by the APU between 10,000 and 17,000'?. Both electrical systems and both packs. Two - any combination of electrical systems and packs. One - either one electrical system or one pack - but not both. One electrical system and one pack (at a time).

The APU Bleed Air Valve also functions as a________to give priority to the delivery of electrical power. Pneumatic switch. Emergency release valve. Load Control Valve. Exhaust.

The maximum cabin altitude of________normally occurs when the aircraft is at flight altitude FL370. 8,000. 7,800. 8,330. sea level.

With the PACK switches in AUTO on the ground, placing both pack switches to HIGH shuts down the_____ recirculation fan. center. left. right. neither.

The APU Bleed Air Valve also functions as a_______to give priority to the delivery of electrical power. Pneumatic switch. Exhaust. Emergency release valve. Load Control Valve.

An amber OFF SCHED DESCENT light illuminates if the airplane begins to descend. more than 120 miles from the destination. for the landing airport. without reaching the planned cruise altitude. without setting the landing altitude in the window.

With the______ position selected, the temperature is sensed in the left sidewall riser. BLEED SUPPLY. SUPPLY DUCT. COCKPIT TEMP. CABIN TEMP.

The DUCT OVERHEAT may be reset by using the______ button. SYSTEM RESET. TRIP RESET. MASTER CAUTION RESET. PACK RESET.

AUTO provides_____ if either pack is shut off in flight with the flaps retracted. high flow. low flow.

The deflector doors extend when on the ground and in-flight in icing conditions to provide slush and debris protection to the Ram Air system. true. false.

The altitude horn activates when the cabin altitude reaches_____feet. 10,000. 15,000. 12,500. 14,000.

The purpose of the flow control valve is to maintain airflow over the______. galleys. aircraft electronics. forward cargo. aft cargo.

For extended operations, APU fuel may be provided by the______ pump in the Center tank. LEFT. RIGHT.

The APU Bleed Air Valve also functions as a______to give priority to the delivery of electrical power. Load Control Valve. Emergency release valve. Exhaust. Pneumatic switch.

How many electrical systems and packs can be powered by the APU between 10,000 and 17,000'?. One - either one electrical system or one pack - but not both. Two - any combination of electrical systems and packs. One electrical system and one pack (at a time). Both electrical systems and both packs.

AUTO provides______if either pack is shut off inflight with flaps extended. LOW FLOW. MAX FLOW. HIGH FLOW. NO FLOW.

AUTO provides______if either pack is shut off in flight with the flaps retracted. HIGH FLOW. LOW FLOW.

Heat Exchangers - The Ram Air system is full open when the aircraft is_____ or when _____ with the flaps extended. parked : on the ground. touching down : inflight. on the ground: inflight. parked : inflight.

The DUCT OVERHEAT may be reset by using the button. SYSTEM RESET. TRIP RESET. MASTER CAUTION RESET. PACK RESET.

If the Battery Switch is turned OFF on the ground, the APU will Exam Questions Answers 1. continue to operate 2. shutdown. SHUTDOWN. Continue TO OPERATE.

In the manual mode, the pilot must manually move the outflow valve. TRUE. FALSE.

The Flight Spoilers augment the Aileron operation when the control wheel is rotated more than degrees. eight. FIVE. FIFTEEN. TEN.

The Ground Service Bus is powered by a Ground Power Source. It powers the Battery Charger, the cabin lighting circuits, and utility outlets that may be needed for cabin servicing. TRUE. FALSE.

Inflight or on the Ground with normal conditions, the Standby Power switch in the AUTO position allows the AC Standby Bus to be normally powered by_____. Transfer Bus 1. Transfer Bus 2. Both Transfer Bus 1 and 2.

Where are the control switches for the NO SMOKING and FASTEN SEAT BELT signs?. Center of the overhead panel. Center of the Control Stand.

The PANEL knob on the F/O's panel can adjust the integral lights in the First Officer's instruments and the AFDS mode control panel edge lighting. TRUE. FALSE.

A flight deck switch and a switch on the_____Attendant station control the Emergency Light system. FOWARD. AFT.

Inflight or on the Ground with normal conditions, the Standby Power switch in the AUTO position allows the AC Standby Bus to be normally powered by______. Transfer Bus 1. Transfer Bus 2. Both Transfer Bus 1 and 2.

When the cockpit door is locked with the control stand switch, entry from the cabin requires. use of a key. electrical power.

When the cockpit lights are tested, which lights will flash continuously?. AFDS flood. The Autoflight MCP segmented lights.

How much fluid remains in the hydraulic reservoir when a leak associated with the engine driven pump occurs in System "B"?. 1/2. 3/4. 1/8. 1/4.

The RF (refill) indication appears if the quantity is below____with both engines shut down or after landing with flaps up during the taxi in. 75%. 76%. 80%. 60%.

The "A" hydraulic system is considered full with_____gallons indicated on the fluid quantity gauge. 3. 5. 4. 4.5.

The External AC Bus is powered when the______light is on. The External AC Bus provides power to fuel gauges and the re-fueling panel. GRD POWER AVAILABLE. GEN BUS OFF.

For high performance takeoffs, the________turned Off, and the APU is used to operate one pack until after takeoff. engine bleeds are. left engine bleed only is.

The Anti-collision lights are turned on before. The Anti-collision lights are turned on before. receiving Checklist.

On the ground, the APU may be used to power both the Left and Right Electrical systems. Inflight, the APU generator can power_____ the left or right electrical system. EITHER. BOTH.

If the exterior switch for the nose gear wheel well light is on, can the nose gear wheel well light be turned off by use of the cockpit Wheel Well Light switch?. NO. YES.

The Standby hydraulic pump LOW PRESS light is inhibited when the Standby system is off. TRUE. FALSE.

Inflight when operating on one generator, the_______load is automatically shed. This reduces the load on the operating generator. galley. galley and water system. windshield heat. water system.

The A and B hydraulic systems are each pressurized by an engine driven hydraulic pump and. a pneumatic pump. a manual emergency pump. an electric motor driven hydraulic pump. NONE OF THESE.

How is the "A" hydraulic system normally pressurized?. By an engine driven pump only. By an engine driven pump and an electric motor pump. By an electric motor pump only. None of these.

Takeoff flaps are set to Flaps 1, 5, or 15, while Flaps 30 or 40 are used for a normal landing. Note: The 500 series aircraft does not use______for takeoff. FLAPS 1. FLAPS 5.

If a leak occurs in System "B" that is associated with the electric motor pump, how much fluid will remain in the reservoir?. An electric motor pump leak will not effect the reservoir. 15 qts. Just enough to operate the PTU. None.

The Standby reservoir is pressurized and receives fluid from an interconnecting balance line from_______reservoir(s). THE A. THE B. BOTH.

With the cockpit Emergency Light switch OFF, the NOT ARMED light illuminates and the batteries. will not be charged. continue to be charged.

With an inoperative engine driven generator, the aircraft can dispatch with the APU as the second source of electrical power. TRUE. FALSE.

With an inoperative engine driven generator, the aircraft can dispatch with the APU as the second source of electrical power__. TRUE. FALSE.

If the exterior switch for the nose gear wheel well light is on, can the nose gear wheel well light be turned off by use of the cockpit Wheel Well Light switch?. YES. NO.

Which cockpit light illuminates with the Emergency Exit lights?. The extra bulb in the dome light. Captain's Floods.

If the Battery is less than_______the APU will not start and the fueling valves cannot be powered by the DC External Bus. 28 volts. 26 volts. 24 volts. 23 volts.

TR1 and TR2 provide_____power to the busses. AC: AC. DC: DC. DC: AC. AC: DC.

Rudder pedal steering provides a maximum steering angle of_____. 18 degrees. 7 degrees.

The External AC Bus is powered when the________light is on. The External AC Bus provides power to fuel gauges and the re-fueling panel. GEN BUS OFF. GRD POWER AVAILABLE.

A red indicator is installed for indication of door arming. With the girt bar _____ the Flight Attendant will move the red indicator from across the door window as a signal that the slide is_____. disarmed : disarmed. armed : armed.

When an engine is started, its ID automatically comes on line and powers the respective side of the electrical system. TRUE. FALSE.

The Passenger Oxygen is supplied by. chemical oxygen generating canisters. an oxygen bottle.

Which bus powers the Dome lights?. Battery bus. Hot Battery bus.

The Power Transfer Unit automatically operates with the flaps between 1 and 5 and with reduced output pressure of the system engine driven pump. A. B.

The Oxygen Blow Out disc is located on the_____side of the fuselage. If this disc is missing - the crew oxygen bottle requires servicing. LEFT. RIGHT.

The Hydraulic System "B" electric motor pump is powered by_______. Generator bus #2. the Emergency DC bus. Generator bus #1. the APU.

Lights on the forward overhead panel indicate if a door is not locked, however there are no indicating lights for the_____doors. overwing exit. entrance.

The individual emergency nicad batteries are all charged by 28 Volt______. D.C. Bus #2. D.C. Bus #1.

Where is the Cockpit Dome light switch?. Aft overhead panel. Control Stand.

The PTU provides a backup source of hydraulic pressure to assist the _ system electric motor pump to operate the leading edge devices and the autoslat system when the _ system engine driven pump output is below normal. B: B. A: A.

The Ground Service Power switch is located at the Forward Flight Attendants' station. TRUE. FALSE.

The water pressure for the lavatories is normally provided by the______. hydraulic system. pneumatic system. electrical system.

When normal power is available, the AC Standby Bus is powered by______. the inverter. Main AC Bus. switched Hot Battery Bus. Transfer Bus 1.

The nickel-cadmium battery located in the Electronics Compartment is: 26 volt. 48 volt. 24 volt. 28 volt.

When normal power is available, the AC Standby Bus is powered by_____. the inverter. Main AC Bus. switched Hot Battery Bus. Transfer Bus 1.

In general, the APU GEN OFF BUS light indicates the APU is running but its generator is not applied to either system. The APU GEN OFF BUS light is inhibited when the APU control switch is__. OFF. ON.

With the #2 generator failed, the Bus Transfer Relay allows the #1 generator to provide power to the___. #2 Generator Bus. #2 Transfer Bus.

The potable water tank is normally pressurized by the pneumatic system with pressure regulated at___. 35 psi. 60 psi. 30 psi. 20 psi.

The Standby hydraulic system can be activated_____. manually only. automatically only. automatically or manually. only while in flight.

With the Isolation Valve switch in AUTO, under what conditions will the Isolation Valve open?. None of these. Either Pack Switch OFF. Either Engine Bleed Switch OFF. Any of these.

A Bank Angle Selector is used to limit the roll guidance for the Heading Select mode and the___ mode. VOR. LNAV.

In VNAV descent, the A/T______and the AFDS holds the FMC target speed using pitch. retards thrust to idle. goes to throttle hold.

Engine anti-ice may be used in the air but is not used on the ground. TRUE. FALSE.