737 -800

The Maximum Engine Start EGT limit for 737NG. 725C. 925C. 950C. 975C.

the water pressure fo the lavatories is normally provided by the. pneumatic system. hydraulic system. electrical system.

the maximum continous EGT limit for B737 NG is. 725c. 925c. 950c. 975c.

in the event system A and B fails, the stanby system may be pressurized by a motor driven pump that is powerd by the. #1 ac transfer bus. #2 ac trnsfer bus. DC ESS BUS.

What is the speed limit for extension of the outboard landing lights?. none. 250kts.

the cockpit windows are numbered 1 through 5 on each side all windows except #3 widows are. electrically heated. seal closed.

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

the thrust reversrs are operated ___________. hydraulically. pneumatically.

if the standby hydraulic system is automatically activated during takeoff - when will it shut off?. when flaps are extended. when ailerons are extended. when flaps are retracted. when ailerons are retracted.

if the power quantity is not good. the bus protection panel will not allow the ground power to apply to the electrical system. true. false.

where is the reservoir for hydraulic system B?. aft cargo comparment. left gear well. right gear well. main gear well.

the cargo comparments are sealed and pressurized. The pressurization of these comparments is mantained equal to the cabin by _________. forced airflow. pressure equalization valves.

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

he current Radio Altitude is displayed in the bottom center of the attitude indication area when radio altitude is below feet AGL. (NG). 3000. 1500. 2000. 2500.

The ADF control panel mode selector is used to turn OFF the receiver or to select ANT (used for audio reception only), or - used for normal operation with bearing information and audio reception. (CL). normal. ADF.

The Standby Airspeed Indicator and Standby Altimeter are displayed on the panel. (CL) instrument. CENTER. CAPITAIN.

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

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. TURE. FALSE.

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

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

HOW MANY EQUIPMENT COOLING FANS ARE INSTALLED. TWO. SIX. THREE. FOUR.

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

THE PURPOSE OF THE FLOW CONTROL VALVE IS TO MAINTAIN AIRFLOW OVER THE. AFT CARGO. FWD CARGO. GALLEYS. AIR CRAFT ELECTRONICS.

WHEN A MANUAL MODE IS SELECTED. GREEN MANUAL LIGHT ILUMINATES. MANUAL AC MOTOR STARTS RUNNING. MANUAL DC MOTOR STARTS RUNNING. THE AC MOTOR IS DISABLED.

Heat Exchangers - The Ram Air system is full open when the aircraft is _ ___or when ___with the flaps extended. parked: inflight. on the ground: inflight. touching down: inflight. parked: on the ground.

uring 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 psid. 7 psid.

verheat 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 THE ENGINE THRUST. FIRE.

APU Fire Protection is provided from two bottles of extinguishing agent. (NG). TRUE. FALSE.

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

Flight mode annunciations are displayed in the top three windows on the PFD. Armed modes appear in subscript format. Active modes appear in (NG). white: red. green: red. green : white. white: green.

Weather Radar display range is determined by the _(NG). Weather Range SelectoR. . ND Range Selector.

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

The wheel well system monitors fire conditions, but does not monitor_ (CL) Answers. POWER. OVERHEAT OR FAULT CONDITIONS.

Condition: LNAV is armed. In order for NAV to engage, the aircraft must be within_ active course - regardless of the aircraft heading?(NG). 3NM. 5NM.

If you start a descent using a mode such as AFDS Level Change, what do you have to do in order to recapture the NAV Descent? (NG). Nothing - it will create a new TOD automatically. Update the Cruise Altitude.

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

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

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

modification that requires a route or airway change will be made to which CDU page?(NG). RTE. CLB. LEGS. CRZ.

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

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.

Do the Flight Spoilers extend on the ground?. YES. NO.

THE FUEL TEMPERATURE INDICATOR DISPLAYS THE TEMPERATURE OF THE FUEL IN TANK___. 1. 2.

The Inboard Flight Spoilers and the Ground Spoilers are powered by the. B HYDRAULIC SYSTEM. A HYDRAULIC SYSTEM.

Normally, the______system supplies pressure to the autoslat control valve. STAND BY. B. A.

TCAS does not display any information on aircraft until they are within __laterally and___vertically. 6NM:1200 FEET. 12 nm: 1200 feet. 100 nm: 9000 feet. 30 nm : 9000 feet.

Can the 737 Transfer fuel from tank to tank when inflight?. YES. NO.

ONCE ACTIVATED , HOW LONG WILL THE SCAVANGE SHUTOFF VALVE REMAIN OPEN (IN MINUTES). TWENTY. FIFTEEN.

The final level of TCAS alert is called a resolution advisory (RA). its is displayed as______when the intruder aircraft is_______.A TA generates a voice command and displays symbology directing the aircrew to maneuver the aircraft. red square: within 15 to 35 seconds, depending upon your altitude. an open white diamond: within 30nm and 9000 feet. an amber circle: within 25 to 48 seconds, depending upon your altitude. a solid white diamond: within 6 nm and 1200 feet.

Both PWS Warnings and Cautions are accompanied by aural alerts and a WINDSHEAR message on the nav display. true. false.

with a loss of both hydraulic system, the ailerons can be operated through the contro cables. true. false.

If both Wing Tank Fuel Pump LOW PRESSURE lights come on, the Master Caution and FUEL system annunciatior lights. will come on. will go out.

The best way to avoid a storm is to_____. climb to fly over the storm. deviate laterally, at least 20 miles downwind. descend and fly under the storm. deviate laterally, at least 20 miles upwind.

What is the purpose of the Fuel Vent lines?. To prevent positive overpressures only within the fuel tanks. To prevent positive or negative overpressures within the fuel tanks. To prevent negative overpressures only within the fuel tanks. To prevent positive or negative overpressures within the Center fuel tank only.

The Predictive Windshear System (PWS). is a feature of the Enhanced Ground Proximity Warning Systems look-ahead capability. has its own transmitting antenna and a separate receiver. is a function of the weather rada.

The Fuel Quantity Gauges are powered by Standby AC power. true. false.

If one Wing Tank Fuel Pump LOW PRESSURE light comes on, the Master Caution and FUEL system annunciatior lights. never come on when the recall feature is used. immediately will go out. will only come on when the recall feature is used. immediately come on.

All ground spoiler panels are powered by the. C hydraulic system. B hydraulic system. A hydraulic system.

How many positions are available for the leading edge slats?. Three. One. Four. Two.

TCAS does not display any information on aircraft until they are within___laterally and___vertically. 6 nm : 1200 feet. 12 nm: 1200 feet. 100 nm: 9000 feet. 30 nm : 9000 feet.

The _____provides a back-up method of rudder operation. battery power. there is no further backup. standby Pneumatic system. standby hydraulic system.

The Predictive Windshear System (PWS). is a feature of the Enhanced Ground Proximity Warning Systems look-ahead capability. has its own transmitting antenna and a separate receiver. is a function of the weather radar.

The inboard flight spoilers are operated by the A hydraulic system, and the outboard flight spoilers are operated by the. A hydraulic system. B hydraulic system.

What is the minimum inflight fuel temperature if the freezing point of your fuel is -53 C (in degrees centigrade)?. -45. -30.

can the engines suction feed fuel from the center tanks. false. true.

When is the Fuel Crossfeed VALVE OPEN light illuminated bright?. When the valve is in transit or otherwise disagrees with the selected position. When the valve should not be in theOPEN position. When the valve should be in the OPEN position. When the valve is in the OPEN position.

Will the rudder operate with only one hydraulic system available?. yes. no.

Which Center tank fuel pump normally feeds the #2 engine?. right. left.

In aircraft equipped with color radar, the colors are used to designate the object's intensity. Low intensity is displayed as green; moderate intensity, yellow; high intensity, red; and very high intensity as magenta. true. false.

The Fuel Crossfeed Valve is electrically operated. true. false.

Can the activation of aileron trim cause the flight spoilers to extend?. yes. no.

The Yaw Damper actuator normally uses hydraulic pressure from the ___. B system. both systems. standby system. A system.

When is the Fuel Crossfeed VALVE OPEN light illuminated dim?. When the valve is open and the selector is in the closed position. When the valve is open and the selector is in the open position. When the valve should be open and the selector is in the closed position. When the valve is closed and the selector is in the open position.

The Standby Rudder system can operate the rudder with a failure of. only one hydraulic system. one or both pneumatic systems. Only one pneumatic sistem. One or both hydraulic system.

which wing tank fuel boos pumps are running for normal flight operations ?. Both. the right wing tank pumps only. the left wing tank pumps only. neither.

Flap position ___affect the speed or range of the Autopilot Trim system. Does. Does not.

the L.E Slats move from Extend to Full Extend when the Flap lever is moved ______________. beyond flaps 5. beyond flaps 15. beyond flaps 8. beyond flaps 23.

if the leading edge devices are extended with standby system pressure, they cannot be retracted. true. false.

PWS operates automatically when the aircraft is within 2300 feet of the ground. true. flase.

Water Extinguishers are used on____while Halon 1211 is effective on fuel, grease, and electrical fires. material fires. electrical fires.

How many switches are installed to control the Emergency Lights?. 1. 2.

A Power Transfer unit is designed to automatically operate if the __________ output pressure is low. The PTU provides backup supply to the Autoslats and the leading edge devices. system A engine driven pump. system B engine driven pump.

The Battery Bus is normally powered from. TR3. TR2. TR1. All TR's.

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

The Emergency Light battery packs are charged by power from______. AC Bus #1. DC Bus #1.

Will the Nosegear Taxi light automatically turn off when the gear are retracted?. yes. no.

the voltmeter will display ______________When the Battery is being charged. 28 to 30 volts. 26 to 28 volts. 28 volts. 28 to 30 volts.

What is the purpose of the Standby system?. supply backup pressure to operate the rudder only. To supply backup pressure to operate the thrust reversers only. To supply backup pressure to operate the rudder, thrust reversers, and leading edge devices. To supply backup pressure to operate the leading edge devices only.

How is the DC system powered?. Powered from the AC system through transformer rectifiers. APU. IDGS. External Power.

The PTU shut off valve automatically opens to provide_____system pressure when necessary to operate the PTU. A. B. A and B.

The aircraft is equipped with______-90KVA generators. two. five. three. four.

Power to the Cockpit lighting is normally divided between the two. Main AC buses. AC Emergency Buses.

The OFF position of the Bus Transfer Switch opens the. DC Crosstie Relay. Bus Tie Braker.

The OVERHEAT lights on the hydraulic control panel monitor the fluid temperature in the case of drainage of the associated_________________pump. All of these. Engine driven. Pneumatic. electric motor.

Maximum nose wheel steering is_____when controlled by the tiller. 78 degrees. 84 degrees.

With the POSITION lights switch in the STROBE and STEADY position,____lights will operate. both the strobes and the steady colored navigation. only the steady colored navigation.

The cargo compartments comply with the_____category. That is - they are not ventilated and will not normally support a fire. Class C FAA. Class D FAA.

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

DC power is normally provided by onboard _____DC transformer Rectifiers that convert AC power to Dc power. 14 volt. 28 volts.

the OVERHEAT lights on the hydraulic control panel monitor the fluid temperature in the case of drainage of the associated _______Bus. all of these. electric motor. engine driven. pneumatic.

concerning the entery light jst outside the cockpit door. What will the light do when the cockpit door is opened with at leas one engine running?. Dim. full Bright.

Note:if no other power is on the aircraft, the position lights switch STEADY position will power the appropiate lights from the________ bus power. battery. transfer.

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