Blue illumination of APU GEN OFF BUS means:

Yaw damper inputs (main or standby) can be overridden:

Illumination of the STANDBY POWER OFF lights indicates:

The FMC advisory Message BUFFET ALERT indicates:

Refer to the RF indication to the right of the hydraulic system quantity indication. This indication is displayed:

Landing auto brake setting may be selected after touchdown:

The trailing edge flaps are at 15 units, the correct indication on the aft overhead panel for the leading edge devices is:

On the ground, for primary ATC communication:

Aircraft in flight. You have 2500 kg of fuel in the No 1 main tank and 3060 kg of fuel in the No 2 main tank. You will see:

The FMC Alerting Message INSUFFICIENT FUEL means:

An amber IAS DISAGREE alert in the bottom of the speed tape indicates:

For landing, what is maximum fuel imbalance between No 1 and No 2 main tanks?

The amber LOW PRESSURE Light for System B Electric Hydraulic Pump illuminates. What are the other indications?

What is the maximum authorised thrust reduction below any certified rating?

What is the condition of the VALVE OPEN Light when the crossfeed selector is positioned OPEN and the crossfeed valve is closed?

The APU may be used as a pneumatic source up to:

The SMYD computers receive inputs from:

Following an unpressurised takeoff, when is the first engine Bleed Switch positioned to ON?

The supplemental and temporary data bases has storage capacity for:

Fuel for the APU is normally supplied from the:

Refer to the thermal anti-ice (TAI) CDS indication. TAI is shown above each N1 indicator:

Which window(s) are heated with the LEFT FWD WINDOW HEAT switch ON?

APU cooling air:

The right IRS is electrically powered from:

Which systems use engine bleed air for operation?

Arrivals can be selected on the FMC for either the origin or destination airport on the DEP/APR page:

Which of the following will cause activation of the takeoff configuration warning system?

When the manual gear extension access door is open:

If a wet start is detected, the EEC will automatically turn off ignition and shut off fuel to the engine:

The number of flight spoilers located onn each wing are:

What happens with the IAS/MACH display on the MCP if SPD INTV switch is pushed during VNAV operation:

With normal power source on the buses, placing the battery switch to OFF will remove power from:

The Recirculation Fan:

The amber LE FLAPS TRANSIT light:

(RF) Indication is displayed to the right of the hydraulic system quantity:

Which statement is true?

In degraded mode, what are the combinations for transmission and reception at the degraded station?

The scratch pad message VERIFY GW AND FUEL appears:

The ND Wind direction/speed and wind arrow is:

The purpose of the landing gear transfer unit is to:

Elevator feel system is provided by the elevator feel computer. This computer receives inputs of:

During cruise the FMC Alerting Message VERIFY POSITION indicates:

What pitch mode is annunciated in the FMA after takeoff when the autopilot is first engaged in CMD?

The flap/slat electronics unit (FSEU) provides:

With the STANDBY POWER switch in the AUTO position, loss of both engine driven generators and APU generator will result in that AC standby bus is powered by battery through static inverter and DC standby bus is powered by battery:

What is the primary source of conditioned air from the cockpit?

The amber LOW PRESSURE Light for the No 1 Engine Driven Hydraulic Pump illuminates. What should you do?

When operating on standby power:

The air/ground system receives logic signals from:

During cruise you note both center tank fuel pumps have failed as indicated by the illumination of both center tank fuel pump LOW PRESSURE lights. You still have 320 kg of fuel in the center tank and both main tanks are full. You will see:

A DUCT OVERHEAT light only will cause:

Predictive Windshear alerts are triggered from:

The Power Transfer Unit provides an alternate source of power for the Autoslat System if:

The FMC alerting message RESET MCP ALT means:

With the Multifunction Display Switch (MFD) is SYS in lower DU shows:

The GROUND POWER AVAILABLE light will extinguish when:

During flight with hydraulic system B inoperative (no fluid in system B):

During an ILS approach the captain observes his BARO minimum reference altitude turns from green to flashing amber for three seconds, this means:

The hydraulic brake pressure indicator displays accumulator nitrogen pre-charge pressure of 1000 psi and:

The EEC provides redline overspeed protection for:

Engine oil pressure is in the yellow band at take off thrust. Which of the following is true

What could cause the amber ANTISKID INOP Light to illuminate?

With the loss of hydraulic system B, (system A operating normally):

The crew fails to properly accomplish normal procedures and takes off with the APU powering both transfer buses:

The amber OFF SCHEDULE DESCENT Light illuminates. What does this indicate?

The Predictive Windshear alerts are available:

With ENGINE START switch in OFF, automatic ignition will occur:

If the thrust lever(s) are advanced after touchdown:

In the PACK TRIP OFF non-normal procedure, the crew selects a warmer temperature in order to:

The APU switch to OFF position has an automatic shutdown delay of:

The Auto position of the Cockpit Voice Recorder (CVR) On/Auto switch:

One of the purposes of the FMC FIX INFO page is to:

The Power Transfer Unit provides a backup source of hydraulic pressure to operate the:

The APU starter cycle may take up to:

Illumination of the BAT DISCHARGE light indicates:

The left IRS is electrically powered from:

A leak in standby hydraulic system will cause system B fluid indication decrease to approximately:

In normal operation, what provides the A/T system with N1 limit values?

The alpha vanes provide angle-of-attack information to the stall warning system, auto throttle, auto pilot, auto slats and are anti-iced:

Emergency exit light can be activated from:

Placing the TEST Switch in the FAULT/INOP position tests:

The PASS OXY ON Light illuminates, what does this indicate?

What information is available with the IRS mode selector in ATT?

Which A/T modes permit manual thrust changes without A/T interference?

How many independent Flight Control Computers (FCCs) are there in the Autopilot Director System (AFDS)?

The APU is capable of supplying bleed air for both air conditioning packs:

The EGT display, both box and dial, turn red and the EEC automatically turns off ignition and shut off fuel to the engine if:

If the APU GEN OFF BUS light fails to illuminate by the end of the start cycle:

The AUTOSLAT system:

The First Officer observes the word PITCH displayed in amber in the lower portion of the PFD during an ILS approach. This means:

With the CONTROL PANEL select switch on the Displays Source Panel in the BOTH ON 2 position:

On the ground the TR UNIT amber light illuminates if:

Refer to the Cabin/Flight Altitude placard. At a cruise altitude FL290, the cabin altitude should read:

Select the correct statement:

Impact fittings located in the opening of each main gear well:

During taxiing out for takeoff, the amber AUTO BRAKE DISARM Light illuminates. What should you do?

When does the amber DUAL BLEED Light illuminate

Once activated, the APU DC operated fuel pump operates automatically until:

A leak in the No. 2 engine driven hydraulic pump or associated lines can result in a total loss of hydraulic system B pressure:

To climb to FL280 in the shortest distance, MAX ANGLE should be selected on page?

How many fire extinguishing bottles are there totally for engine and APU fires?

The FMC Advisor Message DRAG REQUIRED indicates the aircraft is:

During the ILS approach on the radio altimeter remaining perimeter and pointer turns amber and flashes for 3 seconds. This means:

During normal operations, hydraulic quantity indications vary when:

Illumination of the APU DET INOP Light will cause following lights to illuminate:

Which mode must be armed before the second autopilot can be selected during a dual channel A/P approach?

Which bus supplies electrical power to the auxiliary battery charger:

In addition to hydraulic system A and B, the rudder can also be powered by the standby hydraulic system through the:

During AUTO LAND at which radio altitude should the flare mode be engaged?

The number of ground spoilers on each wing are:

A WING BODY OVERHEAT light indicates:

The Autoslat system:

An illuminated BLEED TRIP OFF light indicates:

A valid FMC PERF INIT page Scratch Pad entry for actual FUEL is:

The ELEC light will illuminate in flight if:

If during RECALL on TAXI CHECKLIST, you push and release the system annunciator, the IRS light comes ON. The GPS light is illuminated on the AFT OVERHEAD PANEL, and extinguishes when Master Caution is reset.

The flight crew oxygen system uses auto pressure breathing masks / regulators with pressure breathing starting at:

While flying an ILS approach below 1,000 feet Radio Altitude, a BELOW G/S alert occurs. To cancel the alert:

What is the position of the isolation valve when the ISOLATION VALVE Switch is in AUTO?

What is the maximum airspeed limit according MEL, when WINDOW HEAT is inoperative for window nr 4?

There are CDS fuel alerts indications for:

The elevator control column override mechanism allows:

The Ground Proximity Warning System Test:

If an outboard display unit fails, the PFD is automatically displayed:

How are the Engine Bleed Air valves powered?

What does an illuminated main tank fuel pump LOW PRESSURE Light indicate?

Dotted red areas on terrain display indicate:

During the PRELIMINARY COCKPIT PREPARATION, the IRS Mode Selectors are normally positioned to:

During normal operation with the OVHT DET Switch in NORMAL, an alert is initiated if:

With fuel in the center and main tanks, both engines operating and all fuel pump switches ON, fuel from which tank(s) is used first?

Placing the TEST Switch, on fire protection panel to FAULT/INOP position tests:

The amber DUAL BLEED light is illuminated before starting engines. What should you do?

The cross bus tie relay automatically opens at glide slope capture to:

In the event of an elevator jam, an override mechanism allows:

During a normal engine start:

The landing gear indicator lights found on the center panel will illuminate red when:

Where do you read the flight crew oxygen pressure?

Which pitot probes and static ports are not heated

During cruise you note both center tank fuel pumps have failed as indicated by the illumination of both center tank fuel pump LOW PRESSURE lights. You still have 320 kg of fuel in the center tank and both main tanks are full. You will see:

Of the four lights located on the APU control panel, which light will NOT cause an automatic shutdown of the APU when it illuminates?

An amber ALT DISAGREE in the bottom of the altimeter tape is an indication of:

The Look-Ahead Terrain alerting system will show for terrain:

Autopilot trim and main stabiliser trim use:

If a landing is made with RTO selected:

The Cockpit Voice Recorder uses four independent channels to record flight deck audio for a maximum of:

While making a no engine bleed air take off and an engine failure occurs, when should the bleed air switches be positioned to ON?

After lift-off, the A/T remains in THR HLD until:

A magenta bug on the vertical speed indicator in the PFD indicates:

Pulling the engine fire warning switch up:

Refer to the Cabin/Flight Altitude placard. At a cruise altitude FL290, the cabin altitude should read:

If the FAULT Light on the IRS Mode Selector Unit illuminates, it indicates:

What is the source of electrical power for the engine fuel shutoff valves?

Electrical power to start the APU comes from:

An Amber PACK light illumination during Master Caution recall, that extinguishes when master caution is reset, indicates:

During VNAV operations the Fuel Quantity Indicating System fails:

The APU starts, operates and can supply electrical power alone up to:

The landing gear configuration warning horn will activate anytime a gear is not down and locked:

The curved trend vector extending from the aircraft symbol on ND MAP and MAP CTR is divided into three segments, it represents with range greater than 20 NMs:

An amber ROLL displayed in the lower portion of the altitude indicator on the PFD means:

When is the ENGINE ANTI-ICE turned on if icing condition exists on the ground?

The mach/airspeed warning system can only be checked on the ground:

If GROSS WT is not available from the FMC, the APPROACH REF page will be:

Landing auto brake setting may be selected after touchdown:

One basic principle of operation for the 737 electrical system is:

The power source for Fire Extinguishing is:

Engine bleed air is obtained from:

Activated at 14,000 feet the passenger oxygen masks drop down from the stowage:

The Standby Hydraulic System powers the:

To see both left and right GPS position relative to the FMC position you select:

The TR Unit light will illuminate in flight if: