Boeing B737 MAX - Anti Ice and Rain

Which portion of the wings does the wing anti-ice system heat?

Three inboard leading edge slats.

Outboard leading edge slats.

Outboard leading edge slats and flaps.

Leading flaps.

Correct! Wrong!

When are the ENGINE ANTI-ICE switches turned ON if icing conditions exist on ground?

When cleared on the runway.

Before engine start.

During taxi out.

Immediately after engine start.

Correct! Wrong!

Dual angle-airflow sensors (alpha vanes) provide angle-of-attack information to the stall warning system, autothrottle, autopilot and autoslats and are anti iced:

Whenever the alternate static ports are heated.

Whenever wing anti-ice is being used.

By independent 115V AC heating elements, controlled by the Probe Heat switches.

By actuating the LEFT or RIGHT FWD window heat switch.

Correct! Wrong!

Positioning ENG ANTI-ICE switch to on has what effect?

Adjusted stall warning logic for stick shaker, minimum maneuver speed bars on airspeed indicator, and automatically adjusted FMC displayed VREF; return to normal when engine anti-ice is positioned to OFF.

Stall warning logic adjusts stick shaker and minimum maneuver speed bars on airspeed indicator.

FMC displayed VREF is adjusted automatically.

Adjusted stall warning logic for stick shaker, minimum maneuver speed bars on airspeed indicator, and automatically adjusted FMC displayed VREF; remain for rest of flight.

Correct! Wrong!

The aircraft is on the ground. You place the WING ANTI-ICE switch to ON. Which conditions will allow the wing anti-ice valve to open?

Thrust on both engines is above the setting for takeoff thrust and the temperature inside both wing distribution ducts is below the thermal switch activation temperature.

Thrust on both engines is below the setting for takeoff thrust and the temperature inside both wing distribution ducts is below the thermal switch activation temperature.

Thrust on both engines is above the setting for takeoff thrust or the temperature inside both wing distribution ducts is above the thermal switch activation temperature.

Thrust on both engines is below the setting for takeoff thrust or the temperature inside both wing distribution ducts is above the thermal switch activation temperature.

Correct! Wrong!

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

L1, L2, L3.

L2, L4, L5.

L1 only.

L2, L3, L4, L5.

Correct! Wrong!

The OVHT test will cause all overheat lights to come on and the ON lights will eventually go out. How does a pitot reinstate the Window heat after performing an Overheat test?

Cycle all switches OFF for 10 seconds and ON.

Cycle power OFF and ON to Main AC Bus 2.

Cycle all switches OFF and ON.

Correct! Wrong!

Illumination of an amber COWL ANTI ICE light indicates:

The respective cowl anti-ice valve is open.

The respective cowl anti-ice valve is in transit, the cowl anti-ice vave position disagrees with the respective engine anti-ice switch position.

An overtemperature or overpressure condition.

An overpressure condition.

Correct! Wrong!

What do the green ON lights indicate above the Window heat switches?

Illuminated means the window Overheat system has activated.

Extinguished means heat still being applied to window but not yet at correct operating temperature, illuminated means window at correct temperature.

Illuminated means heat being applied to windows, extinguished means windows at correct temperature

Illuminated means window heat needs to be switched on for that window, extinguished means heat now being applied to that window.

Correct! Wrong!

Which pitot probes and static ports are not heated?

No.2 Aux pitot probe and static port.

Alternate static ports.

Elevator pitot probes.

No.1 Aux pitot probe and static port.

Correct! Wrong!

Windshield wipers of are provided to maintain a clear area on the cockpit No.1 windows. Which of the following statements is correct?

INT is a three second intermittent operation.

Each wiper is operated by a separate system

Windshield wipers may be operated on a dry windshield

Windshield wipers are hydraulically operated & electrically controlled

Correct! Wrong!

Illumination of the amber ENGINE ANTI-ICE caption indicates that:

The engine cowl thermal anti-ice system has been inhibited due to a system failure.

The engine cowl thermal anti-ice system has been inhibited due to a system failure or when an engine core anti-ice valve fails closed.

An engine core anti-ice valve has failed closed.

Correct! Wrong!

Passing 3000 feet climbing, you have selected Engine Anti-Ice ON. Passing FL90, you select them OFF.

Stall warning logic, airspeed indications and minimum maneuver speeds on the airspeed indicator return to normal.

Stall warning logic, airspeed indications and minimum maneuver speeds on the airspeed indicator return to normal, if wing anti-ice has not been used in flight.

Stall warning logic and minimum maneuver speeds on the airspeed indicator return to normal, if wing anti-ice has not been used for takeoff.

Stall warning logic and minimum maneuver speeds on the airspeed indicator return to normal.

Correct! Wrong!

The window heat PWR TEST:

Also tests the overheat protection system.

Provides a confident test.

Must be tested before each flight.

Must be tested before using the window heat system.

Correct! Wrong!

If you select the WING ANTI-ICE switch on the ground:

Wing anti-ice control valves open if thrust on both engines is below takeoff warning setting and temperature inside both distribution ducts is below thermal switch activation temperature.

Wing anti-ice control valves open if thrust on both engines is below takeoff warning setting.

Wing anti-ice control valves open if thrust on either engine is below takeoff warning setting and temperature inside both distribution ducts is below thermal switch activation temperature

Correct! Wrong!

The amber COWL ANTI-ICE is illuminated.

It indicates an excessive temperature in the duct between the cowl anti-ice valve and cowl lip.

It indicates an overpressure and excessive temperature condition.

It indicates an overpressure condition in duct downstream of engine cowl anti-ice valve.

It indicates either an overpressure or an excessive temperature condition

Correct! Wrong!

Temperature controllers maintain the correct temperature on windows No. 1 and 2. In the event of an overheat, power is automatically removed.

True.

False.

Correct! Wrong!

What happens when the WING ANTI-ICE switch is placed ON while in flight?

All statements are correct.

FMC displayed Vref is not adjusted

Stick shaker logic is biased for icing conditions.

Both Control valves open.

Correct! Wrong!

Both windshield wipers are controlled with a common switch.

False.

True.

Correct! Wrong!

When operating on standby power, only the captain's pitot probe is heated, however, the CAPT PITOT light does not illuminate for a failure.

True.

False.

Correct! Wrong!

Positioning the WING ANTI-ICE switch to ON in flight:

Adjusts FMC displayed VREF automatically when WING ANTI-ICE switch is ON.

Sets stick shaker logic for icing conditions for the remainder of the flight.

Have no influence on stick shaker logic.

Sets stick shaker logic for icing conditions only when WING ANTI-ICE switch is ON.

Correct! Wrong!

The R ELEV PITOT light is illuminated. What does this indicate?

The Right elevator pitot is not heated.

System B hydraulic pressure is low.

The Right elevator pitot is blocked.

All statements are correct.

Correct! Wrong!

The cowl anti-ice valve is ___ controlled and _ operated.

Electrically _ Electrically.

Electrically _ Mechanically.

Pneumatically _ Mechanically.

Electrically - Pneumatically.

Correct! Wrong!

Power to window numbers 1 and 2 must be initially selected OFF by the flight crew if an overheat condition is detected.

True.

False.

Correct! Wrong!

Power to window numbers 1 and 2 is automatically removed if an overheat condition is detected.

You select the engine anti-ice valve to the ON position. The COWL VALVE OPEN light is illuminated blue and the TAI indication illuminates on the CDS. What happened?

The cowl anti-ice valve fails to move to the position commanded by the ENG ANTI-ICE switch.

This is a normal indication.

There is excessive pressure in the duct leading from the cowl anti-ice valve to the cowl lip.

There is excessive heat applied to the cowl lip.

Correct! Wrong!

On the ground and in flight, the wing anti-ice valves close if the forward thrust levers are advanced above the takeoff warning setting.

True.

False.

Correct! Wrong!

When operating on standby power only the Captain's pitot probe is still heated - if the Captain's pitot probe heating fails in this condition, there is no CAPT PITOT alert given.

False

True.

Correct! Wrong!

With the WING ANTI-ICE switch ON and the aircraft on the ground, the WING ANTI-ICE switch remains ON regardless of the control valve position.

False.

True.

Correct! Wrong!

When operating on standby power, only the captain's pitot probe is heated, however, the CAPT PITOT light does not illuminate for a failure.

True.

False.

Correct! Wrong!

The rain removal system for the forward windows comprises of the following:

Windshield wipers, heated windows, hydroscopic rain repellent coating.

Windshield wipers.

Heated windows, Windshield wipers.

Windshield wipers, hydroscopic rain repellent coating.

Correct! Wrong!

If the cowl anti-ice valve fails to move to the position indicated by the ENG ANTI-ICE switch, the COWL VALVE OPEN light remains illuminated bright blue and an amber TAI indication immediately illuminates on the CDS.

True.

False.

Correct! Wrong!

The wing anti-ice system provides bleed air to all leading edge slats:

True.

False.

Correct! Wrong!

The wing anti-ice system provides protection for the three inboard leading edge slats by using bleed air. The wing anti-ice does not include the leading edge flaps or the outboard leading edge flaps.

The engine Cowl Anti-Ice valve is located UPSTREAM of the Engine Bleed Air Valve.

False.

True.

Correct! Wrong!

The WING ANTI-ICE switch automatically trips OFF:

When both thrust levers are set for takeoff and airspeed is above 60 knots.

When both thrust levers are set for takeoff and airspeed is above 80 knots.

When both thrust levers are set for takeoff.

At liftoff when the air-ground sensor goes to the air mode.

Correct! Wrong!

Stall warning logic, airspeed indications, and minimum maneuver speeds on the airspeed indicator return to normal when engine anti-ice is positioned OFF if wing anti-ice has not been used in flight.

False.

True.

Correct! Wrong!

Does the availability of bleed air for engine anti-ice require that the engine bleed air switch be ON?

Yes.

No.

Correct! Wrong!

What is the maximum airspeed limit when WINDOW HEAT is inoperative?

250 KIAS below 10 000 feet.

280 KIAS.

250 KIAS.

280 KIAS below 10 000 feet.

Correct! Wrong!

The wing anti-ice control valves are:

AC motor operated

Both DC & AC motor-operated.

DC motor-operated.

Correct! Wrong!

The pitot probe for standby airspeed continues to be heated when the airplane is on standby power.

False.

True.

Correct! Wrong!

The pitot probe for standby airspeed is not heated when the airplane is on standby power.

A conductive coating on the outer glass pane of window numbers 1 and 2 permits electrical heating to prevent ice build-up and fogging. Window number 3 is not electrically heated.

True.

False.

Correct! Wrong!

What maintains the correct temperature on windows No. 4 and 5?

A thermal switch located on window No. 5.

These windows are heated with cabin air.

Individual thermal switches.

A thermal switch on window No. 4.

Correct! Wrong!

Boeing 737 MAX - Anti Ice and Rain

Quiz

Boeing B737 MAX - Anti Ice and Rain

Which portion of the wings does the wing anti-ice system heat?

When are the ENGINE ANTI-ICE switches turned ON if icing conditions exist on ground?

Dual angle-airflow sensors (alpha vanes) provide angle-of-attack information to the stall warning system, autothrottle, autopilot and autoslats and are anti iced:

Positioning ENG ANTI-ICE switch to on has what effect?

The aircraft is on the ground. You place the WING ANTI-ICE switch to ON. Which conditions will allow the wing anti-ice valve to open?

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

The OVHT test will cause all overheat lights to come on and the ON lights will eventually go out. How does a pitot reinstate the Window heat after performing an Overheat test?

Illumination of an amber COWL ANTI ICE light indicates:

What do the green ON lights indicate above the Window heat switches?

Which pitot probes and static ports are not heated?

Windshield wipers of are provided to maintain a clear area on the cockpit No.1 windows. Which of the following statements is correct?

Illumination of the amber ENGINE ANTI-ICE caption indicates that:

Passing 3000 feet climbing, you have selected Engine Anti-Ice ON. Passing FL90, you select them OFF.

The window heat PWR TEST:

If you select the WING ANTI-ICE switch on the ground:

The amber COWL ANTI-ICE is illuminated.

Temperature controllers maintain the correct temperature on windows No. 1 and 2. In the event of an overheat, power is automatically removed.

What happens when the WING ANTI-ICE switch is placed ON while in flight?

Both windshield wipers are controlled with a common switch.

When operating on standby power, only the captain's pitot probe is heated, however, the CAPT PITOT light does not illuminate for a failure.

Positioning the WING ANTI-ICE switch to ON in flight:

The R ELEV PITOT light is illuminated. What does this indicate?

The cowl anti-ice valve is _________ controlled and _______ operated.

Power to window numbers 1 and 2 must be initially selected OFF by the flight crew if an overheat condition is detected.

You select the engine anti-ice valve to the ON position. The COWL VALVE OPEN light is illuminated blue and the TAI indication illuminates on the CDS. What happened?

On the ground and in flight, the wing anti-ice valves close if the forward thrust levers are advanced above the takeoff warning setting.

When operating on standby power only the Captain's pitot probe is still heated - if the Captain's pitot probe heating fails in this condition, there is no CAPT PITOT alert given.

With the WING ANTI-ICE switch ON and the aircraft on the ground, the WING ANTI-ICE switch remains ON regardless of the control valve position.

When operating on standby power, only the captain's pitot probe is heated, however, the CAPT PITOT light does not illuminate for a failure.

The rain removal system for the forward windows comprises of the following:

If the cowl anti-ice valve fails to move to the position indicated by the ENG ANTI-ICE switch, the COWL VALVE OPEN light remains illuminated bright blue and an amber TAI indication immediately illuminates on the CDS.

The wing anti-ice system provides bleed air to all leading edge slats:

The engine Cowl Anti-Ice valve is located UPSTREAM of the Engine Bleed Air Valve.

The WING ANTI-ICE switch automatically trips OFF:

Stall warning logic, airspeed indications, and minimum maneuver speeds on the airspeed indicator return to normal when engine anti-ice is positioned OFF if wing anti-ice has not been used in flight.

Does the availability of bleed air for engine anti-ice require that the engine bleed air switch be ON?

What is the maximum airspeed limit when WINDOW HEAT is inoperative?

The wing anti-ice control valves are:

The pitot probe for standby airspeed continues to be heated when the airplane is on standby power.

A conductive coating on the outer glass pane of window numbers 1 and 2 permits electrical heating to prevent ice build-up and fogging. Window number 3 is not electrically heated.

What maintains the correct temperature on windows No. 4 and 5?

The cowl anti-ice valve is ___ controlled and _ operated.