737-MAX Flashcards by István Szijjártó

What causes both of the BLEED lights to illuminate at the same time?

Both BLEED switches off ater Take Off or go around

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Engine bleed air is extracted from what stages of the compressor?

4th and 10th

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In flight, how many air conditioning packs is one engine bleed capable of supplying on the 737 MAX?

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How is the operation of the bleed air system controlled?

Electronically controlled

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What causes both PACK lights to illuminate at the same time?

Both PACK control switches in the OFF position after takeoff

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Where are the RAM DOOR FULL OPEN lights located on the 737 MAX

These lights are not on the MAX

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If smoke is detected within the equipment cooling system, what amber caution light will illuminate?

EQUIP SMOKE

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After selecting the ENG ANTI-ICE switches to ON in flight, the following indication is observed in steady state. What is true concerning the engine anti-ice system?

The left anti-ice valve disagrees with the ENG ANTI-ICE switch

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What is occurring when a wing anti-ice VALVE light momentarily illuminates amber?

valve is in transit

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Which of the following will cause the ENG ANTI-ICE light to illuminate?

When the cowl thermal anti-ice system has been inhibited due to a system failure

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Which of the following will cause the APU door (DOOR) light to illuminate while on the ground?

When the APU door is open and the APU is shut down

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What causes the REVERSER AIR/GRD light to illuminate?

Reverser air/ground protection is lost

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What mode of idle is selected by the ELEC if the aircraft is inflight below 30,400 feet, the flaps are not extended, the main gear is not down and locked, and the engine anti-ice is on?

Icing idle

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Duuring Engine Start, when can the start levers be moved to the idle detent after Motoring Blanks?

When N1 rotation is seen and N2 is at 25% or Max Motoring is above 20%

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What is indicated when the REVERSER COMMAND light illuminates?

Reverser is commanded in flight

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When conducting extended engine monitoring, what is the starter usage time limit?

5 minutes

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When the autopilot automatically disengages after 1 second of stick shaker activation, what happens to the flight director?

The flight director is temporarily removed from the PFD until airspeed is increased above the amber bar.

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On the 737 MAX, when will FCC logic inhibit autopilot nose up stabilizer trim commands?

When the trailing edge flaps are extended and airspeed is 3 knots or more into the amber bar.

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On the 737NG and 737 MAX, what condition is necessary for the Speed Trim System to operate?

Autopilot must not be engaged

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On the 737 MAX, what does illumination of the SPEED TRIM FAIL light indicate?

Failure of the Speed Trim System (Speed Trim function or MCAS function). If one function fails, the other function is inhibited for the remainder of the flight

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On the 737 MAX, which of the following is true ragarding the STAB TRIM PRI and STAB TRIM B/U cutout switches on the control stand?

When either switch is placed in the CUTOUT position, stabilizer trim inputs from the main electric, autopilot, and Speed Trim System (which includes the Speed Trim Function and MCAS function) are stopped.

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When the Speed Trim System is active on the 737NG or 737 MAX, what happens when the pilot uses the main electric stabilizer trim switches on the control wheel?

The Speed Trim System is overridden

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What is the purpose of the MCAS function on the /£/ MAX?

To increase control column forces by commanding the stabilizer in the nose down direction at elevated angle of attack (AOAs)?

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During which of the following conditions will the MCAS function not operate on the 737 MAX?

Flaps extended

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When may manual stabilizer trim operations become necessary?

During some non-normal flight conditions when called for by the appropriate Checklist

Approximately how many turns of the manual stabilizer trim wheel are required for a change of one stabilizer trim unit?

What should be verified prior to extending the manual trim wheel handles?

Both STAB TRIM cutout switches are in CUTOUT

Which of the following best describes manual operation of the stabilizer?

All of the above are true

What is the purpose of the Manouver Load Alleviation (MLA) system?

Decreases structural loads by partially retracting the speedbrakes

Which statement below correctly describes a function of the Landing Attitude Modifier (LAM)?

Designed to maintain accepteble nose landing gear contact margins for landing

What cause the SPEEDBRAKES EXTENDED light to illuminate in flight?

Speedbrake lever is beyond the ARMED position and a thrust lever is above idle for at least 15 seconds

What is required to activate the Elevator Jam Landing Assist system?

The Elevator Jam Landing Assist switch needs to be ON, actual flap position must be 1 or greater, and the autopilot disconnected

What does illumination of the ASSIST ON light indicate?

The Elevator Jam Landing Assist syatem is activated

What causes the SPOILERS light to illuminate on the Flight Control Panel?

One or more spoiler pairs are inoperative

When activated, what does the Emergency Descend Speedbrakes (EDS) system do?

Raises the speedbrakes to a higher-than normal position during the emergency descent manouver

How many large format Display Units (DU’s) are located on the flight deck?

Select where the Multi-Function Display (MFD) switches are located?

(Adjacent to the right FMC)

On which display will all of the following be located: flight number, SELCAL transponder code, airplane tail number, and date?

AUX

When an outboard Display Unit (DU) failure is sensed, the displays will automatically reconfigure, what happens to the AUX display?

Half sized AUX display moves to the inboard DU, and goes above the PFD

Which switch selects the Vertical Situation Display (VSD) inset on the Expanded MAP and Center Map modes on the Navigation Display (ND)?

(VSD switch?

Push the switch that allows the crew to manually enter the N1 Targets and V speed bugs on the Airspeed indicator?

(INFO sw)

Where is the clock switch located’

On the glareshield panel

Where are the engine indications normally displayed?

Captain’s or First Officer’s Inboard display unit

Select the switch that will move the engine indications to either the Captain’s or the First Officer’s inboard display unit?

( ↔ double arrow ENG TFR sw)

Where will the hydraulic systems information normally be shown after selecting the SYS switch on the Engine Display Control Panel?

Inboard dsisplay unit opposite the engine display

Select the location of the Captain’s Display Select Switches

(Located under the Captain’s outboard DU)

What Engine Display alert will display if the FMC determines a difference between the total sensed fuel quantity and the calculated fuel quantity values?

FUEL DISAGREE

Where is the fuel quantity source selected on the FMC?

FUEL PROGRESS page 5/5

What messages will show on the CDU scratchpad and appear on the Engine Display as amber alerts?

FUEL DISAGREE, INSUFFICIENT FUEL, and USING RSV FUEL

When is it possible for the fuel FILTER BYPASS lights to extinguish, if both have illuminated at any time during flight?

After engine shutdown on the ground

On FUEL PROGRESS page 5/5 the TOTALIZER fuel value is computed from what?

The Fuel Quantity Indication System (FQIS) gauge readings

Following a takeoff or a go around, check that the LANDING GEAR lever is in what position?

Select the location of the AUTO BRAKE switch

(between FMC’s)

Where is the NOSE WHEEL STEER switch located?

Center forward panel

When pushed, what does the LOCK OVRD switch do?

releases the landing gear lever lock

Drag and drop each item to the correct aircraft

(MAX: 69” fan, nose gear strut 8” longer, dual tail strobe/position lights)

Select the location of the BRAKE PRESS Accumulator Indicator

(between FMC’s)

With a single autopilot engaged, when does the YAW/ROLL ASYMMETRY alert appear?

Autopilot is above 75% of roll authority for more than 20 seconds

Select the bank pointer and slip/skid indication, with ROLL/YAW ASYMMETRY alert active, and the aircraft at 10° of bank

(amber empty pointer)

Select the item(s)that are an indication of an autopilot saturation event

unusual control wheel deflection ROLL/YAW ASYMMETRY alert ROLL AUTHORITY alert

What should be done when you see this on your PFD?

Roll left

What is the purpose of the pitch attitude latch?

to enable the use of high bank angles in recovering from a nose high upset without setting off the alerts

Select the bank pointer and slip/skid indication, in a roll upset condition, indicating that the bank angle is excessive

(solid red bank indivator, empty red slip indicator)

When the aircraft is significantly out of trim (control column is deflected in the roll axis) return the airplane to coordinated flight by doing the following in order.

Apply rudder to maintein flight path Accomplish the primary rudder trim technique Veryfy or set simmetrical thrust trim the rudder in the direction of the down side of the control wheel

Which of the following does not provide inputs for airspeed indications

Speed trim system

Which of the following may be an indication of an unreliable airspeed condition?

All of the above

On which panel can the First Officer’s stick shaker circuit breaker (STICK SHAKER RIGHT) be found?

P6 Panel

On which panel can the Captain’s stick shaker circuit breaker (STICK SHAKER LEFT) be found?

P18 Panel

When performing the Runaway Stabilizer Non-Normal Checklist, how should thrust be controlled after the autothrottle is disengaged?

Thrust should be controlled manually so that the airspeed remains within the range appropriate for the phase of flight.

When performing the Runaway Stabilizer Non-Normal Checklist, what can the pilot do to reduce control column forces

Use main electric stabilizer trim

During a runaway stabilizer condition, which of the following actions should be taken if the runawaycontinues after the autopilot is disengaged?

Move the STAB TRIM cutout switches to CUTOUT

During a runaway stabilizer condition, after the pilotflying disengages the autopilot and autothrottle, Control Column and Thrust Levers are used to control what?

Airplane Pitch Attitude and Airspeed

What can cause the SPEEDBRAKES EXTENDED light to illuminate in flight?

Speedbrake lever is beyond the ARMED position and thrust lever is above idee for at least 15 seconds.

737-MAX Flashcards

(73 cards)