Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

UAL B737 Study (2.27.2024) > 737 MAX Differences > Flashcards

737 MAX Differences Flashcards

1
Q

(FM 6.20.30) If smoke is detected within the equipment cooling system, what amber caution light will illuminate?

A

EQUIP SMOKE

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

(FM 6.20.10) How is the operation of the bleed air system controlled?

A

Electronically controlled

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

(FM 6.20.40) Where are the RAM DOOR FULL OPEN lights located on the 737 MAX?

A

These lights are not on the MAX

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

(FM 6.20.20) What causes both of the BLEED lights to illuminate at the same time?

A

Both Bleed switches in the OFF position after takeoff or go-around

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

(FM 6.20.10) Engine bleed air is extracted from what stages of the compressor?

A

4th and 10th

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

(FM 6.20.10) In flight, how many air conditioning packs is one engine bleed capable of
supplying on the 737 MAX?

A

2

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

(FM 6.20.40) What causes both PACK lights to illuminate at the same time?

A

Both PACK switches in the OFF position after takeoff

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

(FM 6.30.20) Which of the following will cause the ENG Anti-Ice light to illuminate?

A

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

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

(FM 6.30.20) 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?

A

The left engine anti-ice valve disagrees with the ENG Anti-ice switch.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

(FM 6.30.20) What is occurring when the wing anti-ice VALVE light momentarily illuminates amber?

A

Valve is in transit.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

(FM 6.70.40) What can cause the APU door (DOOR) light to illuminate while on the ground?

A

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

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

(FM 6.70.20) What is indicated when the REVERSER COMMAND light illuminates?

A

Reverser is commanded in flight.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

(FM 6.70.20) What causes the REVERSER AIR/GRD light to illuminate?

A

Reverser air/ground protection is lost.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

(FM 3.50) During engine start the start levers are moved to the idle detent when the MOTORING indication blanks and N1 rotation is seen, and the N2 reaches what percent?

A

25%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

(FM 1.30) When conducting extended engine motoring, what is the starter usage time
limit?

A

5 minutes.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

(FM 6.70.10) What mode of idle is selected by the EEC if the aircraft is inflight below 30,400 feet, the flaps ae not extended, the main gear is not down and locked, and the engine anti-ice is on?

A

Icing idle

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

(FM 6.90.10) Describe the function of the Landing Attitude Modifier (LAM)?

A

Designed to maintain acceptable nose landing gear contact margins for landing.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

(FM 6.90.10) What is the purpose of the Maneuver Load Alleviation (MLA) system?

A

Decreases structural loads by partially retracting the speedbrakes.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

(FM 6.90.20) What can cause the SPEEDBRAKES EXTENDED light to illuminate in
flight?

A

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

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

(FM 6.90.10) When activated, what does the Emergency Descent Speedbrakes (EDS) system do?

A

Raises the Speedbrakes to a higher than normal position during the emergency descent maneuver.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

(FM 6.90.10) What is required to activate the Elevator Jam Landing Assist system?

A

The Elevator Jam Landing Assist switch must be selected ON, the flap position must be 1
or greater and the autopilot must be disconnected.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

(FM 6.90.20) What does illumination of the ASSIST ON light indicate?

A

The Elevator Jam Landing Assist system is activated.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

(FM 6.90.20) What causes the SPOILERS light to illuminate on the Flight Control Panel?

A

One or more spoiler pairs are inoperative.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

(FM 6.100.20) Where is the location of the Captain’s Display Select Switches?

A

Located under the Captain’s outboard DU.

25
Q

(FM 6.100.10) How many large format Display Units (DU’s) are located on the flight deck?

A

4

26
Q

(FM 6.100.20) What switch that allows the crew to manually enter the N1 Targets and V speed bus on the Airspeed indicator.

A

INFO

27
Q

(FM 6.100.20) On which display will all of the following be located: flight number,
SELCAL, transponder code, airplane tail number, and date?

A

AUX

28
Q

(FM 6.100.20) Where the Multi-Function Display (MFD) switches are located?

A

Adjacent to the right MCDU

29
Q

(FM 6.100.20) Where are the engine indications normally displayed?

A

Captain’s or First Officer’s Inboard display unit

30
Q

(FM 6.100.20) When an outboard Display Unit (DU) failure is sensed, the displays will
automatically reconfigure, what happen to the AUX display?

A

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

31
Q

(FM 6.100.20) Where will the hydraulic systems information normally be shown after
selecting the SYS switch on the Engine Display Control Panel?

A

The inboard display unit opposite the engine display

32
Q

(FM 6.100.20) Where is the clock switch located?

A

On the glareshield panel.

33
Q

(FM 6.100.20) Which switch selects the Vertical Situation Display (VSD) inset on the
Expanded MAP and Center Map modes on the Navigation Display (ND).

A

VSD (in the center)

34
Q

(6.100.20) Which switch will move the engine indications to either the
Captain’s or the First Officer’s inboard display unit?

A

ENG TFR (center)

35
Q

(FM 6.120.30) What messages will show on the CDU scratch pad and appear on the Engine Display as amber alerts?

A

FUEL DISAGREE, INSUFFICIENT FUEL, and USING RSV FUEL

36
Q

(FM 6.120.20) On FUEL PROGRESS page 5/5 the TOTALIZER fuel value is computed
from what?

A

FQIS gauge readings

37
Q

(FM 6.120.20) Where is the fuel quantity source selected on the FMC?

A

Fuel Progress page 5/5

38
Q

(FM 6.120.20) When is it possible for the fuel FILTER BYPASS lights to extinguish, if
both have illuminated at any time during flight?

A

After engine shutdown on the ground.

39
Q

(FM 6.120.30) What Engine Display alert will display if the FMC determines a difference between the total sensed fuel quantity and the calculated fuel quantity values?

A

FUEL DISAGREE

40
Q

(FM 6.140.20) When pushed, what does the LOCK OVRD switch do?

A

Releases the landing gear lever lock.

41
Q

(FM 3.100) Following a takeoff or a go around, check that the LANDING GEAR lever is
in what position?

A

Up

42
Q

(FM 6.140.20) Where is the NOSE WHEEL STEER switch located?

A

Center forward panel

43
Q

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

A

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

44
Q

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

A

Use main electric stabilizer trim.

45
Q

During a runaway stabilizer condition, which of the following actions should be taken if the
runaway continues after the autopilot has been disengaged?

A

Move both STAB TRIM cutout switches to CUTOUT.

46
Q

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

A

Airplane Pitch Attitude and Airspeed.

47
Q

When may manual stabilizer trim operations become necessary?

A

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

48
Q

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

A

15.

49
Q

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

A

Both STAB TRIM cutout switches are in CUTOUT.

50
Q

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

A

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

51
Q

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

A

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

52
Q

Does the Speed Trim System provide inputs for airspeed indications?

A

No

53
Q

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

A

Autopilot NOT engaged

54
Q

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

A

Failure of the Speed Trim System (Speed Trim function or MCAS function). If one function fails, both functions (the Speed Trim function and MCAS function) are inoperative for the remainder of the flight.

55
Q

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

A

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.

56
Q

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

A

The Speed Trim System is overridden.

57
Q

What is the purpose of the MCAS function on the 737 MAX?

A

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

58
Q

Will the MCAS function operate on the 737 MAX if the flaps are extended?

A

No

59
Q

Wait times for Battery switch Off (FM 3.230.2)

A

NG - 120 seconds after APU off

Max - 5 minutes after APU GEN OFF BUS light.

UAL B737 Study (2.27.2024) (22 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions