Brainscape's Knowledge GenomeTM

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


See full index

737 Systems Test > ESV Study Guide Aircraft General, Air Conditioning, Flight Controls > Flashcards

ESV Study Guide Aircraft General, Air Conditioning, Flight Controls Flashcards

1
Q

The minimum pavement width required for a 180 degree turn is _____ feet.
79
88
57
65

A

79

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

What are the thrust ratings of the CFM 56-7B26 engine?
27K Bump
26K & 24K
22K
All of the above.

A

All of the above.

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

The system that controls and monitors engine parameters is the _____.
Autothrottles
FMC
EEC
FCC

A

EEC

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

The B737-800 is limited to a maximum takeoff weight of _____ pounds.
144,000
174,200
172,500
168,000

A

174,200

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

The B737-800 is limited to a maximum landing weight of _____ pounds.
146,300
136,000
150,000
137,000

A

146,300

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

What is the maximum operating altitude for the B737-800?
42,000 ft.
41,000 ft.
35,000 ft.
37,000 ft.

A

41,000 ft

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

What is the maximum zero fuel weight of the B737-800?
144,000
140,000
138,300
136,000

A

138,300

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

How many escape slides are on the B-737?
8, one at each entry and service door and one at each overwing exit.
6, one at each entry and service door and one at each wing.
2, only one at each forward entry and service door.
4, one at each entry and service door.

A

4, one at each entry and service door.

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

MAX: PSEU Light has been replaced with the ____ light:
MAINT
UNIT
ALERT
SYSTEM

A

MAINT

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

End of AIRCRAFT GENERAL

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

Beginning of AIR CONDITIONING

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

The ram air doors normally modulate to full OPEN when the aircraft is ____.

operating both packs in high flow

in flight with flaps not fully retracted or on the ground

in flight with flaps retracted

on the ground only

A

in flight with flaps not fully retracted or on the ground

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

The APU can supply bleed air for the pack up to ____.

41,000 feet under all conditions

20,000 feet or 12,000 feet if the APU is also providing electricity

17,000 feet or 10,000 feet if the APU is also providing electricity

20,000 feet or 8000 feet if the APU is also providing electricity

A

17,000 feet or 10,000 feet if the APU is also providing electricity

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

The mix manifold receives air from the ____.

left pack, right pack, and pre-conditioned air only

left pack, right pack, recirculation fan, and pre-conditioned air

right pack, recirculation fan, and pre-conditioned air only

left pack and right pack only
A

left pack, right pack, recirculation fan, and pre-conditioned air

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

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

Mix manifold

Both packs

Left pack

Right pack
A

Left pack

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

The primary purpose of the recirculation fans is to ____.

provide overheat detection down stream of the packs

reduce air conditioning pack load

increase airflow at greater cabin differential pressure

filter air for contaminants
A

reduce air conditioning pack load

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

Equipment cooling is provided for electronic equipment in the ____.

E & E bay and forward cargo compartment

E & E bay and flight deck area

E & E bay only

E & E bay and aft cargo compartment
A

E & E bay and flight deck area

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

The equipment cooling system has ___________ fan(s).

1 supply and 2 exhaust

2 supply and 1 exhaust

1 supply and 1 exhaust

2 supply and 2 exhaust
A

2 supply and 2 exhaust

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

Air from the preconditioned ground source enters the air conditioning system through the ____.

left pack valve

mix manifold

bleed valve

right pack valve
A

mix manifold

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

Engine low pressure bleed air is provided by the ____ stage, and engine high pressure bleed air is provided by the ____ stage air.

5th/12th

5th/9th

9th/13th

8th/12th
A

5th/9th

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

Each A/C pack has ____ controllers for pack temperature control.

1

2

3

4
A

2

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

If the primary equipment cooling fan fails, what indications would be displayed?

No indications - the standby fan turns on automatically.

Master Caution light and horn

Warning horn only (Ground Ops)

Master Caution light, the related equipment cooling OFF light, and the OVERHEAD annunciator light on the System Annunciator Panel
A

Master Caution light, the related equipment cooling OFF light, and the OVERHEAD annunciator light on the System Annunciator Panel

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

In the event of a single pack failure at altitude, the remaining pack is capable of maintaining cabin pressure and comfort at an airplane altitude of _____.

37,000 feet

41,000 feet

35,000 feet

25,000 feet
A

41,000 feet

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

The APU will supply bleed air for ____ pack(s) ____.
1) one, only in flight
2) both, on the ground
3) all three, in flight
4) both 1 & 2

A

both 1 & 2

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

Inflight, normal air conditioning system operation would be ____.

Both PACKs from APU

one pack from two engine bleed sources

two packs from one engine bleed source

each pack from its associated engine bleed source
A

each pack from its associated engine bleed source

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
26
Q

Which single bleed source is permitted to supply air to both packs on the ground?

None

Engine only

An engine bleed or APU.

The APU only.
A

The APU only.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
27
Q

The ram air system operates automatically to provide cooling for ____.

emergency cooling needs

the E & E compartment on the ground

the PACK heat exchangers

the right pack alternate air source
A

the PACK heat exchangers

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
28
Q

For maximum cooling (of the pack) the ram air inlet doors modulate toward the _________ .

a mid position

full open position

full closed position

ram air inlet doors do not modulate
A

full open position

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
29
Q

Deflector doors on the ram air system are used on the ground to __________.

prevent backflow of air over the heat exchangers

increase airflow through the ram air doors

prevent slush ingestion on takeoff or landing

allow for smooth air flow over the heat exchangers
A

prevent slush ingestion on takeoff or landing

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
30
Q

The deflector doors on the ram air system are fully extended ____.

on the ground only

on the ground, or inflight with the flaps extended

inflight with the flaps extended

inflight with the gear extended
A

on the ground only

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
31
Q

Zone temperature is controlled by introducing the proper amount of trim air into the______________.

individual zone supply duct

the mix manifold

the pack temp control valve

modulating the ram air inlet doors
A

individual zone supply duct

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
32
Q

Failure of the primary and standby flight deck zone temperature controls will cause the ____ to illuminate.

ZONE TEMP, MASTER CAUTION, and AIR COND annunciator lights

ZONE TEMP light only

PACK light

MASTER CAUTION light only
A

ZONE TEMP, MASTER CAUTION, and AIR COND annunciator lights

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
33
Q

Inflight, the forward cargo compartment is heated by air drawn around it by the ____.

1) outflow valves

2) recirculation fan system

3) equipment cooling system

4) Both 2 & 3

A

Both 2 & 3

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
34
Q

The temperature selector adjusts the desired zone temperature between a range of approximately ____ degrees.

75-85

60-80

65-85

70-80
A

65-85

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
35
Q

When either the primary or standby pack temperature controller fails, what indications will be displayed?

PACK and ZONE TEMP lights

PACK and MASTER CAUTION lights only

MASTER CAUTION, and AIR COND SYSTEM ANNUNCIATOR lights

PACK, MASTER CAUTION, and AIR COND SYSTEM ANNUNCIATOR lights on recall
A

PACK, MASTER CAUTION, and AIR COND SYSTEM ANNUNCIATOR lights on recall

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
36
Q

If the FWD or AFT Cab ZONE TEMP lights illuminate indicating an overheat, this will cause the associated ____ valve to close.

trim air modulating

emergency relief

pressure regulating

pack
A

trim air modulating

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
37
Q

The associated PACK light, Master Caution, and AIR COND annunciator will illuminate when ______.

pack trips caused by primary controller failure

all temperature selectors are placed OFF

pack controller failure and all temperature selectors placed OFF

pack overheats or dual pack controller failure
A

pack overheats or dual pack controller failure

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
38
Q

What fault indication(s) cannot be reset with the trip reset button?

BLEED TRIP OFF

PACK

ZONE TEMP

Wing body overheat
A

Wing body overheat

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
39
Q

The ZONE TEMP light, Master Caution, and AIR COND annunciator lights will illuminate for

an overheat in the duct leading to any of the three zones

a dual temperature controller failure in the CONTROL CAB zone

any single temperature controller failure in any zone during a RECALL test

any of the above
A

any of the above

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
40
Q

What will cause the left Wing-Body Overheat light to illuminate?

A bleed air duct leak in the left engine strut, left inboard wing leading edge, left air conditioning bay, keel beam or APU bleed air duct

A bleed air duct leak in the left wing anti-ice

Only a bleed air leak in the left air conditioning bay

A bleed air leak in the Trim-Air Manifold
A

A bleed air duct leak in the left engine strut, left inboard wing leading edge, left air conditioning bay, keel beam or APU bleed air duct

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
41
Q

Taking off with one or both PACK switches in HIGH is allowed with the engine bleed air switches on.

True

False
A

False

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
42
Q

While accomplishing the QRH procedure for a PACK light illuminated, why do you select a warmer temperature on all three temperature selectors?

Open the pack valve

This causes the pack to revert to high flow

Reduce the workload on the affected air conditioning pack

To extinguish the Pack light
A

Reduce the workload on the affected air conditioning pack

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
43
Q

Placing the trim air switch off will:

Cause both packs switch to high flow

Close the trim pressure regulating and shutoff valve

Cause the left pack temp to be controlled by the Cont Cab temp selector and the right pack by the Fwd and Aft temp selectors

Both 2 and 3 are correct
A

Both 2 and 3 are correct

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
44
Q

If a PACK light illuminates while performing a before taxi check, and resets with master caution reset, you should:

Perform the PACK QRH procedure

Consult the PACK MEL procedure for single channel fault

Contact load agent and perform an bleeds off takeoff

Both one and two are correct
A

Consult the PACK MEL procedure for single channel fault

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
45
Q

Landing with PACK switches in HIGH:

Will automatically revert to normal flow with flaps extended

Is not authorized with engine bleeds on

Is authorized if a QRH checklist calls for it

Both two and three are correct
A

Both two and three are correct

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
46
Q

In order to do a bleeds off takeoff:

Only the left PACK is switched to AUTO

The right PACK switch must turned OFF

Put both PACK switches to HIGH

Put both PACK switches to AUTO
A

Put both PACK switches to AUTO

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
47
Q

At the same time this light illuminates, what other indications do you get?

AIR COND will illuminate on the left System Annunciator Panel.

The right System Annunciator Panel will illuminate AIR COND on recall only.

The Master Caution lights illuminate and the right System Annunicator Panel shows AIR COND.

Only the Master Caution light will illuminate.
A

The Master Caution lights illuminate and the right System Annunicator Panel shows AIR COND.

48
Q

On the NG, both this light and the Master Caution lights are illuminated. What might happen to the left pack next under these circumstances?

The left pack valve will close due to pack underpressure.

The left pack valve will close if sensors have detected excessive temperature in that pack.

The left pack valve will close due to pack overpressure.

The left pack valve will stay open even if the left pack overheats.
A

The left pack valve will close if sensors have detected excessive temperature in that pack.

49
Q

Inflight, with the left pack valve closed due to excessive temperature, what other actions automatically occur in the Air Conditioning System?

The right pack switches to high air flow regardless of flap position.

The right pack switches to high air flow only if flaps are extended.

The right pack stays at normal air flow rate until the left Engine Bleed Air Switch is selected OFF.

The right pack switches to high air flow if flaps are up.
A

The right pack switches to high air flow if flaps are up.

50
Q

What effect will this condition have on the left pack?

Produces a preset temperature of 65 degrees

Output temperatures is controlled by Cont.Cab temperature selector

Output temperature is controlled by the Fwd and Aft temperature selectors

Pack output temperature cannot be controlled
A

Output temperatures is controlled by Cont.Cab temperature selector

51
Q

If this light illuminated only on Recall, ____.

both the Right and Left primary Electronic Controllers have failed

an overheat has occurred in the CONT Cabin Trim Air Supply Duct

both the Primary and Back-Up Flight Deck Zone Temperature Controllers have failed

only one of the CONT CAB Zone Temperature Controllers has failed
A

only one of the CONT CAB Zone Temperature Controllers has failed

52
Q

If this light extinguishes when the master caution light is pressed:

Air conditioning is not available from the left pack.

The system will operate normally.

A zone overheat was indicated.

The trim air system is inoperative.
A

The system will operate normally.

53
Q

If this light illuminated due to an overheat condition in the applicable zone supply duct, the Master Caution Lights will also illuminate; and ____.

the FWD CAB trim air modulating valve closes

none of the trim air modulating valves close

the CONT CAB trim air modulating valve closes

the AFT CAB trim air modulating valve closes
A

the CONT CAB trim air modulating valve closes

54
Q

With all the temperature selectors positioned as above, the packs will adjust for cabin demand. In this case, which statement is most correct?

The left pack controls will cause the left pack to maintain a fixed temperature of 75 degrees, and the right pack to maintain 65 degrees as measured at the pack temperature sensor.

The pack outputs will average.

System operation is normal.

The left pack controls will cause the left pack to maintain a fixed temperature of 65 degrees, and the right pack maintain 85 degrees as measured at the pack temperature sensor.
A

The left pack controls will cause the left pack to maintain a fixed temperature of 75 degrees, and the right pack to maintain 65 degrees as measured at the pack temperature sensor.

55
Q

End of AIR CONDITIONING

A
56
Q

Beginning of ACARS

A

The engine takeoff report is sent approximately 30 seconds after takeoff. If the PACK/BLEED configurations are set to inadvertently cause a CABIN ALTITUDE warning if left unchanged, after how long and how will the crew receive an alert?

45 seconds; SELCAL chime and NON-STANDARD BLEEDS/PACKS message is printed

2 minutes; SELCAL chime and NON-STANDARD BLEEDS/PACKS message is printed

45 seconds; SELCAL chime and BLEEDS and/or PACK lights will illuminate

2 minutes; SELCAL chime and NON-STANDARD BLEEDS/PACKS message displayed in scratchpad

57
Q

The engine takeoff report is sent approximately 30 seconds after takeoff. If the PACK/BLEED configurations are set to inadvertently cause a CABIN ALTITUDE warning if left unchanged, after how long and how will the crew receive an alert?

45 seconds; SELCAL chime and NON-STANDARD BLEEDS/PACKS message is printed

2 minutes; SELCAL chime and NON-STANDARD BLEEDS/PACKS message is printed

45 seconds; SELCAL chime and BLEEDS and/or PACK lights will illuminate

2 minutes; SELCAL chime and NON-STANDARD BLEEDS/PACKS message displayed in scratchpad

A

2 minutes; SELCAL chime and NON-STANDARD BLEEDS/PACKS message is printed

58
Q

What should be entered in the flap setting when trying to get FOS to search for a TPS using standard thrust?

Enter “13” in the flap field.

Leave blank or put in ‘99’ to allow search for standard thrust if possible

Push the Flap Request button

Push the ‘ANY’ button
A

Leave blank or put in ‘99’ to allow search for standard thrust if possible

59
Q

To obtain a TPS via ACARS, what is the minimum input information required for a TPS request?

Runway and OAT

No entries required. Just press the "TPS request" line select button

Runway and flap settings

Only Runway is required. FOS will optimize for any fields left blank
A

Only Runway is required. FOS will optimize for any fields left blank

60
Q

The initial load closeout will be sent to the ACARS printer. The only data uplinked to the FMS is _____?

ZFW and takeoff CG.

Only ZFW, all other values must be reset.

ZFW, takeoff CG, and V-speeds.

Nothing will be uplinked to the FMS, the TPS only outputs to the printer.
A

ZFW and takeoff CG.

61
Q

End of ACARS

A
62
Q

Beginning FLIGHT CONTROLS

A
63
Q

The primary flight controls consist of _____.

elevators, yaw damper, and ailerons

ailerons, elevators, and spoilers

stabilizer, rudder, and spoilers

ailerons, elevators, and rudder
A

ailerons, elevators, and rudder

64
Q

The primary flight controls are normally powered by hydraulic system(s) ____.

A and Standby

A only

A & B

B only
A

A & B

65
Q

____ can be extended by the Standby Hydraulic System in Alternate mode.

Elevators

Leading edge flaps/slats

Ailerons

Trailing edge flaps

A

Leading edge flaps/slats

66
Q

If a FEEL DIFF PRESS light illuminates, ____.

place both Flt Control switches to STBY RUDDER

immediately turn off the associated flight control switch

no crew action is required in flight. Continue normal operations.

depressurize the A or B hydraulic system
A

no crew action is required in flight. Continue normal operations.

67
Q

When the Flaps/Slats Electronics Unit (FSEU) detects a trailing edge asymmetry or skew condition, the FSEU closes the TE Flap Bypass Valve, ____.

illuminates the green EXT light, and displays a needle split on the flap position indicator

and displays a needle split on the Flap Position Indicator

and freezes the TE Flap needles in place, not showing a split

illuminates the amber FLT CONT annunciator light, and displays a needle split on the Flap Position Indicator
A

and displays a needle split on the Flap Position Indicator

68
Q

On aircraft 3AA - 3LB, load relief for the Trailing edge flaps is only provided for flaps ____.

30 and 40

25 and 30

25, 30 and 40

15
A

30 and 40

69
Q

During alternate flap operation, the TE flaps are positioned using ____ power.

electrical or hydraulic

manual

hydraulic

electrical
A

electrical

70
Q

The SPEED BRAKE lever will automatically move to the down detent, and all spoilers will retract, if ____.

the TOGA button is pressed

either throttle is advanced after landing

wheel spinup drops below 50 knots

wheel spinup drops below 60 knots
A

either throttle is advanced after landing

71
Q

In the event hydraulic systems A and B fail, the ailerons and elevators can be operated ____ and the rudder must be operated by the ____ system.

mechanically (manually), standby

automatically, mechanical

mechanically (manually), pneumatic

electrically, alternate
A

mechanically (manually), standby

72
Q

Normally, the ailerons, elevators, and rudder are powered by the _____.

A hydraulic system only

A & B hydraulic systems

Standby system

B hydraulic system only
A

A & B hydraulic systems

73
Q

Hydraulic System A and B pressure to the Main Rudder PCU is reduced at airspeeds above approximately ____ knots.

150

140

120

135
A

135

74
Q

If the aileron control system is jammed, the ____ can still fly the aircraft using the ____ after force is applied to the control wheels and they break free.

FO, ailerons

Captain, spoilers

Captain, control tabs

FO, spoilers
A

FO, spoilers

75
Q

With the trailing edge flaps at 1, the leading edge slats are ____.

in the extend position

in the full extend position

retracted

none of the above
A

in the extend position

76
Q

The horizontal stabilizer is normally powered _____, but may also be operated _____.

manually, electrically

automatically, pneumatically

electrically, manually

none of the above
A

electrically, manually

77
Q

On the ground, speed brakes normally use ____ to destroy lift and make braking more effective.

flight spoilers only

both flight and ground spoilers

ground spoilers only

compression of the left main landing gear strut to deploy the ground spoilers
A

both flight and ground spoilers

78
Q

Leading edge devices can be _____ by the Standby Hydraulic System if System B fails.

extended and retracted

extended

retracted

none of the above
A

extended

79
Q

The ____ of the Stab Trim Indicator corresponds to the allowable range of trim settings for takeoff.

green band

5 to 10 unit range marks

entire scale

APL NOSE UP selection settings
A

green band

80
Q

On aircraft 3AA - 3LB, the autoslat feature is available in flight _____.

with trailing edge flaps selected to 30-40

with trailing edge flaps selected to 1, 2, or 5

at landing flap settings

at all flap settings
A

with trailing edge flaps selected to 1, 2, or 5

81
Q

In aircraft 3AA-3LB, the LE devices will go to the full extend position when you select _____ or greater with the flap handle.

5

10

1

2
A

10

82
Q

If we move the flap lever from 5 to 10, but the leading edge devices all stay in the extend position, the ____ Light will be illuminated.

LE FLAPS TRANSIT

LE FLAPS EXT

AUTO SLAT FAIL

SLATS EXTEND
A

LE FLAPS TRANSIT

83
Q

The maximum altitude for extension of flaps is ____ feet.

30,000

11,000

20,000

15,000
A

20,000

84
Q

Leading edge devices are normally operated by ____.

Hydraulic System B only

Hydraulic System A only

Standby Hydraulic System

Hydraulic Systems A and B
A

Hydraulic System B only

85
Q

Roll control is normally provided by the ailerons, assisted by _____.

flight spoilers

ground spoilers

autoslats

both 1 & 2 above
A

flight spoilers

86
Q

With the SPEED BRAKE Lever in the DOWN detent, how can the speedbrakes be deployed on landing?

The pilot can raise the lever manually.

The speedbrake is not available.

The speedbrake lever will automatically move to full up position when the reverse thrust levers are moved to reverse when above 60 knots.

Both 1 and 3 are correct.
A

Both 1 and 3 are correct.

87
Q

When using the SPEED BRAKE in flight, the speedbrake lever should ____.

be moved to any setting

be moved to the UP position

be moved to the DOWN position

not be moved beyond the flight detent
A

not be moved beyond the flight detent

88
Q

The LE FLAPS TRANSIT light illuminated indicates _____. Select the most correct answer.

leading edge devices are in transit

leading edge devices are not in the programmed position with respect to the trailing edge flaps

a leading edge device asymmetry

any of the above
A

any of the above

89
Q

If wheel spin-up is not detected by the air/ground sensors, the flight spoilers will deploy when ____.

any main gear strut compresses

thrust reverser extension occurs

the right main gear strut compresses

the left main gear strut compresses
A

any main gear strut compresses

90
Q

Prior to what altitude should the Speed Brakes be Down or Armed?

1000 FT AGL

500 FT AGL

2500 FT AGL

5000 FT AGL
A

1000 FT AGL

91
Q

MAX 8: Fly-by-wire Spoiler system provides the following new features.

Maneuver Load Alleviation (MLA), Landing Attitude Modifier (LAM) and Coordinated Flare Cue landing assistance.

Emergency Descent Spoilers (EDS).

Elevator Jam Landing Assist System.

Both 2 and 3 above.
A

Both 2 and 3 above.

92
Q

MAX 8: Emergency Descent Speed Brakes system (EDS):

Generates additional drag to allow the Max to capture and maintain a glidepath similar to the NG.

Armed when the airplane is above 30,000 feet and the cabin altitude warning is active.

Fully automatic with operation transparent to the crew.

Both 2 and 3 above.
A

Both 2 and 3 above.

93
Q

MAX 8: The Spoiler Control Electronics Unit (SCE):

One sensor is applied to the Captains yoke and provides input for Coordination with the HUD Flare Cue during landing.

Translates signals from the speedbrake lever position sensor, the First Officer’s control wheel and other airplane data inputs.

Must be selected on during initial FMC setup.

Both 1 and 2 are correct.
A

Translates signals from the speedbrake lever position sensor, the First Officer’s control wheel and other airplane data inputs.

94
Q

MAX 8: The Spoiler light indicates:

The ground spoilers are armed.

A fault in the spoiler system.

The ground spoilers are deployed.

The flight spoilers are deployed.
A

A fault in the spoiler system.

95
Q

MAX 8: The Elevator Jam Landing Assist Switch is located on:

Aft Overhead Panel

E/E Compartment

First Class Seating Area

Fwd Attendant Panel
A

Aft Overhead Panel

96
Q

During the origination preflight, this light illuminates after the IRS Mode Selectors are moved to NAV. The “Flight Control Panel . . . CHECK” item is accomplished by _____

calling Maintenance. The Speed Trim System has failed

resetting the Stab Trim to Zero

doing nothing. This is a normal indication while the IRUs are aligning

resetting the light with the Press-To-Test Switch
A

doing nothing. This is a normal indication while the IRUs are aligning

97
Q

This light, and the Master Caution Lights, illuminate during initial taxi-out.

No action is required. The Speed Trim System only works with the autopilot engaged.

Reset the SPEED TRIM FAIL light by setting the parking brake.

Check the MEL or call Maintenance. There is a dual channel failure of the Speed Trim System.

No action is required. The Speed Trim System will operate 10 seconds after takeoff.
A

Check the MEL or call Maintenance. There is a dual channel failure of the Speed Trim System.

98
Q

If, instead, this light illuminates once you are in flight, the autopilot ____.

can only be engaged in CWS P Mode

if engaged, has now disengaged and cannot be re-engaged

is still fully operational

has lost the ability to trim the aircraft
A

is still fully operational

99
Q

While extending the flaps electrically through the 5 degree flap position, if you still observe these lights, ____.

the flap gage is indicating an erroneous position

there is a disagreement between the flap handle and the LEDs

the LEDs are still in transit

the flaps have not approached the flaps 10 degree position or beyond in aircraft 3AA-3LB
A

the flaps have not approached the flaps 10 degree position or beyond in aircraft 3AA-3LB

100
Q

When the flaps have been lowered to 15 degrees with the ALT system and a missed approach has been executed, the ____.

TE flaps can be retracted with the ALT system but not the LE devices

TE and LE flaps will retract with the ALT system

TE flaps can be retracted with the ALT system while the LE devices will retract with the PTU

flaps cannot be retracted
A

TE flaps can be retracted with the ALT system but not the LE devices

101
Q

When positioning the flaps for takeoff from UP to 1, the crew noticed this condition. What could have caused this malfunction?

Skewed L.E. Devices

Jammed Rudder

Jammed L.E. Devices

Skewed T.E. Flap
A

Skewed T.E. Flap

102
Q

The ____ protects the flaps in this condition.

FSEU

DEU

EEC

FCC
A

FSEU

103
Q

The FSEU protects the flaps during ____ operation.

Alternate Flap

Normal Flap

Speed Trim operation

both Normal and Alternate Flap
A

Normal Flap

104
Q

As you advance the thrust lever for takeoff, would you get an intermittent horn with the LEDs positioned as indicated?

No. The TE Flaps are set at 5 Degrees.

No. The LEDs are not part of the takeoff warning system.

No. If the parking brake is released.

Yes. The LEDs are not in the proper position.
A

Yes. The LEDs are not in the proper position.

105
Q

The previous condition has now been corrected. The takeoff warning sounds again. Why?

Stab Trim in green band and Stab Trim Cutout Switches in normal.

Stab Trim not in green band or parking brake lever set.

Parking brake released and RTO not selected.

Stab trim in green band and auto throttle switch not armed.
A

Stab Trim not in green band or parking brake lever set.

106
Q

With the TE Flaps and Leading Edge Devices in the correct position, the Stab Trim set in the green band, the parking brake released, and the speed brake handle stowed you still have a Takeoff Warning Horn. What other scenario(s) could be causing this?

Spoiler(s) are not fully down.

Trailing Edge Flaps are at a 15 degree setting.

An Overwing Exit Door did not lock properly.

You must press TO/GA to silence the horn.
A

Spoiler(s) are not fully down.

107
Q

During normal operations with these two FLT CONTROL switches in the ON position, they control pressure to the respective ____.

aileron only

rudder, aileron, and elevator

rudder only

elevator only
A

rudder, aileron, and elevator

108
Q

After loss of system A, the QRH directs you to move the A FLT CONTROL switch to STBY RUD. This action will pressurize the ____.

landing gear transfer unit

A system PCU

Standby hydraulic pump and Standby rudder PCU

aileron, elevator, and rudder systems
A

Standby hydraulic pump and Standby rudder PCU

109
Q

With the loss of B Hydraulic System, the yaw damper will ____.

cause the Yaw Damper Switch to trip off

be inoperative causing the Yaw Damper Light to illuminate

remain operating from the A hydraulic System

be inoperative, but the Yaw Damper Light will not be illuminated until the Flt control B switch is moved to STBY RUD
A

be inoperative, but the Yaw Damper Light will not be illuminated until the Flt control B switch is moved to STBY RUD

110
Q

Placing the B FLT CONTROL switch to STBY RUD will cause the YAW DAMPER switch to ____.

allow you to reconnect the Yaw Damper by selecting the Yaw Damper switch on

pressurize the A Hydraulic system making it fully operational

trip OFF and illuminate the Yaw Damper Light

operate the standby FSEU
A

trip OFF and illuminate the Yaw Damper Light

111
Q

Subsequently, the A Hydraulic System also fails. How would you gain control of the Standby Yaw Damper?

Check that the B System Low Pressure Light is Illuminated.

You cannot recover the Standby Yaw Damper with a Feel Diff Light illuminated.

Turn the Yaw Damper Switch ON.

Ensure both A and B Flight Control Switches are in the Standby Rudder Position and then place the Yaw Damper Switch ON.
A

Ensure both A and B Flight Control Switches are in the Standby Rudder Position and then place the Yaw Damper Switch ON.

112
Q

With the STAB TRIM positioned as indicated, what would happen when the throttles are advanced for TO with all other systems set properly?
radio A steady horn would sound.
radio An intermittent horn would sound.
radio There would be no alert since this is the proper setting for TO.
radio The trim would automatically go to the proper setting.

A

There would be no alert since this is the proper setting for TO.

113
Q

If the trim was set to 10 units nose up and then the throttles are advanced for takeoff, what alert would occur?

A steady horn

An intermittent warning horn and takeoff config lights

A flashing red light

A Stab out of Trim Light
A

An intermittent warning horn and takeoff config lights

114
Q

While applying nose down trim, the electric trim stops. How can you continue to trim if you need more nose down trim?

Have the other pilot push the yoke forward.

Speed trim system will activate and apply trim.

Trim manually, using the manual trim wheel.

Engage autopilot and trim again.
A

Trim manually, using the manual trim wheel.

115
Q

End of FLIGHT CONTROLS

A

737 Systems Test (27 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2025 Bold Learning Solutions. Terms and Conditions