Questions

Question 1

The STAB OUT OF TRIM (amber) light is armed when? ___________ Illuminated when?____________

Answer 1

A/P engaged.
A/P is not trimming the stabilizer properly.

Question 2

If windshear is encountered during an ILS approach, what will the FD command?

Answer 2

Glideslope and LOC; no windshear guidance will be provided until TO/GA is pressed.

Question 3

After the VOR/LOC and G/S are both captured, the APP mode can be exited by:

Answer 3

Pushing a TO/GA switch,

disengaging the A/P and turning off both FD switches,

retuning a VHF NAV receiver.

Question 4

The Bank Angle Selector (rotate) sets a maximum Bank Angle for AFDS operation in what modes?

Answer 4

HDG SEL or VOR modes

Question 5

The Speed Trim improves flight characteristics during manual operations at ______, _____, _____, and ______.

Answer 5

Low Airspeed
Low Gross Weight
Aft CG
High thrust

Question 6

How many degrees of control wheel displacement initiates spoiler deflection?

Answer 6

When the control wheel is displaced more than approximately 10 degrees (1.6 units), spoiler deflection is initiated.

Question 7

What happens when a FLT CONTROL switch is positioned to STBY RUD?

Answer 7

It activates the Standby Hydraulic System and opens the Standby Rudder Shutoff Valve (allowing Standby Hydraulic System pressure to the Standby Rudder PCU)

Question 8

In the MAX, the rudder pressure will return to normal system operating pressure when:

Answer 8

An engine failure is detected or

with both engines operating, Airspeed is reduced below approximately 132 kts.

Question 9

In the MAX, a SPOILERS (amber) light indicates the Spoiler Control Electronic Unit has discovered what?

Answer 9

A Spoiler System fault.

Question 10

The STANDBY PWR OFF (amber) light when Illuminated, indicates one or more of the following busses are unpowered:
________ or ________ or ________

Answer 10

AC Standby Bus
DC Standby Bus
Battery Bus

Question 11

When does the BAT DISCHARGE (amber) light illuminate?

Answer 11

When excessive battery discharge is detected on the main battery and/or auxiliary battery.

Question 12

When will the Generator DRIVE (amber) light illuminate?

Answer 12

When there is an IDG failure

Engine shutdown

IDG disconnected by activation of the DISCONNECT switch

IDG auto-decouple due to high oil temperature (182C)

Question 13

How long will two full charged batteries provide standby power?

Answer 13

Minimum of 60 minutes.

Question 14

What does the BUS TRANSFER switch, in AUTO (guarded) position allow?

Answer 14

Allows the Bus Tie Breakers (BTB) to operate automatically to maintain power to AC transfer busses from any operating generator or external power.

Question 15

The Center Switch on the EFIS control panel must be in which mode for the VSD to display?

Answer 15

Map Mode.

Question 16

The AOA Disagree Alert (amber) indicates the left and right AOA values disagree by more than _____ for more than _____ continuous seconds.

Answer 16

10°
10 seconds

Question 17

When does the ALTITUDE DISAGREE (amber) alert appear?

Answer 17

When CA and FO altitude indications disagree by more than 200 ft for more than 5 continuous seconds.

Question 18

A vertical (amber) bar extending up from the top of the Minimum Speed Bar indicates what on the PFD?

Answer 18

Minimum Maneuvering Speed (Vmvr)

Question 19

How is HGS controlled on the MAX?

Answer 19

MCDU

Question 20

The purpose of the PTU is to provide Hydraulic System B fluid at a flow rate (approximately 6.5 GPM) and pressure sufficient to provide normal rates of operations for the ______ and _______ in the event the Hydraulic System B Engine Driven Pump output pressure drops below a specific value.

Answer 20

Autoslats
Leading Edge Devices (LED)

Question 21

When is the automatic operation for Standby Hydraulic System initiated?

Answer 21

When flaps are extended, and

airborne, or wheel speed greater than 60 kts, and

loss of System A or B while FLT CONTROL switch positioned to ON,

OR:

the main PCU Force Fight Monitor (FFM) trips.

Question 22

What pressurizes both System A and B hydraulic reservoirs?

Answer 22

Regulated Bleed Air

Question 23

When do the letters RF (white) appear?

Answer 23

REFILL (RF) is displayed when hydraulic quantity is below 76%. Valid only when AC is on the ground with both engines shutdown or after landing with flaps up during taxi in.

Question 24

How do you display the Hydraulics in the MAX?

Answer 24

MFD SYS Button.

Question 25

The Alternative Brake System is powered by ________

Answer 25

Hydraulic System A

Question 26

With RTO selected, if the takeoff is rejected prior to wheel speed reaching 90 kts: ______ and ________

Answer 26

Autobraking is not initiated

The RTO autobrake function remains armed.

Question 27

How is braking available if both Hydraulic Systems A and B are lost?

Answer 27

Trapped hydraulic pressure in the Brake Accumulator (system B) can still provide several (6) brake applications or parking brake application for 8 hours.

Question 28

In the MAX, what are the positions of the Landing Gear Lever?

Answer 28

Up
Down

Question 29

What kind of brake discs does the MAX have?

Answer 29

Carbon

Question 30

The DC Fails (amber) light, when illuminated, indicates ________

Answer 30

DC power for related IRS is not normal.

Question 31

What are indications of a left FMC failure?

Answer 31

FMC alert light illuminates

MENU page appears on both CDUs

VTK appears on left nav display

LNAV and VNAV will disengage, but can be reengaged if AP B is in use or is selected.

Question 32

LNAV will engage when ______

Answer 32

Laterally positioned within 3 nm of the active route leg.

Question 33

In the MAX, the FMC Alert light indicates which new indication?

Answer 33

Runway Disagree

Question 34

In the MAX, what fuel indications are on the Fuel Progress Page 5/5?

Answer 34

APU Fuel Used
Totalizer <ACT>
Calculated</ACT>