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CQ 2024 > Jeopardy > Flashcards

Jeopardy Flashcards

1
Q

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

A

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

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2
Q

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

A

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

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3
Q

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

A

pushing a TO/GA switch, disengaging A/P and turning off both F/D
switches, retuning a VHF NAV receiver.

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4
Q

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

A

HDG SEL or VOR modes.

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5
Q

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

A

Low Airspeed, Low Gross Weight, Aft center of gravity, and high
thrust.

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6
Q

How many degrees of control wheel displacement initiates spoiler
deflection?

A

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

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7
Q

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

A

It activates the Standby Hydraulic System and

opens the Standby
Rudder Shutoff Valve

(allowing Standby Hydraulic System pressure
to the Standby Rudder PCU)

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8
Q

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

A

An engine failure is detected or with both engine operating, airspeed is reduced below approx. 132 kts.

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9
Q

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

A

A Spoiler System Fault.

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10
Q

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

A

AC Standby Bus or DC Standby Bus or Battery Bus

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11
Q

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

A

AC Standby Bus or DC Standby Bus or Battery Bus

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12
Q

When does the BAT DISCHARGE light (amber) illuminate?

A

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

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13
Q

When will the Generator DRIVE (amber) light illuminate?

A

When there is a IDG failure / engine shutdown /IDG
disconnected by activation of the DISCONNECT switch/ IDG
auto-decouple due to high oil temperature (182 C).

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14
Q

How long will two fully-charged batteries provide standby power?

A

Two fully-charged batteries have sufficient capacity to provide
standby power for a minimum of 60 minutes.

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15
Q

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

A

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

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16
Q

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

A

MAP

17
Q

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

A

10°, 10

18
Q

When does the ALTITUDE DISAGREE (amber) alert appear?

A

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

19
Q

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

A

Minimum Maneuvering (Vmvr) Speed

20
Q

How is the HGS controlled on the MAX?

A

MCDU

21
Q

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-Drive Pump output press drops below a specific value.

A

Autoslats Leading Edge Devices (LED)

22
Q

When is the automatic operation for Standby Hydraulic System initiated?

A

When flaps are extended, 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.

23
Q

What pressurizes both System A and System B hydraulic reservoirs?

A

Regulated Bleed Air

24
Q

When do the letters RF (white) appear?

When is it valid?

A

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

25
Q

How do you display the Hydraulics in the MAX?

A

MFS SYS Button

26
Q

The Alternate Brake System is power by _________.

A

Hydraulic System A

27
Q

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

A

autobraking is not initiated the RTO autobrake function remains armed

28
Q

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

A

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

29
Q

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

A

Up, Down

30
Q

What kind of brake discs does the MAX have?

A

Carbon

31
Q

The DC Fail (amber) light, when illuminated, indicates _________.

A

DC power for the related IRS is not normal.

32
Q

What are indications of a left FMC failure?

A

FMC alert light illuminates. The MENU page appears on both
CDUs. VTK appears on the left navigation display. LNAV and VNAV
will disengage, but can be reengaged if Autopilot B is in use or is
selected.

33
Q

LNAV will engage when _______.

A

laterally positioned within 3nm of the active route leg.

34
Q

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

A

Runway Disagree

35
Q

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

A
  1. APU Fuel Used
  2. Totalizer <ACT></ACT>
  3. Calculated

CQ 2024 (9 decks)

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