CQ 25 Flashcards

1
Q

When does the Master Caution light illuminate for a single/simple
fault?

A

Master Caution Recall

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2
Q

The PSU supplies oxygen, per seat row, for how many minutes?

A

12 Minutes

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3
Q

When do the overwing emergency exit doors locks engage?

A

A minimum of three of the four entry/service doors are closed, and either engine is running, and the aircraft
air/ground logic indicates that the aircraft is in the air or both thrust levers are advanced.

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4
Q

What is the function of the Electric Air Compressor?

A

This supplies pressurized air to the Potable Water Tank when the pneumatic system is insufficient and is powered by Main Bus number 1.

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5
Q

With both the LED Landing lights ON and Taxi Light ON/AUTO the taxi light function is ______ by the landing light function.

A

the taxi light function is overridden by the landing light function.

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6
Q

Pressurization Panel: The AUTO FAIL (amber) light illuminates if any
of the following conditions occur: (name one)

A
  1. Loss of DC power or Controller fault
  2. Outflow Valve control fault
  3. Excessive differential pressure
  4. Excessive rate of cabin pressure change
  5. High cabin Altitude.
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7
Q

The Wing Body Overheat (amber) light, when illuminated, indicates
what?

A

an overheat has been detected

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8
Q

Thrust must be limited to idle with the __________ light illuminated.

A

Dual Bleed

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9
Q

What does a Bleed Trip Off light indicate?

A

excessively high bleed air Temperature (254⁰C)
OR
excessively high Pressure(220psi) and may be reset with the trip/reset button if conditions permit.

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10
Q

The MAX pneumatic systems use ______ and _______ stage bleed
air.

A

4th and 10th stage

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11
Q

What are your indications when you receive a SELCAL? _______ and
_________ .

A

SELCAL white light and Two-tone chime

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12
Q

Which radio defaults to DATA on power up and at power down?

A

VHF 3

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13
Q

The Radio Tuning Panel (RTP) displays __________ when the selected radio is not available.

A

FAIL - FAIL

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14
Q

What does an illuminated Offside Tuning (white) Light indicate?

A

The radio normally associated with this panel is being tuned by another radio tuning panel, or the radio tuning panel is being used to tune a radio not normally
associated with this radio tuning panel.

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15
Q

On the MAX, where is the SELCAL light?

A

Just below the Mic selector, on the ACP.

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16
Q

With the Ignition Select System at IGN R, what is the power source?

A

AC Standby Bus

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17
Q

What will remove an amber ENG FAIL indication?

A

The engine recovers,
the start lever is moved to CUTOFF, or the fire switch is pulled.

18
Q

What does the THRUST crew alert on the Engine Display indicate?

A

The associated engine thrust is more or less than the commanded thrust. THRUST is displayed in conjunction with the N1 command sector illuminating
amber.

19
Q

The Thrust Mode Display (green) indicates R-TO. What mode is
active?

A

Reduced Takeoff

20
Q

In the MAX, how long should you wait after the APU GEN OFF BUS
(blue) light extinguishes before the positioning the Battery Switch to
OFF? (CW)

21
Q

During a FAULT/INOP test, the failure of the FAULT light to illuminate
indicates _________.

A

the Fault Monitoring System is inoperative

22
Q

If the OVHT DET switch is positioned to A or B, the system operates
as _______.

A

a single loop system.

23
Q

Rotating an Engine Fire Switch in one direction
____________________.

A

electrically fires a squib, discharging the extinguisher into the related engine

24
Q

How long do we have fire suppression after the Cargo DISCH switch
is pushed?

A

195 minutes

25
Q

The MAX has how many wheel well fire detector loops?

26
Q

The Fuel LOW (amber) Alert is displayed when the respective Main
Tank fuel quantity is less than _________ for greater than _________.

A

2000 lbs, 30 seconds

27
Q

Aside from a leak, what could cause a progressive fuel imbalance?

A

the Crossfeed Valve open,
no Center Tank fuel feed,
Main Tank Fuel Pumps operating within the normal pump output pressure tolerances

28
Q

Opening the Crossfeed valve inflight, ______________.

A

allows fuel from a main tank, with operating fuel pumps, to provide fuel to both engines

29
Q

IMBAL (amber) alert means the main tanks differ by more than
______ pounds.

30
Q

The FUEL FLOW (amber) Alert is displayed when_______ on the
MAX.

A

when the difference between actual engine fuel flow rate and the FMS expected fuel flow rate exceeds the
predetermined FMC threshold value for 5 continuous minutes

31
Q

The COWL ANTI-ICE (amber) light illuminates due to _____________.

A

Excessive pressure in the duct.

32
Q

Which leading devices are on the Wing Anti-ice system?

A

3 inboard Leading Edge slats

33
Q

A TAI (amber) indication to the left of an N1 display on the Upper
Display Unit indicates:

A

the Cowl Anti-Ice valve failed to move to the position selected by the ENG ANTI-ICE switch.

34
Q

Positioning the WING ANTI-ICE switch to ON in flight______________?

A

opens both control valves and sets stall warning logic for icing conditions

35
Q

On the MAX, how is the engine core anti-ice controlled?

A

Automatically, by the EEC

36
Q

With a TCAS Pitch Command on the PFD displayed, keep the aircraft symbol _______ the area indicated by the red lines.

37
Q

If not previously commanded on, Predictive Windshear for takeoff
automatically turns on by__________.

A

advancing thrust levers beyond 53 degrees.

38
Q

The GPWS provides BANK ANGLE alert when the roll angle exceeds
___⁰, ___ ⁰, and ___ ⁰?

A

35 ⁰, 40 ⁰, and 45 ⁰

39
Q

Which button do I select on the radar panel to display turbulence?

40
Q

The MAINT (amber) light, when illuminated, indicates _________.

A

a system fault exists that must be reviewed by Maintenance.

41
Q

ETOPS:
Limited Overwater:
Extended Overwater:

A

ETOPS: 180 minutes
Limited Overwater: 50nm (except Gulf of America, Gulf of California and Southeast coast
Extended Overwater: 60 minutes from adequate airport

42
Q

Flag Fuel:
ETOPS Fuel:

A

Flag Fuel:
-fuel to destination
-Fuel to alternate
-30 minutes of holding fuel
-10% of flight time to destination
ETOPS Fuel
-CP to diversion
-6 scenarios, decomp/1-eng decomp/1-eng
-If FLAG doesn’t meet this, then look for ETOPS add