Airplane General

Question 1

When does the master caution light illuminate for a single/single fault?

Answer 1

Master Caution Recall

Question 2

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

Answer 2

12 minutes

Question 3

When do the over wing exit door locks engage?

Answer 3

A minimum of 3 of 4 entry/service doors are closed, and either engine is running, and air/ground logic indicates that the aircraft is in the air or both thrust levers are advanced

Question 4

What is the function of the electric air compressor?

Answer 4

Pressurized air to the potable water tank when pneumatic system is off or insufficient
- < 30 psi and operates up to 40 psi.
CAB/UTIL switch ON
-Water service panel door is closed/not removed.
-Powered by the Main bus # 1
-

Question 5

With both LED landing lights ON and taxi light on/auto the taxi light function is____________. By the landing light function?

Answer 5

Taxi light doesn’t come on just the landing lights

Question 6

Pressurization panel: Auto Fail amber light illuminates if any of the following conditions occur?
Name one:

Answer 6

-Loss of DC power
-CPC - Controller Fault
-Outflow valve control fault
-Excessive Differential Pressure (> 8.75 PSI)
-Excessive rate of cabin pressure change (+-2000 FPM)
-High Cabin Altitude (>15,800 FT)

Question 7

The wing body overheat amber light when illuminated, indicates what?

Answer 7

An overheat has been detected.
Bleed air leak!
Eng strut
Inboard wing leading edge
Air conditioning bays
Keel berm
Apu bleed duct

Question 8

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

Answer 8

Dual Bleed

Question 9

What does a Bleed Trip Off Light indicate?

Answer 9

NG only-
-High bleed air temp 254C
-High pressure 220 psi
-Reset with the trip/reset button if able. Follow QRH?
*Will get AIR COND annunciator and master caution

Question 10

The MAX pneumatic systems use_________ and___________ stage bleed air

Answer 10

4th and 10th

Question 11

What are your indications when you receive a SELCAL? __________and _________

Answer 11

SELCAL white light and two tone chime

Question 12

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

Answer 12

VHF 3

Question 13

The Radio Tuning Panel displays ________ when the selected radio is not available?

Answer 13

FAIL FAIL

Question 14

What does an illuminated offside tuning white light indicate?

Answer 14

The radio normally associated with this panel is being tuned by another radio tuning panel, or the panel is being used to tune another radio. A radio of tuning offside.

Question 15

On the MAX where is the SELCAL light?

Answer 15

Just below the MIC selector, on the ACP

Question 16

With the ignition select system at IGN R, what is the power source ?

Answer 16

AC Standby bus

Question 17

What will remove an amber ENG FAIL indication ?

Answer 17

The engine recovers,
Start lever is moved to CUTOFF
The fire switch is pulled

Question 18

What does the THRUST crew alert on the Eng display indicate?

Answer 18

The associated eng thrust is more or less than commanded thrust.
N1 command selector turns amber.

Question 19

The thrust mode display green, indicates R-TO. What mode is active?

Answer 19

Reduced Takeoff

Question 20

In the MAX, How long should you wait after the APU GEN OFF BUS (blue) light extinguishes before positioning the battery switch to off?

Answer 20

5 min
2 for the NG

Question 21

During anFAULT/INOP test, the failure of the FAULT light to illuminate indicates?

Answer 21

The fault monitoring system test failed.
Tests eng and apu fire tests
Both master cautions
OVHT/DET system annunciator
FAULT light illuminates
Apu DET light illuminates

Write it up and Call Mx

Question 22

Rotating and Eng fire switch in one direction

Answer 22

Electrically fired a squib, discharging the extinguisher in the the related engine

Question 23

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

Answer 23

195 min 180 + 15 mins for extra
1 HRD = high rate discharge
15 min timer until low rate discharge starts.
1 low rate discharge

Question 24

The max has how many wheel well fire detector loops?

Answer 24

2

Question 25

The fuel LOW (Amber) alert is displayed when the respective main tank fuel quantity is less than __________ for greater than __________?

Answer 25

2000 lbs 30 seconds It’s below the fuel indication for each main tank. Stays on until 2500 lbs in that tank.

Question 26

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

Answer 26

The crossfeed valve open, no center tank fuel feed, Main tank pumps operating within the normal pump output pressure tolerances.

Question 27

Opening the crossfeed valve inflight, _________\

Answer 27

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

Question 28

IMBAL (Amber) alert means the main tanks differ by more than ______pounds?

Answer 28

1000 for greater than 60 seconds Displays below the lower tank indication. Stays on until within 200 or less Inhibited on the ground or when LOW fuel alerts

Question 29

The fuel flow (Amber) alert is displayed when ________ on the max?

Answer 29

When the difference between actual engine fuel flow rate and the FMS. threshold value for 5 continuous minutes Eng Fuel flow is abnormally HIGH QRH will send you to the Fuel Leak - Engine Checklist

Question 30

The COWL anti ice (Amber) light illuminates due to _______

Answer 30

Excessive pressure in the duct

Question 31

Which leading edge devices are on the wing anti-ice system?

Answer 31

Three inboard leading edge slats

Question 32

The TAI (Amber) indication to the left of an N1 display on the upper display unit indicates:

Answer 32

The cowl anti ice valve has failed to move to the position selected by the Eng anti ice switch

Question 33

Positioning the WING ANTI ICE switch to ON in flight?

Answer 33

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

Question 34

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

Answer 34

Automatically by the EEC

Question 35

With a TCAS pitch command on the PFD displayed, keep the aircraft symbol _________the area indicated by the red lines.

Answer 35

Outside

Question 36

If not previously commanded on, predictive windshear for takeoff automatically turns on by___________

Answer 36

Advancing thrust levers beyond 53 degrees

Question 37

The GPWS provides BANK ANGLE alert when the roll angle exceeds ___, ____and _____

Answer 37

35 degrees, 40 degrees 45 degrees

Question 38

Which button on the radar panel to display turbulence ?

Answer 38

WX + T

Question 39

The MAINT (Amber) light, when illuminated, indicates______

Answer 39

That when a system fault exists that must be reviewed by maintenance Pack controller fail Thrust reverser issue PSEU on NG

Question 40

If the OVHT DET switch is positioned to A or B, the system operates as __________?

Answer 40

A single loop system.