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A320 > General > Flashcards

General Flashcards

1
Q

Lighting system includes (4) FECC

A

Flight Deck
Exterior
Cabin Normal and Emergency
Cabin signs

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2
Q

What light is powered directly from aircraft batteries and can be used when there is no AC power to the airplane and in the emergency electrical configuration?

A

FO dome light

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3
Q

Which light only works on the CA side in the emergency electrical or battery-only configuration?

A

Flood lights

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4
Q

STBY COMPASS light is available in what 2 situations?

A

Emergency electrical configuration

Operation on battery only

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5
Q

T/F - The nose gear lights automatically extinguish when the nose gear retracts?

A

True

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6
Q

Above what airspeed will the extension of landing lights possibly cause airframe buffet?

A

280 kts

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7
Q

In the event of excessive cabin altitude, what lights automatically illuminate?

A

Cabin Lights and seatbelt lights

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8
Q

What powers the escape path lights and signs in the event of electrical failure?

A

Self contained battery packs

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9
Q

Emergency Lighting consist of?

(LOEEE)

A

Lav aux lights
Overhead emergency
Escape Path
Exit
Escape slide

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10
Q

Loss of which bus results in the overhead emergency lights illuminating?

A

AC Bus 1

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11
Q

Under normal conditions: which bus charges the emergency dedicated battery packs?

A

DC ESSential Shed

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12
Q

When are the dedicated battery packs NOT charged? (3)

acronym: EEN

A

Emergency lights are selected on

Emergency lights are illuminated due to aircraft electrical power failure

The NO PORTABLE ELEC DEVICE switch is selected to AUTO, and the landing gear is extended.

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13
Q

What flight deck lights are available in the emergency electrical configuration?

A

Standby compass
CA instrument flood
FO dome

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14
Q

Icing conditions exist when OAT (ground or TO) or TAT (inflight) is XXX and visible moisture exists

A

10C or below

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15
Q

Engine Anti-ice must be on for all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temperature is below XXX

A

-40C SAT

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16
Q

T/F - Cockpit door will automatically lock during decompression or if electrical power is lost

A

False

17
Q

Which hydraulic system supplies hydraulic pressure to open and close the cargo doors

A

Yellow system

18
Q

When should a TOGA thrust takeoff be performed?

COWTD

A

Contaminated runway
Obstacle on the departure path
Wind shear
Tailwind
Dispatch or crew deems necessary

19
Q

FMGS navigation accuracy check is required when? (3) NIL

A

NAV ACCUR DOWNGRAD - scratchpad
IRS ONLY NAV - scratch pad
LOW - PROG page display

20
Q

When can FMC be considered to be reliable?

A

FMC distance is within 3NM of the radio distance.

21
Q

What must happen if FMC distance is greater than 3NM?

A

Raw data must be referenced.

22
Q

Pressurization Controller gets information from what? (4) FLAT

A

FMGS
Landing gear (wow)
ADIRS (Air data inertial ref sys)
TLA

23
Q

When Pressurization is in manual mode, what is no longer displayed?

A

LFE

24
Q

Manually setting the LFE would be performed due to: (2)

A

Both FMGCs failing

The intended airport is not in the FMGC database

25
Q

APU bleed air is prohibited above

A

20000ft

26
Q

In normal operations, which BMC (1 or 2) is used to control and monitor the APU bleed system and the function of the automatic operation of the crossbleed valve during normal operations.

A

BMC 1

27
Q

APU

Starter motor cycle Cooldown

A

60 seconds
60 seconds
60 minutes

28
Q

Autopilot

All OTHER phases of flight auto pilot disengagement height.

A

500’ RA (900’ A321)

29
Q

Autopilot

non-ILS approaches disengagement height.

A

DA, MDA, DDA

30
Q

Autopilot

CAT1 disengagement height.

A

160’ RA

31
Q

Autopilot

Non-auto-land ILS approach with CAT2 or CAT3 SINGLE or CAT3 DUAL FMA annunciations, min disengagement height.

A

80’ RA

32
Q

Autopilot

CAT2/3 auto-landings, min disengagement height.

A

NONE- Auto pilot is always required throughout landing and rollout.

A320 (2 decks)

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