A330 Systems General Flashcards

1
Q

2 types of SYSTEM RESETS

A
  1. Instructed by ECAM or QRH procedure
  2. System Reset Table in QRH (consult maintenance)
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2
Q

5 Circuit Breakers in cockpit

A

3 in the cockpit door frame
1 under each pilot seat on the pedestal

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3
Q

ADIRS ATT position provides

A

Attitude and Heading information only (must be updated in the MCDU every 10 minutes)

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4
Q

Flashing IR Fault

A

ATT and HDG info can be recovered in ATT mode

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5
Q

Solid IR fault

A

IR has failed

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6
Q

2 Types of ADIRU alignment

A

Quick (under 5 sec): 30 sec duration, only clears ground speed.

Full (5 or more sec): clears ground speed and drift, captures ppos. 7-10 min duration.

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7
Q

IRS ONLY in Class 2 NAV

A

6.2 hours from alignment

5.7 hours from last FM position update

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8
Q

APU fire in the ground

A

APU Shutdown and Fire Bottle activated automatically

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9
Q

APU how many fire bottles?

A

1

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10
Q

How many APU FIRE loops?

A

2

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11
Q

What sets off APU FIRE warning?

A

Both loops detect fire

One loop broke, 1 detects fire

2 loops break within 5 sec

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12
Q

APU FIRE PUSHBUTTON

A

-Shuts down APU
-CRC silenced
-Arm squibs
-LP fuel valves, APU fuel pumps shut off
-APU gen deactivates
-APU bleed and x-bleed valve close

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13
Q

APU Fire Test?

A

APU FIRE pb light
Agent squib and disch lights
2 master Warning lights
CRC
E/WD APU FIRE warn msg

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14
Q

Turn Damp

A

Controlled by PRIMs
In normal flight envelope
Normal Law or AP engaged
Airspeed greater than 200

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15
Q

PRIM

A

3 PRIMs
Used for NORM ALT and DIRECT laws

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16
Q

SECs

A

2 SECs
Used for direct law if no PRIMs operational

17
Q

Fuel Jettison

A

2,200lb/min (plus burn)

Transfers Trim to Center, Outer to Inner

Jettisons from inner and center simultaneously

18
Q

Automatic activation of
EMER ELEC CONFIG

A

Loss of AC BUS 1 and AC BUS 2 (big green) AC ESS BUS 1,2 + AC ESS SHED BUS 1,2

Loss of both engines (little green) AC ESS BUS 1,2

19
Q

RAT min speed

A

140kt

20
Q

Land Recovery Pushbutton

A

Powers Land Recovery Buses.
LGCIU 1 **
SFCC1 ** (slat chnl only)
BSCU Ch1
LH windshield heat
LH landing light
(
little green)

21
Q

GPWS System off

A

Inhibits basic GPWS modes 1-5

22
Q

RCDR starts automatically…

A

On ground for 5 min after power up

After 1st engine start

In the air

23
Q

CKPT OXY half amber box

A

Check limitation chart

24
Q

MASK MAN ON

A

Drops passenger oxygen masks

25
Q

SYS ON light

A

Passenger O2 drop command sent

26
Q

CREW SUPPLY

A

controls valve between masks and cylinder

27
Q

Wipers max speed

A

230kt

28
Q

No Smoking

A

Hardwired on,
Switch in on position turns on exit signs and left on will deplete internal batteries

29
Q

2 exterior locations to shut down APU

A

Refueling Panel

External Power Panel

30
Q

Controls all APU logic

A

ECB (Electronic Control Box)

31
Q

APU gets fuel from…

A

Left Inner Collector Tank
Trim Pipe
Trim Tank

32
Q

EMER EXIT ARMED, lights come on if…

A

Normal electrical power fail

AC BUS 1 fails

Cabin Altitude over 9550’

33
Q

Ditching Pb switch…

A

O utflow valves close
C argo isolation valves close
R am air inlet closes
A vionics Vent Ovbd closes
P ack flow cont valves close

Used for ditching, deicing

34
Q

Cabin Pressurization modes

A

AUTO (airport database)

SEMI AUTO (ldg elevation)

MANUAL (set V/S manually)

35
Q

PROBE/WINDOW heat

A

Normally in AUTO
Automatic in flight and after 1st engine start.
ON activates probe/window heat on low setting in the ground. (TAT probes only energized in flight)

36
Q

ENG Anti Ice

A

Used for Anti-Ice
Fails open. No limitations

37
Q

Wing Anti-Ice

A

Deice (ECAM or visible ice)
Fails closed
Only 4 outer slats heated

If activated on the ground 30 sec test occurs then turns off until off ground.