A330 Systems General Flashcards

(37 cards)

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

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
SYS ON light
Passenger O2 drop command sent
26
CREW SUPPLY
controls valve between masks and cylinder
27
Wipers max speed
230kt
28
No Smoking
Hardwired on, Switch in on position turns on exit signs and left on will deplete internal batteries
29
2 exterior locations to shut down APU
Refueling Panel External Power Panel
30
Controls all APU logic
ECB (Electronic Control Box)
31
APU gets fuel from…
Left Inner Collector Tank Trim Pipe Trim Tank
32
EMER EXIT ARMED, lights come on if…
Normal electrical power fail AC BUS 1 fails Cabin Altitude over 9550’
33
Ditching Pb switch…
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
Cabin Pressurization modes
AUTO (airport database) SEMI AUTO (ldg elevation) MANUAL (set V/S manually)
35
PROBE/WINDOW heat
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
ENG Anti Ice
Used for Anti-Ice Fails open. No limitations
37
Wing Anti-Ice
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.