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QT A320 > ATA29 - Hydraulic > Flashcards

ATA29 - Hydraulic Flashcards

1
Q
  1. The PRIORITY VALVES operate in case of :
    High HYDRAULIC PRESSURE in the GREEN system
    Low HYDRAULIC PRESSURE in the three hydraulic systems
    High HYDRAULIC PRESSURE in the GREEN and YELLOW systems
A

Low HYDRAULIC PRESSURE in the three hydraulic systems

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2
Q
  1. The YELLOW SYSTEM may be powered by :
    ENG 1 HYDRAULIC PUMP
    ENG 2 HYDRAULIC PUMP, the YELLOW ELEC PUMP or the PTU
    ENG 2 HYDRAULIC PUMP, the YELLOW ELEC PUMP, the RAT
A

ENG 2 HYDRAULIC PUMP, the YELLOW ELEC PUMP or the PTU

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3
Q
  1. In case of BLUE ELEC PUMP failure, when the RAT MAN ON P/B is pressed :
    The BLUE HYDRAULIC SYSTEM is pressurized by the RAT
    The EMERGENCY GENERATOR is supplying ELECTRICAL POWER
    The BLUE HYDRAULIC SYSTEM is pressurized and the EMERGENCY GEN is
    running
A

The BLUE HYDRAULIC SYSTEM is pressurized by the RAT

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4
Q
  1. Can you operate a cargo door when no electrical power is available ?
    Yes
    No
A

Yes

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5
Q
  1. In flight the ENG 1 PUMP FAULT light illuminates amber in case of :
    A RESERVOIR LOW LEVEL or LOW AIR PRESSURE
    A RESERVOIR OVERHEAT
    Both answers are corrects
A

Both answers are corrects

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6
Q 
202. In flight, if BLUE ELEC PUMP fails, BLUE SYSTEM :
Is lost
Can be recovered by RAT
Can be recovered by PTU
Can be recovered by RAT and by PTU
A

Can be recovered by RAT

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7
Q
  1. The GREEN SYSTEM operates :
    THE REVERSER 1
    THE REVERSER 2
    Both answers are correct
A

THE REVERSER 1

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8
Q
  1. When extended in flight, the RAT pressurizes :
    The GREEN SYSTEM
    The YELLOW SYSTEM and the GREEN SYSTEM via the PTU
    The BLUE SYSTEM
A

The BLUE SYSTEM

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9
Q
  1. The YELLOW SYSTEM comprises :
    One ENGINE DRIVEN PUMP, one ELEC PUMP, one HAND PUMP
    One ENGINE DRIVEN PUMP, two ELEC PUMPS
    One ENGINE DRIVEN PUMP, one HAND PUMP and the RAT
A

One ENGINE DRIVEN PUMP, one ELEC PUMP, one HAND PUMP

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10
Q
  1. The YELLOW SYSTEM operates :
    The REVERSER 1
    The REVERSER 2
    Both answers are correct
A

The REVERSER 2

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11
Q
  1. During first ENGINE START the PTU is :
    Automatically running
    Tested
    Inhibited
A

Inhibited

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12
Q
  1. The BLUE SYSTEM includes operation of :
    The FLAPS
    The SLATS
    The FLAPS and SLATS
A

The SLATS

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13
Q
  1. HYDRAULIC GREEN SYSTEM only remaining, the HORIZONTAL STABILIZER is :
    Available
    Lost
A

Available

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14
Q
  1. On ground, with both engines stopped, how can GREEN SYSTEM be pressurized ?
    By the GREEN ENGINE PUMP
    By the YELLOW ENGINE PUMP and the PTU
    By the YELLOW ELEC PUMP and the PTU
A

By the YELLOW ELEC PUMP and the PTU

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15
Q
  1. PTU at AUTO, the PTU AUTOMATICALLY runs :
    If the BLUE HYDRAULIC SYSTEM is lost
    When differential pressure between GREEN AND YELLOW SYSTEM is more than
    500 PSI
    As soon as a differential pressure between GREEN and YELLOW SYSTEM is
    detected
A

When differential pressure between GREEN AND YELLOW SYSTEM is more than
500 PSI

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16
Q
  1. HYDRAULIC GREEN SYSTEM only remaining, the AUTO PILOT FUNCTION is :
    Available with AP1
    Lost
    Available with AP2
A

Lost

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17
Q
  1. The YELLOW SYSTEM includes operation of :
    The left and right elevator
    The left elevator only
    The right elevator only
A

The right elevator only

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18
Q
  1. On ground the BLUE SYSTEM is pressurized when :
    The APU is running
    One engine is running
    EXT POWER is available
A

One engine is running

19
Q
  1. The FIRE SHUT-OFF VALVES shut off :
    The BLUE and YELLOW SYSTEMS
    The YELLOW and GREEN SYSTEMS
    The GREEN and BLUE SYSTEMS
A

The YELLOW and GREEN SYSTEMS

20
Q 
216. Engine 2 energizes :
The BLUE SYSTEM PUMP
The GREEN SYSTEM PUMP
The YELLOW SYSTEM PUMP and the GREEN SYSTEM via the PTU if the
GREEN SYSTEM PUMP is failed
A

The YELLOW SYSTEM PUMP and the GREEN SYSTEM via the PTU if the
GREEN SYSTEM PUMP is failed

21
Q
  1. If on ground with ENG 1 stopped ; does the ENG 1 PUMP FAULT light illuminate
    amber due to GREEN PUMP LOW PRESSURE ?
    Yes
    No
22
Q
  1. The HYD FIRE SHUT-OFF VALVE closes when :
    The ENG MASTER SWITCH is set to “OFF” position
    The FIRE P/B is released out
    Automatically if fire is detected
A

The FIRE P/B is released out

23
Q 
219. In case of SINGLE SYS LO PR :
The MASTER WARN LIGHT ILLUMINATES
The MASTER CAUTION LIGHT ILLUMINATES and THE SINGLE CHIME
SOUNDS
There is NO WARNING
A

The MASTER CAUTION LIGHT ILLUMINATES and THE SINGLE CHIME

SOUNDS

24
Q
  1. The RAT can be extended :
    Automatically in case of loss of power to AC BUS 1 and 2
    Manually from the overhead panel
    The two answers are correct
A

The two answers are correct

25
Q
  1. The YELLOW SYSTEM includes operation of :
    The FLAPS
    The FLAPS and SLATS
    The SLATS
26
Q
  1. On newer aircraft, with Yellow System lost :
    The NWS is lost
    The NWS is operative
    The NWS operates on alternate
A

The NWS is lost

27
Q
  1. The ENG 2 FIRE VALVE is between the YELLOW RESERVOIR and :
    The ENG 2 HYDRAULIC PUMP
    The YELLOW ELEC PUMP
    The YELLOW HAND PUMP
A

The ENG 2 HYDRAULIC PUMP

28
Q
  1. In case of reservoir overheat, the FAULT lights of the faulty system stay ON :
    For 30 seconds
    Continuously
    As long as the overheat is detected
A

As long as the overheat is detected

29
Q
  1. On ground and before engine start, with BLUE PUMP AUTO and ELEC POWER
    available, the BLUE PUMP is :
    Automatically energized
    Energized if the BLUE PUMP OVRD P/B is pressed
A

Energized if the BLUE PUMP OVRD P/B is pressed

30
Q
  1. If BLUE SYSTEM is lost, the FLAPS are :
    Normal
    Slow
    Lost
31
Q
  1. In flight the RAT is extended :
    Manually only
    Manually or automatically
    Automatically only
A

Manually or automatically

32
Q
  1. The GREEN SYSTEM operates :
    The LEFT AILERON
    The RIGHT AILERON
    Both answers are correct
A

Both answers are correct

33
Q 
229. Is the hydraulic fluid can be transfered from GREEN to YELLOW or YELLOW to
GREEN SYSTEM ? :
No
Yes, by the PTU
Yes in case of leakage
34
Q
  1. The hydraulic reservoirs are pressurized :
    From the PNEUMATIC SYSTEM
    From the PACKS 1 and 2
    From the LH ENGINE or the PNEUMATIC SYSTEM
A

From the LH ENGINE or the PNEUMATIC SYSTEM

35
Q
  1. The YELLOW SYSTEM operates :
    SPOILERS 3
    SPOILERS 2 and 4
    SPOILERS 1 and 5
A

SPOILERS 2 and 4

36
Q
  1. The GREEN SYSTEM operates :
    SPOILERS 3
    SPOILERS 2 and 4
    SPOILERS 1 and 5
A

SPOILERS 1 and 5

37
Q
  1. The BLUE SYSTEM operates :
    The LEFT AILERON
    The RIGHT AILERON
    Both answers are correct
A

Both answers are correct

38
Q
  1. On ground, BLUE ELEC PUMP P/B AT AUTO, the BLUE SYSTEM is energized if :
    One BATTERY is on AUTO
    GROUND ELECTRICAL POWER is ON
    One engine is running or BLUE PUMP OVRD P/B has been pressed
A

One engine is running or BLUE PUMP OVRD P/B has been pressed

39
Q
  1. The BLUE SYSTEM operates :
    SPOILERS 2 and 4
    SPOILERS 3
    SPOILERS 1 and 5
A

SPOILERS 3

40
Q
  1. The GREEN SYSTEM operates :
    The RIGHT ELEVATOR
    The LEFT ELEVATOR
    Both answers are correct
A

The LEFT ELEVATOR

41
Q
  1. YELLOW ELEC PUMP P/B SWITCH OFF and CARGO DOOR MANUAL SELECTOR
    VALVE set at OPEN or CLOSE POSITION, the PTU and the FLIGHT CONTROLS
    are :
    Operative
    Inhibited
42
Q
  1. NORMAL HYDRAULIC POWER is provided by :
    ENGINE DRIVEN PUMPS for all SYSTEMS
    ENGINE DRIVEN PUMPS for GREEN and YELLOW, ELEC PUMP for BLUE.
    ENGINE DRIVEN PUMPS for GREEN and BLUE, ELECTRIC PUMP for YELLOW
A

ENGINE DRIVEN PUMPS for GREEN and YELLOW, ELEC PUMP for BLUE.

43
Q
  1. The RAT can be restowed :
    In FLIGHT
    On GROUND only
    On GROUND and in FLIGHT
A

On GROUND only

44
Q
  1. The POWER TRANSFERT UNIT is :
    Reversible between GREEN and YELLOW
    One way GREEN to YELLOW
    Reversible between BLUE and YELLOW
A

Reversible between GREEN and YELLOW

QT A320 (21 decks)

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