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AS Airbus Limitations > . > Flashcards

. Flashcards

1
Q

What is the meaning of USE MAN PITCH TRIM when displayed on the PFD?

A

You are in Direct Law

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2
Q

What speed does Vmax represent?

A

It is the lowest of Vmo/Mmo, Vle or Vfe

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3
Q

If power fails to the ECAM Control Panel, which buttons are still functional?

A

EMR CANC, ALL, CLR, STS, RCL

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4
Q

What does PASSENGER SYS ON light mean?

A

The signal to release the oxygen door masks has been sent

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5
Q

What does the FAULT light on the ENG ANTI ICE pushbutton indicate?

A

Switch/Anti-ice valve position disagreement

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6
Q

When do WING ANTI ICE valves automatically close?

A

Bleed leak detected

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7
Q

How many hydraulic pumps are on the GREEN system?

A

1 Engine, 1 PTU

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8
Q

What does an amber FAULT light on the PTU pushbutton indicate?

A

Reservoir pressure is low

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9
Q

What is the purpose of the hand pump on the YELLOW hydraulic system?

A

To provide YELLOW hydraulic pressure for cargo door operations

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10
Q

With the RCDR in auto, when does the CVR record?

A

On the ground for 5 minutes after electrical power is supplied to the aircraft

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11
Q

What are the pitch and bank angle limits indicated by the Green = sign on the PFD

A

Pitch = 30° up, 15° down, Bank = +/-67°

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12
Q

Which Hydraulic systems provide pressure to Alternate brakes?

A

YELLOW system

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13
Q

If you push the EMER CANC pushbutton on the ECAM SWITCHING panel for a Level 3 warning, how long is that warning inhibited?

A

For that one occurrence

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14
Q

When do the passenger oxygen masks automatically deploy?

A

When the cabin altitude exceeds 14,000 feet

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15
Q

What does the amber FAULT light in the WING ANTI ICE pushbutton indicate?

A

Low duct pressure is detected

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16
Q

What condition will cause the PTU to operate if the pushbutton is in AUTO?

A

A difference of 500 PSI between GREEN and YELLOW hydraulic system

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17
Q

What does an amber FAULT light in the hydraulic ENG PUMP pushbutton indicate?

A

Overtemp in the reservoir

18
Q

To record the flight attendants during their pax safety briefings, the ACP 3 __VOL knob needs to be out and in the 1 o’clock position

A

PA

19
Q

The aircraft must be above _ for MAX AUTO break to achieve that.

A

72 kts

20
Q

How long does the PAX OXYGEN last?

A

Approximately 13 min

21
Q

What does an amber FAULT light in the APU BLEED push button indicate?

A

An APU bleed leak

22
Q

What happens if you turn the WING ANTI ICE switch to ON when on the ground?

A

The wing anti-ice valves will open for a 30 second test

23
Q

In what position do the WING and ENGINE Anti-Ice valves fail in electric power is lost?

A

Wing valves close, engine valves open

24
Q

After engine start with the APU BLEED pushbutton ON, which source of bleed pressure is supplying the packs?

A

APU

25
Q

How many hydraulic pumps are in the YELLOW system?

A

1 Engine, 1 Electric, 1 PTU, 1 Hand Pump

26
Q

If the ECAM actions lead you to turn OFF the PTU for a Reservoir Overheat, will the FAULT light go away?

A

No, not until the overheat subsides

27
Q

How are the flight control surfaces controlled and actuated?

A

All surfaces are controlled electrically, and actuated hydraulically

28
Q

What powers the emergency generator?

A

BLUE hydraulic power from the RAT

29
Q

What is the purpose of the DFDR EVENT pushbutton?

A

Briefly pressing this button sets an event mark on the Flight Data Recorder

30
Q

What is the meaning of MANUAL PITCH TRIM ONLY on the PFD?

A

You are in Mechanical Backup

31
Q

What part of the wing is heated?

A

Outboard 3 slats

32
Q

What flow rate is provided when the APU BLEED pushbutton is ON?

A

High Flow

33
Q

What occurs when you press the RAT MAN ON pushbutton on the HYD panel?

A

The RAT extends providing pressure to the BLUE hydraulic system

34
Q

What is normal hydraulic system pressure?

A

3000 +/- 200 PSI

35
Q

Which item does NOT use the GREEN hydraulic system?

A

RAT, EMER GEN

36
Q

Which systems are NOT on the YELLOW system?

A

Normal brakes, slats

37
Q

What is the function of the hydraulic priority valves?

A

Hydraulic power to the flaps, slats, landing gear, and emergency generator are cut off if the pressure drops below a predetermined value

38
Q

Which of the following is NOT provided by the FACs?

A

Spoiler roll control

39
Q

How many Bleed Monitoring Computers (BMC) are installed?

A

2

40
Q

In Normal Law with flaps and slats extended, what are the aircraft load limitations?

A

+2.0G/0.0G

41
Q

Which RMP and MCDU is available in the Emergency Electrical Configuration?

A

RMP & MCDU 1

AS Airbus Limitations (3 decks)

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