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A320 (SB) > A320 Limitations > Flashcards

A320 Limitations Flashcards

1
Q

Max altitude

A

39,800’

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2
Q

Max taxi weight

A

77,400kg

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3
Q

Max take off weight

A

77,000kg

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4
Q

Max zero fuel weight

A

61,000 kg

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5
Q

Max landing weight

A

64,500 kg

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6
Q

Turning circle

A

22.8 m

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7
Q

Maximun runway altitude

A

9,200’

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8
Q

Normal runway width
Nominal
Minimal

A

45m

30m

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9
Q

Max demonstrated Xwind

A

38 kts

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10
Q

Max tailwind for takeoff

A

10 kts

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11
Q

Max tailwind for landing

A

10 kts

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12
Q

Max wind for Pax door operation

A

65 kts

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13
Q

Max wind for cargo door operation
if into wind or leeward
must be closed by

A

40 kts
50 kts
65 kts

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14
Q

Max Xwind for Damp GOOD
GOOD TO MEDIUM
MEDIUM
MEDIUM TO POOR
POOR

A 
38 KTS
29 KTS
25 KTS
20 KTS
15 KTS
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15
Q

Max speed cockpit window open

A

200 kts

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16
Q 
Max flap extension speeds
                             0
                             1
                             1 + F
                             2
                             3
                            Full
                            Max altitude
A 
Vmo Mmo
230 kts
215 kts
200 kts
185 kts
177 kts
20,000'
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17
Q

Max operating speed Vmo

Mmo

A

350 kts

M 0.82

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18
Q

Max speed with the landing gear extended (VLE)

A

280 kt /M 0.67

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19
Q

Max speed at which the landing gear may be extended (VLO extension)

A

250 kt /M 0.60

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20
Q

Max speed at which the landing gear may be retracted (VLO retraction)

A

220 kt /M 0.54

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21
Q

Max tyre speed on ground

A

195 kts

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22
Q

Max Taxi speed

A

above 76t max 20 kts during turn

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23
Q

Max wiper speed

A

230 kts

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24
Q

Avionics ventilation on ground

49 °C < OAT ≤ 55 °C

A

2 hours

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25
Q

Cabin pressure
Max positive diff
Max negative diff
Safety relief valve setting

A
  1. 0 psi
    - 1.0 psi
  2. 6 psi
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26
Q

Auto pilot use height

Take-off

A

100 ft AGL and at least 5 s after liftoff

27
Q

Auto pilot use height

In approach with F-G/S  mode

A

200 ft AGL

28
Q

Auto pilot use height

In approach with FINAL APP, V/S or FPA mode

A

250 ft AGL

29
Q

Auto pilot use height

In circling approach

A

500 ft AGL for aircraft category C

30
Q

Auto pilot use height

ILS/MLS approach when CAT1 is on the FMA

A

160 ft AGL

31
Q

Auto pilot use height

GLS  approach when AUTOLAND is not displayed on the FMA

A

160 ft AGL

32
Q

Auto pilot use height

ILS/MLS  approach when CAT2 or CAT3 (single or dual) is displayed on the FMA

A

0 ft AGL if autoland

33
Q 
Auto pilot use height
         PAR approach (Precision Approach Radar)
A

250 ft AGL

34
Q

Auto pilot use height

After a manual go-around

A

100 ft AGL

35
Q

Auto pilot use height

In all other phases

A

500 ft AGL

36
Q

Max wind for ILS/MLS CAT II OR CAT III and for GLS CAT I

A

Headwind : 30 kt
Crosswind : 20 kt
Tailwind : 10 kt

37
Q

APU
number of start attempts
rest period after

A

3 start attempts

60 min wait period

38
Q

APU

Max altitude to assist engine start

A

20 000 ft

39
Q

APU

Max altitude for air conditioning and pressurization (single pack operation)

A

22,500’

40
Q

APU

Max altitude for air conditioning and pressurization (dual pack operation)

A

15 000 ft

41
Q

APU

Use of APU bleed air for wing anti-ice

A

not permitted

42
Q

ENGINES Thrust setting Take-off and go-around
all engines time ____ EGT____
one engine inop time ____ EGT____

A

5 min 635 °C

10 min 635 °C

43
Q

ENGINES Thrust setting

MCT time ____ EGT____

A

no time limit 610 °C

44
Q

ENGINES Starting EGT limit

inflight/onground

A

635 °C

45
Q

ENGINES

Minimum oil pressure

A

60 PSI

46
Q

ENGINES starter limits
Pause between starts (man & auto)
Pause after __ attempts or __ min cycle time

A

15 seconds

3 attempts or 5 min cycle, pause 30 minutes

47
Q

ENGINES reduced thrust take-off

highest TMAXFLEX = ISA + ______

A

ISA + 55

Lower than the actual OAT

48
Q

ENGINES

Xwind limit for start

A

35 kt

49
Q 
FUEL
Max imbalance at TAKE-OFF
Inner tanks, (outer balanced)
fuel quantity       FULL
fuel quantity      3000kg
fuel quantity      1450 kg
A

500 kg
1 050 kg
1 450 kg

50
Q

FUEL
Max imbalance at TAKE-OFF
Outer tanks, (inner balanced)
Max assymetry

A

370 kg

51
Q 
FUEL
Max imbalance IN FLIGHT AND AT LANDING
inner tanks, (outer balanced)
fuel quantity       FULL
fuel quantity      4300kg
fuel quantity      2250 kg
A

1500 kg
1600 kg
2250 kg

52
Q

FUEL
Max imbalance at take-off
outer tanks

A

690 kg

53
Q

FUEL

Minimum fuel quantity for takeoff

A

1500 kg

or No ECAM alert for fuel low level

54
Q

ICING

Definition of icing conditions

A

OAT (on ground or after takeoff) or the TAT (in flight) is at or below 10 °C and visible moisture, vis less than 1600m surface snow, standing water or slush may be
ingested by the engines, or freeze on engines, nacelles or engine sensor probes.

55
Q

Rain repellant should only be used _____

A

Moderate to heavy

56
Q

BRAKE TEMPERATURES

Maximum brake temperature for takeoff (brake fans off)

A

300 °C

57
Q

Maximum NWS angle

A

±75°

58
Q

Minimum oil temp for take-off

A

50 °C

59
Q

Minimum oil pressure

A

60 Psi

60
Q

Minimum engine oil

A

11 qt plus 0.3 qt/hr

61
Q

Cabin alt warning

A

9550’ +/- 350’

62
Q

Manual start maximum cycle time

A

2 minutes

63
Q

Maximum CRANK cycle time

A

5 minutes

64
Q

In NAV mode, the IR will not provide valid magnetic heading and magnetic track angle

A

‐ North of 73 ° North,

and ‐ South of 60 ° South.

A320 (SB) (3 decks)

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