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A320 Limitations > Limitations > Flashcards

Limitations Flashcards

1
Q

Flight maneuvering and Load Acceleration limits:

Other configurations

A

0g to 2g

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2
Q

Operational parameters:

Runway slope

A

+/- 2%

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3
Q

Operational parameters:

Runway altitude

A

9200 ft

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4
Q

Operational parameters:

Nominal Runway width

A

45m

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5
Q

Operational parameters:

Minimal Runway width

A

30m

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6
Q

Max Crosswind:

Takeoff

A

35 kt

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7
Q

Max Crosswind:

Landing

A

38 kt

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8
Q

Maximum certified tailwind:

Take off and landing

A

15 kt

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9
Q

Maximum wind for passenger door operation

A

65 kt

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10
Q

Maximum wind FWD and AFT cargo door

A

40 kt (50 kt nose into wind)

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11
Q

Speeds

Maximum flaps/slats speeds

1

A

230 kt

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12
Q

Speeds

Maximum flaps/slats speeds

1 + F

A

215 kt

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13
Q

Speeds

Maximum flaps/slats speeds

2

A

200 kt

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14
Q

Speeds

Maximum flaps/slats speeds

3

A

185 kt

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15
Q

Speeds

Maximum flaps/slats speeds

FULL

A

177 kt

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16
Q

Speeds

Cockpit window open M

A

200 kt

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17
Q

Speeds

VMO

A

350 kt

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18
Q

Speeds

MMO

A

0.82 M

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19
Q

Speeds

Maximum speed with L/G extended

A

280 kt/0.67 M

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20
Q

Speeds

Maximum speed for L/G extension

A

250 kt/0.60 M

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21
Q

Speeds

Maximum speed for L/G retraction

A

220 kt/0.54 M

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22
Q

Speeds

Maximum tire speed

A

195 kt (Ground speed)

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23
Q

Speeds

Wipers maximum speed

A

230 kt

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24
Q

Speeds

Minimum control speed for landing (VMCL)

A

116 kt
(See FCOM p. 2227 for VMCA & VMCG)

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25
Q

Cabin Pressure

Maximum positive differential pressure

A

9.0 PSI

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26
Q

Weight limitations

Maximum taxi weight

A

77.400 kg

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27
Q

Weight limitations

Maximum takeoff weight (brakes release)

A

77.000 kg

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28
Q

Weight limitations

Maximum landing weight

A

67.400 kg

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29
Q

Weight limitations

Maximum zero fuel weight

A

64.300 kg

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30
Q

Weight limitations

Minimum weight

A

40.600 kg

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31
Q

Cabin Pressure

Maximum negative differential pressure

A

-1.0 PSI

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32
Q

Cabin Pressure

Safety relief valve setting

A

8.6 PSI

33
Q

Auto Flight System
Minimum AGL for autopilot use:

At take off

A

100 ft and at least 5s after lift off

34
Q

Auto Flight System
Minimum AGL for autopilot use:

In APCH with FINAL APP, V/S, or FPA

A

250 ft

35
Q

Auto Flight System
Minimum AGL for autopilot use:

In circling

A

500 ft

36
Q

Auto Flight System
Minimum AGL for autopilot use:

ILS when CAT I is displayed on the FMA

A

160 ft

37
Q

Auto Flight System
Minimum AGL for autopilot use:

ILS when CAT2 or CAT3 SINGLE or DUAL displayed on the FMA

A

0 ft if autoland

38
Q

Auto Flight System
Minimum AGL for autopilot use:

After manual go-around

A

100 ft

39
Q

Auto Flight System
Minimum AGL for autopilot use:

All other phases

A

500 ft

40
Q

Auto Flight System
Minimum AGL for autopilot use:

ILS CAT2 manual landing

A

80 ft

41
Q

Auto Flight System
Minimum AGL for autopilot use:

CAT II and CAT III fail passive autoland

A

approved in CONF 3 or FULL

42
Q

Auto Flight System
Minimum AGL for autopilot use:
Maximum wind for ILS CAT II or CAT III

Headwind

A

30 kt

43
Q

Auto Flight System
Minimum AGL for autopilot use:
Maximum wind for ILS CAT II or CAT III

Tailwind

A

10 kt

44
Q

Auto Flight System
Minimum AGL for autopilot use:
Maximum wind for ILS CAT II or CAT III

Crosswind

A

20 kt (15 for automatic rollout with OEI)

45
Q

Automatic Landing

ILS CAT I, CAT II, CAT III autoland

A

approved in CONF 3 or FULL

46
Q

Automatic Landing

Glide slope angle

A

-2.5° to 3.25°

47
Q

APU

After 3 start attempts

A

60 min before next attempt

48
Q

APU

Maximum EGT for start (below 35.000ft)

A

1090°C

49
Q

APU

Maximum EGT for start (above 35.000ft)

A

1120°C

50
Q

APU

APU running (Max temp)

A

675°C

51
Q

APU

APU start or shutdown is permitted during refueling/defueling (see conditions in FCOM)

A

APU

APU start or shutdown is permitted during refueling/defueling (see conditions in FCOM)

52
Q

APU

Operation (elec. power) and normal restart limit

A

41.000 ft

53
Q

APU

Battery start limit altitude

A

25.000ft

54
Q

Maximum altitude:

Assist engine start

A

20.000 ft

55
Q

Maximum altitude:

Air conditioning and pressurization (single pack)

A

22.500 ft

56
Q

Maximum altitude:

Air conditioning and pressurization (dual pack)

A

15.000 ft

57
Q

Maximum altitude:

APU bleed air for wing anti-ice is not permitted

A

Maximum altitude:

APU bleed air for wing anti-ice is not permitted

58
Q

Engines (CFM LEAP-1A26)
Thrust Setting/EGT Limits

Takeoff(1) and Go-around (normal)

(1) = Incl. TOGA, FLEX, and DERATE (if installed) thrust modes

A

Time limit: 5 min

EGT limit: 1060°C

59
Q

Engines (CFM LEAP-1A26)
Thrust Setting/EGT Limits

Takeoff(1) and Go-around (One engine out)

(1) = Incl. TOGA, FLEX, and DERATE (if installed) thrust modes

A

Time limit: 10 min

EGT limit: 1060°C

60
Q

Engines (CFM LEAP-1A26)
Thrust Setting/EGT Limits

MCT

A

Time limit: No limit

EGT limit: 1025°C

61
Q

Engines (CFM LEAP-1A26)
Thrust Setting/EGT Limits

Starting (on ground)

A

Time limit: -

EGT limit: 750°C

62
Q

Engines (CFM LEAP-1A26)
Thrust Setting/EGT Limits

Starting (In flight)

A

Time limit: -

EGT limit: 875°C

63
Q

Engines (CFM LEAP-1A26)
OIL

Maximum continuous temperature

A

140°C

64
Q

Engines (CFM LEAP-1A26)
OIL

Maximum transient temperature

A

15 min / 155°C

65
Q

Engines (CFM LEAP-1A26)
OIL

Minimum starting temperature

A

-40°C

66
Q

Engines (CFM LEAP-1A26)
OIL

Minimum temperature before take off

A

19°C

67
Q

Engines (CFM LEAP-1A26)
OIL

Minimum oil quantity

A

highest of:

10.6 qt

Or

8.9 qt + est. consumption
(max. 0.45 qt/hr)

68
Q

Engines (CFM LEAP-1A26)
OIL

Minimum oil pressure

A

17.4 PSI

69
Q

Starter

Ground starts

A

60s pause required between succesive cycles
(Cycle = max. 3 automatic start attemps)

after three failed cycles 15 min cooling period required

70
Q

GA SOFT mode is prohibited with OEI

A

GA SOFT mode is prohibited with OEI

71
Q

Flight controls

Max. altitude with slats and/or flaps extended

A

20.000 ft

72
Q

Fuel

JET A1 min. temperature

A

-43°C

73
Q

Fuel

Maximum temperature

A

(+55°C)

74
Q

Fuel

Minimum fuel quantity for take off

A

1500 kg

75
Q

Landing gear

Maximum brake temperature for take off
(Brake fans off)

A

300°C

76
Q

Landing gear

Maximum brake temperature for take off
(Brake fans on)

A

150°C

77
Q

Temperatures

Maximum lowest temperature for operation

A

-70°C at 39.800 ft

78
Q

Icing conditions

Temperature on ground or after takeoff?

A

at or below 10°C

+

Visible moistre

Visible moisture forms:
- clouds
- fog with vis. 1600m or less
- rain
- snow
- sleet
- ice crystals

+ when operating on twy/rwy with wet surface + temp ≤10°C

A320 Limitations (1 decks)

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