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A320 Rating > A320 Limitations > Flashcards

A320 Limitations Flashcards

1
Q

A320 Load Acceleration Limit

A

Clean Config -1g - +2.5g
Other Config 0g - +2g

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2
Q

Maximum Pressure Altitude

A

39 800 ft

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3
Q

Maximum Runway Altitude

A

9 200 ft

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4
Q

Maximum Runway Slope

A

+/- 2%

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5
Q

Runway Width

A

Nominal 45m
Minimum 30m

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6
Q

Maximum Demonstrated Crosswind

A

38kts (Gust Included)

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7
Q

Maximum Tailwind

A

15kts Takeoff and Landing
Tailwind greater than 10kts require Full Flap Landing

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8
Q

Maximum Wind for Passenger Door Operation

A

65kts

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9
Q

Maximum wind for Cargo Door Operation

A

40kts (or 50kts if aircraft nose into wind or doors on leeward)
Cargo Doors must be closed before wind speed exceeds 65kts

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10
Q

Maximum Speed for Cockpit window open

A

200kts

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11
Q

Maximum Flap/Slat Speeds for Flaps 1

A

1 230kts (Holding)
1+F 215kts (Take Off)

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12
Q

Maximum Flap/Slat Speeds for Flaps 2

A

2 - 200kts (Take Off/Approach)

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13
Q

Maximum Flap/Slat Speeds for Flaps 3

A

3 - 185kts (Take Off/Approach/Landing)

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14
Q

Maximum Flap/Slat Speeds for Flaps Full

A

Full - 177kts (Landing)

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15
Q

Maximum Operating Speeds VMO/MMO

A

VMO - 350 until ~25 000ft
MMO - M0.82

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16
Q

Maximum Speed for VLE (Extended)

A

280kts or M0.67

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17
Q

Maximum Speed for VLO Extension

A

250kts or M0.60

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18
Q

Maximum Speed for VLO Retraction

A

220kts or M0.54

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19
Q

Maximum Tire Speed

A

195kts

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20
Q

Minimum Control speed for landing (VMCL)

A

109kt

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21
Q

Minimum Control Speed in air (VMCA)

A

112kts at Sea level decreasing with altitude

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22
Q

Minimum Control Speed on the ground (VMCG)

A

1+F 112kts at Sea Level

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23
Q

Maximum Taxi Speed Turn

A

20kts

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24
Q

Maximum Speed for Wipers Operation

A

230kts

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25
Q

Maximum Taxi Weight

A

71 900kg

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26
Q

Maximum Take off Weight (Brake Release)

A

71 500kg

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27
Q

Maximum Landing Weight

A

66 000kg

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28
Q

Maximum Zero Fuel Weight

A

62 500kg

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29
Q

Minimum Weight

A

37 230kg

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30
Q

Maximum Time for No Aircon on Ground

A

20 minutes recommended

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31
Q

Avionics Ventilation ground Operation Limit

A

OAT less than or equal 49C - No limitation

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32
Q

Cabin Differential Limits & Safety Relief Valve Setting

A

-1.0 PSI to 9.0PSI
8.6PSI

33
Q

Maximum Normal Cabin Alt

A

8000ft

34
Q

Cabin Altitude Warning
Max Cabin Altitude Selection

A

9550ft +/- 350ft
14 000 ft

35
Q

Minimum Height for Autopilot Engagement on Take Off

A

100ft AGL and at least 5 seconds after lift off

36
Q

Minimum Height for Autopilot Circling Approach

A

500ft AGL (Cat C)
600ft AGL (Cat D)

37
Q

Minimum height for Autopilot F-G/S Mode

A

200ft AGL

38
Q

Minimum height for Autopilot FINAL APP, V/S or FPA mode

A

250ft AGL

39
Q

Minimum height for Autopilot ILS/MLS with CAT I Displayed

A

160ft AGL

40
Q

Minimum height for Autopilot ILS/MLS with CAT II or CAT III (Single or dual)

A

0ft AGL if Autoland
80ft AGL Manual landing CAT II

41
Q

Minimum height for Autopilot GLS with CAT I Displayed

A

160ft AGL

42
Q

Minimum height for Autopilot GLS with AUTO LAND displayed

A

0ft AGL if Autoland

43
Q

Minimum height for Autopilot LPV approach with (SLS) when APPR1 is displayed

A

160ft AGL

44
Q

Minimum height for Autopilot engagement after Manual Go Around

A

100ft AGL

45
Q

Minimum height for Autopilot all other modes

A

500ft AGL

46
Q

ILS CAT III Fail Passive (Single) MDH

A

50ft AGL

47
Q

ILS CAT III Fail Operational (Dual)

A

Alert Height 100ft
CAT III with DH - Minimum DH 22ft
CAT III without DH - Minimum RVR 75m

48
Q

CAT II/CAT III Fail Passive Autoland Engine out Approach Requirements

A

Configuration Full & procedures completed prior to 1000ft AGL

49
Q

Maximum Wind Conditions for ILS/MLS CAT II/CAT III & GLS CAT I

A

Headwind 30kts
Tailwind 10kts
Crosswind
20kts without Automatic Rollout
15kts with Automatic Rollout

50
Q

Autoland Limitations;
Config
Glideslope Angle
Airport Elevation
Aircraft Weight
Pressure Altitude

A

CONF 3 and CONF FULL
Angle -2.5 to -3.15
Airport below 6500ft
Weight below Maximum Landing Weight
-1000ft Pressure Altitude

51
Q

APU Start Attempts

A

After 3 Attempts must wait 60 min prior to new attempt

52
Q

Maximum APU Rotor Speed

A

107% N

53
Q

Maximum APU EGT

A

Start Below 35 000ft 1,090 C
Start Above 35 000ft 1,120 C
While Running 675 C

54
Q

APU Bleed - Maximum Altitude to Assist engine start

A

20,000ft

55
Q

APU Bleed - Maximum Altitude for Air conditioning and pressurization (single Pack)

A

22,500ft

56
Q

APU Bleed - Maximum Altitude for Air Conditioning and Pressurisation (Dual Pack)

A

15,000ft

57
Q

TOGA EGT Limitation

A

635 C
AEO - 5 min
OEI - 10 min

58
Q

MCT EGT Limtitation

A

610 C
No Time Limit

59
Q

Engine Starting EGT Limitations

A

635 C on ground and in flight

60
Q

Oil Temperature Limitations

A

Max Continuous 155 C
Max Transient (15min) 165 C
Min Starting -40 C
Min Before Above Idle -10 C
Min before Takeoff 50 C

61
Q

Minimum Oil Quantity

A

11 qt + Estimated Consumption (0.3qt/h)

62
Q

Minimum Oil Pressure

A

60 psi

63
Q

Maximum Total Engine Crank Time

A

5 min

64
Q

Maximum manual Engine start cycle time

A

2 min

65
Q

Engine Start Cycle Limits

A

3 Starts Total with 15 second pause, then 30 minutes cooling period

66
Q

Engine N2 Starter Limitations

A

Starter must not be run when N2 is above 10% on ground and 18% in flight

67
Q

Reverse Thrust on landing Limits

A

Max reverse not to be used below 70kts
Idle reverse permitted to aircraft stop

68
Q

Engine Crosswind Start limit

A

35kts

69
Q

Maximum Altitude for Operating with slat and/or flaps extended

A

20 000ft

70
Q

Fuel Temperature Limits (JET A1)

A

Minimum -43 C
Maximum 54 C

71
Q

Maximum Fuel Imbalance (Takeoff - Inner Tanks)

A

500kg if other tank full

Maximum allowable asymmetry increase as heavier tank reduces in quantity

72
Q

Maximum Fuel Imbalance (Takeoff - Outer Tanks)

A

370kg

73
Q

Maximum Fuel Imbalance (In flight and Landing - Inner Tanks)

A

1500kg if other tank full

Maximum allowable asymmetry increase as heavier tank reduces in quantity

74
Q

Maximum Fuel Imbalance (In flight and Landing - Outer Tanks)

A

690kg

75
Q

Minimum Fuel Quantity for Takeoff

A

1500kg

76
Q

Definition of severe ice accretion

A

Ice accumulation on the airframe reaches approximately 5mm thick or more

77
Q

Maximum brake temperature for Take Off

A

300 C

78
Q

Maximum nose wheel steering angle

A

+/-85

79
Q

Taxi with deflated or damaged tyres

A

One tyre per gear deflated 7kts during turn
Two tyre deflated on same main gear 3kts Maximum
Maximum NWS Angle 30 Degrees

A320 Rating (3 decks)

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