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Airbus 320 > Limitations A320 PR-MYX (MSN 5342) > Flashcards

Limitations A320 PR-MYX (MSN 5342) Flashcards

1
Q

Flight Maneuvering Load Acceleration Limits

A

Clean Configuration: -1 g/+2.5 g
Other Configurations: 0 g/+2 g

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2
Q

Maximum/minimum takeoff altitude

A

14.100 ft / -2.000 ft

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3
Q

Maximum Operating Altitude

A

39.800 ft

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4
Q

Runway Slope

A

+/- 2 %

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5
Q

Runway Altitude (max)

A

14.100 ft

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6
Q

Nominal Runway Width

A

45 m

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7
Q

Minimal Runway Width

A

30 m

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8
Q

Maximum demonstrated crosswind for takeoff and landing

A

38 kt

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9
Q

Maximum tailwind for takeoff

A

15 kt

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10
Q

Maximum tailwind for landing

A

15 kt

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11
Q

Whenever a tailwind exceeds 10kt, which flap configuration must be used for landing?

A

Flaps Full

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12
Q

Maximum wind for passenger door operation

A

65 kt

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13
Q

Maximum wind for FWD and AFT cargo door operation

A

*40 kt
*50 kt if the aircraft nose is into the wind and cargo doors are on the leeward side

Note: The FWD and AFT cargo doors must be closed before the wind speed exceeds 65 kt

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14
Q

Maximum taxi weight

A

77.400 kg

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15
Q

Maximum takeoff weight

A

77.000 kg

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16
Q

Maximum landing weight

A

66.000 kg

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17
Q

Maximum zero fuel weight

A

62.500 kg

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18
Q

Minimum weight

A

37.230 kg

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19
Q

Cockpit Window Open Maximum Speed

A

200 kt

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20
Q

Maximum Flap/Slat Speeds

A

Conf 0 - VMO/MMO
Conf 1 - 230 kt
Conf 1+F - 215 kt
Conf 2 - 200 kt
Conf 3 - 185 kt
Conf Full - 177 kt

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21
Q

VMO/MMO

A

350 kt / M 0.82

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22
Q

Maximum Speeds with the Landing Gear Extended

A

*Gear Extended (VLE) - 280 / M 0.67
*Gear Extension (VLO extension) - 250 / M 0.60
*Gear Retraction (VLO retraction) - 220 / M 0.54

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23
Q

Maximum Tire Speed

A

195 kt

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24
Q

Minimum Control Speed for Landing

A

VMCL = 113 kt

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25
Q

Taxi Speed Limitation

A

When the takeoff weight is higher than 76.000 kg - Do not exceed a taxi speed of 20 kt during a turn

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26
Q

Wipers Maximum Operating Speed

A

230 kt

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27
Q

Air conditioning supply limitation

A

With passengers on board, it is not recommended to exceed 20 min without air conditioning supply.

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28
Q

APU Bleed & HP Air Start Unit Limitation

A

The crew must not use air from the APU Bleed and from the HP Air Start unit at the same time to prevent any adverse effect on the Bleed Air System

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29
Q

Avionics Temperature Limitation

A

*OAT ≤ 49 C = no limitation
*49 C < OAT ≤ 55 C = 2 h
*55 C < OAT ≤ 60 C = 1 h
*60 C < OAT ≤ 64 C = 30 min

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30
Q

Cabin Pressure
Maximum Positive/Negative Differential Pressure

A

*Maximum positive: 9.0 PSI
*Maximum negative: -1.0 PSI
*Safety relief valve setting: 8.6 PSI

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31
Q

Maximum normal cabin altitude

A

8.000 ft

32
Q

Cabin Altitude warning

A

9.550 ft (+/- 350 ft)

33
Q

APU Bleed & LP air conditioning unit limitation

A

The crew must not use air from the APU Bleed and from the LP air conditioning unit at the same time to prevent any adverse effect on the Bleed Air System

34
Q

Minimum autopilot use after takeoff

A

100 ft AGL and at least 5 seconds after liftoff

35
Q

Minimum autopilot use with FINAL APP, V/S or FPA modes

A

250 ft AGL

36
Q

Minimum autopilot use for circling approach

A

*500 ft AGL for cat C
*600 ft AGL for cat D

37
Q

Minimum autopilot use with CAT 1 displayed on the FMA

A

160 ft AGL

38
Q

Minimum autopilot use with CAT 2 or CAT 3 (single or dual) displayed on the FMA

A

0 ft AGL

39
Q

Minimum autopilot use after a go-around

A

100 ft AGL

40
Q

Minimum autopilot use in all other phases

A

500 ft AGL

41
Q

ILS CAT II Limitations

A

*Minimum decision height = 100 ft
*At least one autopilot engaged in APPR mode
*CAT 2, CAT 3 Single or CAT 3 Dual must be displayed on the FMA

Note: Manual landing A/P Off no later than 80 ft AGL

42
Q

ILS CAT III Single (Fail Passive) Limitations

A

*Minimum descent height = 50 ft
*A/THR must be used in selected or managed speed
*CAT 3 Single or CAT 3 Dual must be displayed on the FMA

43
Q

Alert Height

A

AH = 100 ft

44
Q

ILS CAT III Dual (Fail Operational) Limitations

A

*Alert Height = 100 ft
*A/THR must be used in selected or managed speed
*CAT 3 Dual must be displayed on the FMA

45
Q

CAT III with DH - minimum DH

A

Minimum DH = 22 ft

46
Q

CAT III with no DH - minimum RVR

A

Minimum RVR = 75 m

47
Q

CAT II and CAT III Fail Passive engine out autoland limitations

A

*Approved only in Conf Full
*Engine out procedures must be completed before reaching 1.000 ft in approach

48
Q

Maximum autoland wind limitations (headwind, crosswind, tailwind)

A

*Headwind: 30 kt
*Crosswind: 20 kt (no auto rollout) / 15 kt (with automatic rollout)
*Tailwind: 10 kt

49
Q

Autoland approved landing configurations

A

Conf 3 and Conf Full

50
Q

Autoland maximum glideslope angle

A

-3.15°

51
Q

Automatic Landing
Minimum glideslope angle

A

-2.5

52
Q

Maximum/minimum autoland altitude limit

A

Maximum: 9.200 ft
Minimum: -1.000 ft pressure altitude

53
Q

Autoland maximum weight limit

A

With aircraft at or below the maximum landing weight

54
Q

Automatic rollout performance vs.
Runway condition

A

*Approved on dry and wet runways
*Performance not demonstrated on contaminated runways

55
Q

Automatic rollout:
One engine/thrust reverser inoperative limitations

A

The remaining thrust reverser can be used provided that:
*No more than idle thrust is used
*The wind does not exceed the maximum wind conditions for automatic rollout

56
Q

APU starter limitations

A

After 3 consecutive start attempts, the flight crew must wait 60 minutes before a new start attempt

57
Q

APU bleed air limitations

A

*Max altitude for assisted start - 20.000 ft
*Max altitude for single pack ops - 22.500 ft
*Max altitude for dual pack ops - 15.000 ft
*Use of APU bleed for wing anti-ice is not permitted

58
Q

Maximum altitude with flaps/slats extended

A

20.000 ft

59
Q

Use of flight controls limitation

A

Rapid and large alternating control inputs, especially in combination with large changes in pitch, roll or yaw (e.g. large sideslip angles) may result in structural failures at any speed

60
Q

Fuel Temperatures (max/mini) Jet A / Jet A1

A

*Jet A
Maximum = +54 °C
Minimum = -36 °C

*Jet A1
Maximum = +54 °C
Minimum = -43 °C

61
Q

Minimum fuel quantity for takeoff

A

1.500 kg

Note: ECAM fuel-related low level alerts for the wing tanks must not appear for takeoff

62
Q

Maximum brake temperature for takeoff (brake fans off)

A

300 °C

63
Q

Maximum NWS angle

A

+/- 85°

64
Q

Taxi with deflated tires

A

1 tire deflated on the main gear = 7 kt
2 tires deflated on the same main gear = 3 kt
Maximum NWS angle = 30 deg

65
Q

IR ground alignment limitation

A

Between Latitudes 73°N and 73°S

66
Q

RNP Accuracy with GPS Primary
(AP ON)

A

Enroute: 1 nm
Terminal: 0,5 nm
Approach: 0,3 nm

67
Q

RNP Accuracy with GPS Primary
(AP OFF / FD ON)

A

Enroute: 1 nm
Terminal: 0,51 nm
Approach: 0,3 nm

68
Q

RNP Accuracy with GPS Primary
(AP OFF / FD OFF)

A

Enroute: 1,1 nm
Terminal: 0,51 nm
Approach: N/A

69
Q

Maximum APU rotor speed (N)

A

N = 107%

70
Q

APU EGT limitations

A

Max EGT for start (FL350B) = 1090 °C
Max EGT for start (FL350A) = 1120 °C
Max EGT for APU running = 675 °C

71
Q

APU battery restart limit (EMER ELEC CONF)

A

25.000 ft

72
Q

Power Supply for PEDs

A

In seat power supply system (ISPSS) for PEDs must be turned off during takeoff and landing

73
Q

GSM Onboard limitations

A

*Mobile phones must not be used in the lavatories and the cockpit
*Below 3000 m AGL (~ 10.000 ft)
*In some geographical areas

74
Q

Rain repellent usage

A

Crews should use rain repellent in case of moderate to heavy rain

75
Q

Definition of Icing Conditions

A

Icing conditions exist when OAT or TAT is at or below +10 °C and visible moisture in any form is present (clouds, fog with visibility of 1600 m or less, rain, snow, etc)

76
Q

Maximum brake temperature for takeoff (brake fans ON)

A

150 °C

Airbus 320 (6 decks)

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