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1 Airbus A320 > Limitations > Flashcards

Limitations Flashcards

1
Q

Tailwind for Takeoff:

A

15kt

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2
Q

Tailwind for Landing:

A

10kt

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3
Q

Maximum taxi speed(DRY):

A

30kt

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4
Q

Maximum taxi speed(WET):

A

15kt

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5
Q

Maximum taxi speed during a turn (DRY):

A

10kt

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6
Q

Maximum taxi speed during a turn (WET):

A

5kt

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7
Q

Maximum Operating Altitude / Runway altitude:

A

9.200ft

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8
Q

VMO/MMO:

A

350KT / M 0.82

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9
Q

Maximum speed with landing gear extended (VLE):

A

280kt / M 0.67

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10
Q

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

A

250kt / M 0.60

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11
Q

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

A

220kt / M 0.54

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12
Q

Maximum speed with windshield wipers in use:

A

230kt

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13
Q

Maximum speed with cockpit window open:

A

200kt

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14
Q

VFE Flaps 0, 1, 1+F, 2, 3, full

A

VMO/MMO, 230, 215, 200, 185, 177

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15
Q

TOGA all engines time/ temperature

A

5 min/ 1.060 °C

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16
Q

TOGA One engine inoperative time/ temperature

A

10 min/ 1.060 °C

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17
Q

MCT limit time/ temperature

A

No time limit/ 1.025 °C

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18
Q

Starting engine temperature on ground/ in flight

A

750 °C/ 875 °C

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19
Q

Maximum taxi weight:

A

77.400 kg / 79.400 kg

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20
Q

Maximum takeoff weight (brake release):

A

77.000 kg / 79.000 kg

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21
Q

Maximum landing weight:

A

67.400 kg

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22
Q

Maximum zero fuel weight:

A

64.300 kg

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23
Q

Minimum weight:

A

40.600 kg

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24
Q

A321 Maximum taxi weight

A

89 400 kg

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25
Q

A321 Maximum takeoff weight (brake release)

A

89 000 kg

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26
Q

A321 Maximum landing weight

A

79 200 kg

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27
Q

A321 Maximum zero fuel weight

A

75 600 kg

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28
Q

A321 Minimum weight

A

46 600 kg

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29
Q

LOAD ACCELERATION LIMITS clean/ other

A

-1 g to +2.5 g/ 0 g to +2 g

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30
Q

Runway slope (mean)

A

±2 %

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31
Q

Runway altitude

A

14 100 ft/9 200 ft

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32
Q

The maximum wind for passenger door operation is 65 kt ‐ The maximum wind for FWD and AFT cargo door operation is 40 kt (or 50 kt, if the aircraft nose is into the wind, or if the FWD and AFT cargo doors are on the leeward side) ‐ The FWD and AFT cargo doors must be closed before the wind speed

A

exceeds 65 kt

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33
Q

Landing distance reduction associated with Porous Friction Course (PFC)/Grooved wet runways is applicable only if runway pressure altitude is below

A

4 000 ft.

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34
Q

A321 VFE Flaps 0, 1, 1+F, 2, 3, full

A

VMO/ MMO, 243, 225, 215, 195, 186

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35
Q

MAXIMUM TIRE SPEED , Maximum ground speed

A

195 kt

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36
Q

VMCL

A

116 kt

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37
Q

Maximum ceiling

A

39,800ft

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38
Q

The maximum wind for passenger door operation is

A

65 kt

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39
Q

The maximum wind for FWD and AFT cargo door operation is

A

40 kt (or 50 kt, if the aircraft nose is into the wind, or if the FWD and AFT cargo doors are on the leeward side)

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40
Q

The flight crew must not use bleed air from the APU BLEED and from the HP Air Start Unit at the same time, to prevent

A

any adverse effect on the Bleed Air System.

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41
Q

AVIONICS VENTILATION OAT ≤ 49 °C

A

No limitation

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42
Q

Maximum positive differential pressure

A

9.0 PSI

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43
Q

Maximum negative differential pressure

A

-1.0 PSI

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44
Q

Safety relief valve setting

A

8.6 PSI

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45
Q

Maximum differential pressure (Δp) and safety valve setting tolerance =

A

± 7 hPa (0.1 PSI)

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46
Q

Outflow valve closure

A

15,000ft

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47
Q

Maximum cabin altitude selection

A

14,000ft

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48
Q

Cabin Alt warning

A

9,550 +- 350ft

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49
Q

Maximum normal cabin altitude

A

8,000ft

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50
Q

Minimum cabin altitude selection

A

-2,000ft

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51
Q

The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at the same time, to prevent

A

any adverse effect on the Air Conditioning system.

52
Q

AP At takeoff

A

100 ft AGL and at least 5 s after liftoff

53
Q

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

A

250 ft AGL

54
Q

AP In circling approach

A

500 ft AGL for aircraft category C

55
Q

AP ILS/MLS approach when CAT1 is displayed on the FMA

A

160 ft AGL

56
Q

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

A

0 ft AGL if autoland

57
Q

AP After a manual go-around

A

100 ft AGL

58
Q

AP In all other phases

A

500 ft AGL

59
Q

All other phases The AP or FD in OP DES or DES mode can be used in approach. However, its use is only permitted if the FCU selected altitude is set to, or above, the higher of the two:

A

MDA/MDH or 500 ft AGL

60
Q

A321 all other phases

A

900 ft AGL

61
Q

If GPS PRIMARY LOST is displayed on the ND and MCDU, the navigation accuracy remains sufficient for RNP operations provided that,

A

the RNP value is checked or entered on the MCDU and HIGH ACCURACY is displayed.

62
Q

NAV mode may be used after takeoff provided that:

A

‐ GPS PRIMARY is available, or ‐ The flight crew checked the FMGS takeoff updating.

63
Q

APU bleed Max altitude to assist engine start

A

20 000 ft

64
Q

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

A

20 000 ft

65
Q

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

A

15 000 ft

66
Q

Use of APU bleed air for wing anti-ice is

A

not permitted

67
Q

The In-Seat Power Supply System (ISPSS) for the Portable Electronic Device (PED) carried by the passengers must be

A

turned off during takeoff and landing.

68
Q

After three consecutive APU start attempts, the flight crew must wait

A

60 min before a new start attempt.

69
Q

Maximum EGT for APU start (below 25 000 ft)

A

900 °C

70
Q

Maximum EGT for APU start (above 25 000 ft)

A

982 °C

71
Q

Maximum EGT for APU running (with 5 s confirmation for shutdown)

A

682 °C

72
Q

Maximum EGT for APU running (for immediate shutdown)

A

700 °C to 742 °C

73
Q

Engine Maximum N1

A

101 %

74
Q

Engine Maximum N2

A

116.5 %

75
Q

Maximum continuous temperature

A

140 °C

76
Q

Maximum transient temperature (15 min)

A

155 °C

77
Q

AP A321 Circling Approach

A

600 ft AGL for aircraft category D

78
Q

Nominal runway width

A

45m

79
Q

Minimal runway width

A

30m

80
Q

Maximum certified crosswind for takeoff

A

35kt gust included- AFM and engine limitation

81
Q

Maximum demonstrated crosswind for landing

A

38kt gust included- not AFM, but certification campaign

82
Q

Cockpit window open maximum speed

A

200kt

83
Q

Outflow valve closure

A

15,000ft

84
Q

CAT II minimum decision height

A

100ft

85
Q

CAT II for manual landing, AP should be disconnected no later than

A

80ft

86
Q

ILS CAT II A321 maximum headwind, tailwind, crosswind:

A

15, 10, 10kt

87
Q

A320 ILS CATII maximum headwind, tailwind, crosswind:

A

30, 10, 20 (15 if OEI)

88
Q

Oil maximum continuous temperature

A

140 C

89
Q

Oil max transient temperature (15 min)

A

155 C

90
Q

Oil minimum start temperature

A

-40C

91
Q

Oil minimum temperature before takeoff

A

19C

92
Q

Minimum oil pressure

A

17.4 PSI

93
Q

Max oil pressure above 50C

A

130.5 PSI

94
Q

Max oil pressure above 50C

A

145 PSI

95
Q

Engine starter- one cycle standard automatic start

A

Up to 3 attempts

96
Q

Automatic or manual ground starts, pause required between successive cycles

A

60s

97
Q

Engine starter must not be run when N2 is above

A

63%

98
Q

TFLEX can not be higher than TMAXFLEX equal to ISA+

A

55C

99
Q

TFLEX can not be lower than

A

Flat temperature (TREF) an actual OAT

100
Q

Max crosswind for engine start

A

45 kt

101
Q

Engine crosswind limit at takeoff

A

35kt

102
Q

Max operating altitude with slats/flaps extended

A

20,000 ft

103
Q

Max fuel imbalance at takeoff- tank full

A

500kg

104
Q

Max fuel imbalance at takeoff- heavier tank

A

1.050kg max asymmetry

105
Q

Max fuel imbalance at takeoff- inner - heavier tank 1,450 kg

A

1,450 kg max asymmetry

106
Q

Max fuel imbalance outer tanks (inner balanced)

A

370kg

107
Q

Max fuel imbalance inner in flight and landing- heavier tank full

A

1500kg

108
Q

Max fuel imbalance in flight and landing heavier tank 4,300kg

A

1,600kg

109
Q

Max fuel imbalance in flight and landing- heavier tank 2,250kg

A

2,250kg

110
Q

Max fuel imbalance in flight and landing outer tanks

A

690kg

111
Q

A321 max fuel imbalance at takeoff inner heavier full

A

400kg

112
Q

A321 Max fuel imbalance takeoff heavier 3,000kg

A

400kg

113
Q

A321 Max fuel imbalance takeoff inner heavier 700kg

A

700kg

114
Q

A321 max fuel imbalance inner in flight and landing heavier full

A

1,320kg

115
Q

A321 max fuel imbalance inner heavier 4,000kg in flight and landing

A

1,450kg

116
Q

A321 max fuel imbalance inner in flight and landing heavier 2,350kg

A

2,350kg

117
Q

Minimum fuel for takeoff

A

1,500kg

118
Q

Definition of icing conditions- OAT on ground or TAT in flight at or below

A

10C and visible moisture in 1SM 1,600m or less

119
Q

Severe ice accretion

A

5 mm on airframe or more

120
Q

Rain repellent only in rain

A

Moderate or heavy

121
Q

Max brake temperature for takeoff fans off

A

300C

122
Q

Max NWS angle

A

+_85 degrees

123
Q

Max taxi speed one tire deflated

A

7kt

124
Q

Max speed 2 tires deflated on same main gear

A

3kt

125
Q

Max NWS angle tire deflated

A

30 degrees

126
Q

Ground IRS alignment possible between latitude

A

73 degrees N and S

1 Airbus A320 (22 decks)

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