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A320 > Limitation > Flashcards

Limitation Flashcards

1
Q

Maneuver load (clean)

A

-1g to +2.5g

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2
Q

Maneuver load (other conf)

A

0g to +2g

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3
Q

Runway slope

A

±2%

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4
Q

Runway altitude

A

9.200ft
(YYB~YYL - 14.100ft)

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5
Q

Runway width

A

45m
minimal 30m

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6
Q

Maximum crosswind for takeoff

A

25kt (Gust Included)

Azul limitation

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7
Q

Maximum crosswind for landing

A

25kt (Gust Included)

Azul limitation

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8
Q

Maximum Tailwind for Takeoff

A

15kt

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9
Q

Maximum tailwind for landing

A

10kt

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10
Q

Maximum wind for passenger door operation

A

65kt

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11
Q

Maximum wind for FWD and AFT cargo door operation

A

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

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12
Q

The FWD and AFT cargo doors must be closed before the wind speed exceeds

A

65kt

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13
Q

Maximum recomended crosswind on wet and contaminated runways

A

15kt

*Note:​ The maximum crosswind values given in the above table are recommended values​based on Azul Safety Department assessement for regular operations.

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14
Q

Altitude limitation for landing on PFC/Grooved wet runways

A

Runway pressure altitude below 4 000ft

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15
Q

Cockpit window open maximum speed

A

200kt

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16
Q

Maximum flap/slat speeds A321

A

Flap 1 - 243kt (Holding)

Flap 1 + F - 225kt (Takeoff)

Flap 2 - 215kt (Takeoff/Approach)

Flap 3 - 195kt (Takeoff/Approach/Landing)

FULL - 186kt (Landing)

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17
Q

Maximum flap/slat speeds A320

A

Flap 1 - 230kt (Holding)

Flap 1 + F - 215kt (Takeoff)

Flap 2 - 200kt (Takeoff/Approach)

Flap 3 - 185kt (Takeoff/Approach/Landing)

FULL - 177kt (Landing)

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18
Q

Maximum operating speed VMO/MMO

A

350kt / M 0.82

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19
Q

Maximum speed with landing gear extended (VLE)

A

280kt/M.067

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20
Q

Maximum speed in wich the landing gear may be extended (VLO extension)

A

250kt/M.060

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21
Q

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

A

220kt/M.054

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22
Q

Maximum tire speed

A

195kt

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23
Q

Minimum control speed for landing (VMCL)

A

116kt

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24
Q

Wipers maximum operating speed

A

230kt

*Note:​ This limitation is applicable when the wipers are sweeping. It is not applicable if the wipers​are not sweeping for any reasons

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25
Q

Maximum taxi weigth A320

A

77 400 kg (170 637 lb)

79 400 kg (175 047 lb) (PR-YRD, PR-YRE, PR-YRH, PR-YRI, PR-YRJ, PR-YRK, PR-YRT, PR-YRU)

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26
Q

Maximum takeoff weight A320

A

77 000 kg (169 755 lb)

79 000 kg (174 165 lb) (PR-YRD, PR-YRE, PR-YRH, PR-YRI, PR-YRJ, PR-YRK, PR-YRT, PR-YRU)

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27
Q

Maximum landing weight A320

A

67 400 kg (148 591 lb)

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28
Q

Maximum zero fuel weight A320

A

64 300 kg (141 757 lb)

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29
Q

Minimum weight A320

A

40 600 kg (89 508 lb)

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30
Q

Maximum taxi weght A321

A

88 400 kg (197 093 lb)

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31
Q

Maximum takeoff weight A321

A

88 000 kg (196 211 lb)

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32
Q

Maximum landing weight A321

A

79 200 kg (174 606 lb)

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33
Q

Maximum zero fuel weight A321

A

75 600 kg (166 669 lb)

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34
Q

Minimum weight A321

A

46 600 kg (102 736 lb)

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35
Q

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

A

20 min

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36
Q

The flight crew must not use bleed air from the ___________ and from the ___________ at the​same time, to prevent any adverse effect on the Bleed Air System

A

APU BLEED

HP Air start unit

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37
Q

During ground operations and depending on the Outside Air Temperature (OAT), the flight crew must​limit the time that the aircraft electric power supply is used, in normal avionics ventilation system​configuration, as follows:

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​ - 0.5 h

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38
Q

Cabin pressure - maximum positive differential pressure

A

9.0 PSI

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39
Q

Cabin pressure - maximum negative differential pressure

A

-1.0 PSI

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40
Q

Cabin pressure - safety relief valve setting

A

8.6 PSI

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41
Q

Packs use with LP air conditioning unit

A

The flight crew must not use conditioned air from the packs and from the LP Air Conditioning Unit at​the same time, to prevent any adverse effect on the Air Conditioning system

42
Q

Use of autopilot at takeoff

A

100 ft AGL and at least 5s after takeoff

43
Q

Use of autopilot in approach with F-G/S mode

A

200 ft AGL

44
Q

Use of autopilot in approach with FINAL APP, V/S or FPA mode

A

250 ft AGL

45
Q

Use of autopilot in circling approach

A

500 ft AGL for aircraft category C (600 ft AGL for​aircraft category D)

46
Q

Use of autopilot in ILS/MLS approach when CAT 1 is displayed on the FMA

A

160 ft AGL

47
Q

Use of autopilot in ILS/MLS approach when CAT2, CAT3 SINGLE or CAT3 DUAL is displayed on FMA

A

0 ft AGL if autoland

48
Q

Use of autopilot after manual go-around

A

100 ft AGL

49
Q

Use of autopilot in all other fases

A

500 ft AGL

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: MDA/MDH or 500 ft AGL

50
Q

RNP accuracy with GPS PRIMARY - en route

A

With AP on - 1 NM

With AP off and FD on - 1 NM

With AP off and FD off - 1.1 NM

51
Q

RNP accuracy with GPS PRIMARY - in terminal area

A

With AP on - 0.5 NM

With AP off and FD on - 0.51 NM

With AP off and FD off - 0.51 NM

52
Q

RNP accuracy with GPS PRIMARY - in approach

A

With AP on - 0.3 NM

With AP off and FD on - 0.3 NM

With AP off and FD off - 0.3 NM with F-LOC​​ deviation​ (Not authorized without ​F-LOC​ ​ deviation)

53
Q

If GPS PRIMARY LOST is displayed on the ND and MCDU

A

The navigation accuracy remains​sufficient for RNP operations provided that, the RNP value is checked or entered on the MCDU ​and HIGH ACCURACY is displayed

54
Q

ILS CAT II minimum decision height

A

100 ft

(For manual landing, AP should be disconnected no later than 80 ft AGL)

55
Q

Limit of APU start attempt

A

After three consecutive APU start attempts, the flight crew must wait 60 min before a new start​attempt

56
Q

APU maximum N speed

A

107 %

57
Q

APU maximum EGT for start (bellow 25 000 ft)

A

900 ºC

58
Q

APU maximum EGT for start (above 25 000 ft)

A

982 ºC

59
Q

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

A

682 ºC

60
Q

Maximum EGT for APU running (for immediate shutdown)

A

700 ºC to 742 ºC

61
Q

APU operation and normal restart envelope

A

41 000 ft

62
Q

APU battery restart limit (Elec emerg config)

A

25 000 ft

63
Q

Maximum altitude for use of APU BLEED

A

20 000 ft

64
Q

APU BLEED maximum altitude to assist engine start

A

20 000 ft

65
Q

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

A

20 000 ft

22 500 ft (PR-YRT, PR-YRU)

66
Q

APU BLEED maximum altitude altitude for air conditioning and pressurization (dual pack operation)

A

15 000 ft

67
Q

TOGA/FLEX/EGT time and temperature limit (all engines operative)

A

Time limit 5 minutes

EGT limit 1060 ºC

68
Q

TOGA/FLEX/EGT time and temperature limit (one engine inoperative)

A

Time limit 10 minutes

EGT limit 1060 ºC

69
Q

Maximum continuous thrust time and temperature limit

A

Time not limited

EGT limit 1025 ºC

70
Q

EGT temperature limit starting (on ground)

A

750 ºC

71
Q

EGT temperature limit starting (in flight)

A

875 ºC

72
Q

Maximum N1

A

101 %

*Note:​ The N1 limit depends on the ambient conditions and on the configuration of the engine air​bleed. These parameters may limit N1 to a value that is less than the above-mentioned N1​value

73
Q

Maximum N2

A

116.5 %

74
Q

Oil temperature - maximum continuous temperature

A

140 ºC

75
Q

Oil temperature - maximum transient temperature (15 min)

A

155 ºC

76
Q

Oil temperature - minumum starting temperature

A

-40 ºC

-29 ºC (PR-YRA, PR-YRB, PR-YRC, PR-YRD, PR-YRE, PR-YRF, PR-YRH, PR-YYI, PR-YYJ, PR-YYK, PR-YYL)

77
Q

Oil temperature - minumum temperature before takeoff

A

19 ºC

78
Q

Minimum oil quantity

A

The minimum oil quantity is the highest value of:

​‐​ 10.6 qt, or​
‐​ 8.9 qt + estimated consumption.​

Maximum estimated consumption = 0.45 qt/h

79
Q

Minimum oil pressure

A

17.4 PSI

80
Q

Maximum oil pressure (when oil temperature is above 50 °C)

A

130.5 PSI

81
Q

Maximum oil pressure (when oil temperature is bellow 50 °C)

A

145 PSI

82
Q

Starter attempts and time for cooling

A

‐​ A standard automatic start that includes up to three start attempts, is considered one cycle​

‐​ For ground starts (automatic or manual), a 60 s pause is required between successive cycles

​‐​ A 15 min cooling period is required, subsequent to three failed cycles

​‐​ The starter must not be run when N2 is above 63 %

83
Q

Maximum reverse thrust speed limitation

A

Maximum reverse should not be used below 70 kt. Idle reverse is permitted down to aircraft stop

84
Q

FLEX temperature limitation

A

TFLEX cannot be:

​‐​ Higher than TMAXFLEX, equal to ISA + 55 °C. (+50 ºC on LEAP 1A 29K) (+52 ºC on LEAP 1A 32K)

​‐​ Lower than the flat temperature (TREF).​

‐​ Lower than the actual OAT.

85
Q

Engine crosswind limitation for start

A

45 kt

86
Q

Engine crosswind limitation for takeoff

A

35 kt (gust included)

87
Q

Maximum altitude with flaps/slats extended

A

20 000 ft

88
Q

Fuel imbalance at takeoff - inner tanks (outer tanks balanced) - A320

A

Full - 500 kg (1 102 lb)

3 000 kg (6 613 lb) - 1 050 kg (2 314 lb)

1 450 kg (3 196 lb) - 1 450 kg ( 3 196 lb)

89
Q

Outer tanks maximum assimetry (inner tanks ballanced)

A

370 kg (815 lb)

90
Q

Fuel imbalance in flight and at landing - inner tanks (outer tanks balanced) - A320

A

Full - 1 500 kg (3 306 lb)

4 300 kg (9 479 lb)​ - 1 600 kg (3 527 lb)

2 250 kg (4 960 lb)​ 2 250 kg (4 960 lb)

*There is no limitation below 2 250 kg​(4 960 lb)

91
Q

Outer tanks maximum assimetry

A

690 kg (1 521 lb)

The maximum fuel imbalance in the outer wing fuel tanks (one full/one empty) is allowed provided​that:​

‐​The fuel quantity of the outer and inner wing fuel tanks of one side is equal to the fuel quantity of​the outer and inner wing fuel tanks on the other side, or​

‐​On the side of the lighter outer tank, the fuel quantity of the inner tank is more than the fuel​quantity of the opposite inner tank. The difference between the fuel quantity in the inner tanks​should not be more than 3 000 kg (6 613 lb).

​*Note:​ In exceptional conditions (i.e. fuel system failure), the above-mentioned values for​maximum fuel imbalance may be exceeded without significant effect to the aircraft​handling qualities. The aircraft remains fully controllable in all flight phases

92
Q

Fuel imbalance at takeoff - A321

A

Full​ - 400 kg (882 lb)

3 000 kg (6 614 lb)​ - 400 kg (882 lb)

700 kg (1 543 lb)​ - 700 kg (1 543 lb)

93
Q

Fuel imbalance in flight and at landing

A

Full​ - 1 320 kg (2 910 lb)

4 000 kg (8 818 lb)​ - 1 450 kg (3 196 lb)

2 350 kg (5 180 lb)​ - 2 350 kg (5 180 lb)

*Note:​ In exceptional conditions (i.e. fuel system failure), the above-mentioned values for​maximum fuel imbalance may be exceeded without significant effect to the aircraft​handling qualities. The aircraft remains fully controllable in all flight phases.

94
Q

Minimum fuel quantity for takeoff

A

1 500 kg (3 307 lb)

The ECAM alerts that are related to fuel low level in the wing tanks (FUEL WING TK LO LVL, etc.)​must not appear for takeoff

95
Q

Use of rain repellent

A

Moderate or heavy rain

95
Q

Maximum brake temperature for takeoff (brake fan off)

A

300 ºC

96
Q

Maximum NWS angle

A

±85 °

97
Q

Maximum tire speed during turn if one tire per gear is deflated

A

7 kt

98
Q

Maximum tire speed during turn if two tires on the same main gear is deflated

A

3 kt

99
Q

Maximum NWS with tire deflated

A

30 º

A320 (3 decks)

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